CA2031521C - Aerial gunnery target - Google Patents
Aerial gunnery targetInfo
- Publication number
- CA2031521C CA2031521C CA002031521A CA2031521A CA2031521C CA 2031521 C CA2031521 C CA 2031521C CA 002031521 A CA002031521 A CA 002031521A CA 2031521 A CA2031521 A CA 2031521A CA 2031521 C CA2031521 C CA 2031521C
- Authority
- CA
- Canada
- Prior art keywords
- vented
- inflator
- target
- visual augmenter
- hoop
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41J—TARGETS; TARGET RANGES; BULLET CATCHERS
- F41J9/00—Moving targets, i.e. moving when fired at
- F41J9/08—Airborne targets, e.g. drones, kites, balloons
- F41J9/10—Airborne targets, e.g. drones, kites, balloons towed
Abstract
An aerial gunnary target (42) which is towed behind a towing aircraft (24). The gunnery target includes an extension device (46) that separates a forebody assembly (48) from a visual augmenter (44). The target (42) also includes a vented inflator (56) positioned at the forward end of the visual augmenter (44). The vented inflator (56) maintains the front end of the visual augmenter (44) open during towing. The visual augmenter (44) is generally cylindrical in shape with an open aft end and an adjustment device for varying the size of the aft opening. In addition, the visual body is comprised of a mesh netting (54) which preferably includes a plurality of interconnected strands (94) joined together to form a plurality of diamond shaped openings. The interconnected strands are each formed of a plurality of knitted threads and the strands are preferably joined together by knitting some or all of threads of one strand with some or all of the threads of an interconnecting strand.
Description
w~`fU/l2'f'f~ l'CT/US'`f0/0224l ~E~I~L GUNNE~ TARGET
B~CKGROUND OF THE INVENTION
rI~I,l) ()I Tll~ INV~NTION
The Eield of tllis invention lies w]thin the target and gunnery art. In particular, it lies within the specific fielc3 oE aerial targets that are towed behind an aircraf~.
DESCRIPTION OF T~IE RELAT~D ~Rl`
To improve the shootir.g and pursuit skil]s of aircraft pilots, various types of targets have been developed which are towed behind a towing aircraft.
Some of the earlier target constructions included elongated fabric panels or banners such as those disclosed in U.S. r~atent Nos. 2,731,046 and 2,807,Z87.
mhese targets included woven panels attached to a bridle assembly which, in turn, was attached to a long cable secured to a towing aircraft. ~lternate prior art forms of tow targets include those f ound in U.S. Patents Nos.
B~CKGROUND OF THE INVENTION
rI~I,l) ()I Tll~ INV~NTION
The Eield of tllis invention lies w]thin the target and gunnery art. In particular, it lies within the specific fielc3 oE aerial targets that are towed behind an aircraf~.
DESCRIPTION OF T~IE RELAT~D ~Rl`
To improve the shootir.g and pursuit skil]s of aircraft pilots, various types of targets have been developed which are towed behind a towing aircraft.
Some of the earlier target constructions included elongated fabric panels or banners such as those disclosed in U.S. r~atent Nos. 2,731,046 and 2,807,Z87.
mhese targets included woven panels attached to a bridle assembly which, in turn, was attached to a long cable secured to a towing aircraft. ~lternate prior art forms of tow targets include those f ound in U.S. Patents Nos.
2,342,651 and 3,000,634 which Eeat~lre one or more cylindrical sleeves being dra~3ged behind a tow aircraft.
Such targets have proven to be susceptlble to flagging and oscillation when dragged at high speeds.
U.S. Patent No. 4,205,848 discloses a banner proposed for use as an aerial gunnery target which includes a plurality of single strands extendingbetween forward and aft frame structures. This type of prior art target is described as avoiding the prior art problems of flagging and oscillatiny at high speeds due .
~U~YYO 2031521 I'C~/US90~0~4l to the elimination of transmitted forces between the individual strands e~tendi-ng along t~l^e length of the target.
Nonetheless, single strands also tend to whip and flag and snap in a manne~ similar to a whip cracking.
This whipping action tends to break the ends of the strands thus shortening tlle length of the augmenter.
Also, the use of individua1ized strands creates a problem of target survivability after epeated hits by the pursuing plane. Once the individ-ualized strands are hit they tend to freely flow about thus degrading the visual acuity of the target and i-ts performance.
Moreover, the positioning of the radar or scoring device close to the forward end of the target makes the device susceptible to destruction due to hits by the pursuing aircraft.
The various visual augmenters such as the banners, sleeves, and interconnected strands discussed above, have also presented tlie problem of environmental impact. For those visual augmenters which are released before landing of the to~^ting aircraft, there lies the possibility of the visual augmenter dropping into a body of water. This is especially true for the lighter banners which are more apt to be influenced by ~tind currents. The visual augmenters which fall into a body of water and are formed of relatively buoyant material such as polypropelene preser,t a problem to fishermen and the like in that the visual augmenters tend to tangle up in the netting used by fish-ermen and the propellers of w~/l2~6 l'C1/US9l~/0224l both commercial and recreation boats. Prior art attempts to solve this problem have included the positioning of weights on the forward end of the vi!;ual augmenter. Ilowever, even with the weights attached to the forward end of tl1e visual augmenter, portions of the visual augmenter tend to float upwardly towards the surface of t:h(' water theret-y causing even n greater hazard due to difficulty in spotting ti1e augmenters.
In addition, the visual augmenters of the prior art were pronc to be c1ifficult to visually detect due to a lack of visual acuity. This problem in visual detection being especially true for the individual strand configuration of the prior art as often the individual strands bellow outwardly decreasing contrast between the augmenter and the environmental background.
sur1M~Ry O~ TIIE INV~NTION
The presen~ invention, among other things, presents a solution to the a-forementioned problems associated with the prior art. In so doing, the present invention provides for the visual augmenter to be spaced well away from the forebody assembly carrying the radar or scoring device. To achieve this spacing, an extension device is utilized wl1ich has a front end attached to the rear end of a forebody assembly and a rear end attached to the visual augmenter. Hence, the extension device places the forebody assembly in a position which is less likely to be subjected to hits by pursuing aircraft. The extension device inc]udes one or ~ V YU/ I L~ CT /US90/0224l 2031~21- -.
more riser lines extending either from a frame or swivel connection attached to the forebody assembly. A
plurality of suspension lines extend from the end of each of the riser lines. The suspension lines extend outwardly away from the riser lines and are attached to a vented inflator which is attached to the forefront of the visual augmenter.
In the prior art system~ refèrred to, the visua]
augmenter was connected to a frame structure which gave the front, open end of thè visual augmenter the desired shape. This feature of using the frame structure attached to the forebody is not available when utilizing the present invention's flexible extension device which extends far from the frame. In other words, without a frame structure connected directly to the forwar~ end of the visual augmenter, there exists the possibility of the visual augmenter losing its shape at the forward end.
The vented inflator of the present invention avoids this problem by creating the aerodynamic forces necessary to keep the forward end of a cylindrical type visual augmenter open and in an inflated condition. The vented inflator includes a forward hoop and a rearward hoop joined together by a plurality of flexible panels connected between the forward and rearward hoops. The panels are spaced from one another along the periphery of each of the hoops so as -to create air vents between adjacent panels. The panels are also preferably connected to the hoops in a manner which prevents W~/12~96 rcT/us90/n224l 203i521 slippage of the panels along the ho~p. Also, the forward hoop is larger than the rearward hoop such that when the forward ancl rearward hoops are tensioned the panels form a frusto conica1 rim at the forward end of the visual augmenter. The vented inflator thus acts to maintain the forward end of the visual augmenter in an open position.
The visual augmel1t~r is generally cylindrical with an open front end and an open aft end which includes an adjusting dcvice that enables the size of the aft opening to be adjusted. This adjustment feature allows for manipulation of the drag created by the visual augmenter. For situations in which the visual augmenter is to be towed at high speeds, it is preferable that the adjusting device create a large opening at the aft end of the visual augmenter. If lower speeds are anticipated then the adjustment device is preferably manipulated to c-eate less of an opening at the aft end.
The visual augmenter is formed of mesh netting that is comprised of a plurality of strands which intersect one another to form a plurality of longitudinally extending diamond sha~ed openings. The strands are comprised of knitted threads and at the point of intersection of each strand some or all of the knitted threads (forming each strand) are knitted together so as to create the diamond shaped mesh netting. The arrangement of the inter-connected strands forming the mesh netting tends ~o reduce the drag of the ~ ~ YU/ I L~ C1 /US90/0224l 6 -- ~
~ visual augmenter. This reduced dr~g is due in part to the compression of tl1e interconnecting strands caused by the wind forces acti,ng on the visual augmenter. The mesh netting also tends to improve visual acuity by maintaining a compacted condition rather,than a bellowing configuration as exp,erienced in the prior art.
The mesh netting also increases the useful life of the visual augmenter even after re,peated hits. In the event that a hit tends to puncture a hole or sever a strand in the mesh netting there is no adverse affect on the netting which surrounds the point of impact and holds the device together. The visual augmenter of the present invention is also not as susc~ptible to flo~ting when material such as nylon is used as the threads for knitting the individual strands that are loined together to form the mesh nettlng. The mesh netting also tends to become entangled along its entire length with the various elements lying on ,the underwater surface. The use of lead weights further ensures that the visual augmenter will not easily drift with the wind currents and will remain.on the bottom of a-body of water into which the visual augmenter drops.
One embodiment of the invention has, by way of wind tunnel tests, proven particularly suited for aircraft which are capable of travellin~ at speeds between 240-500 KNTS during a dragging run. In this embodiment, the vented inflator includes forward and rearward connection means that, when in opération, assume a circular configuration. The forward connection ..~,u,I'Y~ I'Cl`/US90/02241 - 2031~21 -- 7 -- .
~ means features a first webbing member circular in shape and preferably itl the Lorm of.a strap made of nylon.
The forward connection means can .also include a second webbing member also pre~erabJy in the form of a strap made of nylon.
The rearward connection means features a nylon strap having a circular config~lration which is of a lesser diameter than that of the first a~d second webbing members.
A plurality of attachment memb`ers extend longitudinally and in spaced relationship between the forward and rearward connectlon means. One end of the attachment members is attached to the nylon strap forming the rearward connection means. 'rhe attachment members include a body section which is attached to the forward connection means as well as a second end which is also attached to the conllected means such that a loop is formed which extends out away from both said forward and rearward connection mears.
Because the rearward connection.means is of a lesser diameter than the forward connection means, the attachment members are at an incline as they extend between the forward and rearward ccnnectiGn means. In addition, the securement of the end of t.he attachment members and the rearward connectlon means is such that the strap member of the rea~ward.connection means is inclined so as to have a planar surface cor.fronting the air rushing into the vented.inflator.
2 0 3 1 5 2 1 l'~/U~9(~t(l224l A visual augmenter, which is preferably the same as the mesh netting previously described, is sandwiched hetween the first and second webbing members. In addition, the attacl~ er1t members ar~ arranged to have a first portion sandwiched between the Elrst and second webbinq members, a second portion which forms the aforementioned loop and a thir-d portion attached to the underside of the second web~ing member. The two webbing members, the mesh netting and the first and third portion of the attachrnent members are joined together such as by way oE a stitching process.
A bead, which can be a circular nylon rope, is positioned forwardly tG one-side of the first and second webbing members and attached to the mesh netting such as by a thread looping through the mesh netting and around the bead.
A plurality of suspension lines include loops which extend through the looped second po~tion of the attachment members. Tl1e suspension members can be made to converge to a common point for ease in interconnection with a dragging line or tow cable.
While in operation, the in rushing air acts to inflate the vented inflator and also the forward end of the visual augmenter wher~in the entire visual augmenter can then be inflated as well. The incline of the attachment members and rearwar~ connection means assist in ensuring the visual augmenter is inflated and maintained inflated. The visual augmenter is also, however, designed to keep drag to a mlnimum and the air U/12~ . 2 0 3 1 ~ 2 1 1'CT/US90/02241 - '3 -, vents formed between the attachment members allows for use of tlle target with hi,gher speed aircraft without early degradation of tl-e target. Tlius, the target can be used for repeated and extended runs which can reduce substantially the cost.of target practice and allow for prolonged pursuit.
~RI~F DFSCRI~TION C~ TllE DRAWINGS
The present invention will be more fully understood from th~ detailed description given hereinbelow and the accompanyinc3 drawings which are given by way of illustration only, and thus are not limitative of the present invention, and wherein:
FIG. 1 is a side v].ew of a prior art aerial gunnery target being towed by,a towing aircraft;
FIG. 2 is a side view of an embodiment of the present invention being towed by a towi.ng aircraft;
FIG. 3 is a side view of a prior art aerial gunnery target;
FIG. 4 is a side view of an embodiment of the present invention; ..
FIG. 5 is a perspective, partially cut-away view of the embodiment showri in Fig. 4;
W~/12~96 2 0~ 1521 1'ClJUS90/02241 FIG. 5A and 5~ are partially cut-away views of the vented inflator shown in Fig. 5;
FIG. G is a close-up of the mesh netting forming the visual augmenter;
FIG. 7 is a planar view of one of the panels forming the vented inflator sh-own in Figs. 5A and 5B;
FIG. 7B shows a cross-sectional side view of a panel and the manner in which the panel is connected to the hoops.
FIG. 7C shows a cross-sectional cut-away view of material forming the vented inflator panels.
FIG. 8 is a graph which illustrates a calculated comparison of the drag experieneed by an increased length visual augmenter wit11 the drag of the present invention;
FIG. 9 shows an inflator panel's normal force and drag with respect to velocity;
FIG. 10 shows the additional calculated drag increment resulting from the addition of a vented inflator.
WO90/12996 rCT/US90/0224l 203iS2~
FIG. 11 shows a force diagram for the vented inflator panels wl1ile in a state of tension;.
I'IGS. 1~-12~ show a cu~-away view of the riser and suspension lines featured in Fig. 5;
FIG. 13 shows an alternate embodiment of the present invention whlch utilizes a swivel connection between the forebody assembly and the riser lines;
FIG. 14 shows another embodiment of the present invention which has a swive] connecti~n and a dracT line connecting the forebody assembiy to the riser lines;
FIG. 15 shows the visual augmenter in a non-deployed state;
FIG. 16 shows a close-~p view of the frame assembly positioned behin(3 the forebody assembly; and FIGS. 17A and 17B show the aft end of the visual augmenter cut-away from the remainder of the visual augmenter as well as the adjusting~devlce positioned at the aft end.
FIG. 18 shows a side view of an alternate embodiment of the present invention;
- ~Y~J ~U~ J~rcr/usso/0224l 2031~21 FIG. 19 sl1ows a front v~ew of that which is shown in FIG~ 18; ..
I'IG. 20 shows a cll~awc~y view Or the interior of the visual augmenter shown in rIG. 18;
5FIG. 21~ shows a crocs-sectional and cutaway view of the forward end of that whicl1 is shown in FI~. 18;
FIG. 21B shows in greater detail that which is shown in FIG. 21A;
FIG. 22~ shows in planar view the forwardmost end of the suspension line a~sembly shown in I'IG, 18;
FIG., 22B shows the rearward, looped end of one of suspension ].ines shown in EIG. 22A;
FIG. 23A shows.in side view tha~ which is shown in FIG. 22A; and -15FIG. 23B shows a side view of that which is shown in FIG. 22B.
DET/~ILED DESCRIPTION OF TIIE PRLFERRED EMBODIMENTS
Fig. 1 shows a prior art aeri.al gunnery target 22being towed by towing aircraft 24. Aerial gunnery t:arget 22 includes visual augmenter 2~ formed of a plurality of individual strands 28 which are connected W~/129~6 rCT/US90/0224l ~_ - 13 -to the branclles of frame 30.. ~ plurality of the individual strands are arrarlc3ed in series along each of the branche.~ ~r ~ ralrl~ ~() alld .e~l-end rearwardly to a point of connectio,n made possible by cap 32. Radar detecti.on device 34 is posi.ti.oned at the center of fràme 30 anc3 create.s radar zone R. A pursuing aircraft (not shown) pursues the usually brightly colored visual augmenter 22 and attempts to shoot within zone R while preferably avoidlng direct hi.ts to vi,sual augmenter 22 and the other components of visual augmenter 2Z. Scorinc3 ~s achieved electronically by determining the position and number of shots passing through the radar zone R. Ra,dar clevice 34 is attached at its forward end to tow line 36 which is attached to reeling mechclnislll 3~. Tow line 36 usually extends to about 2,000 feet behind.the towing aircraft. During take-off, aerial gunnery target 22 is stored in canister 40 and at some poi.nt during ~liglit canister 40 is opened and aerial gunnery ~arget 22 is deployed.
Fig. 2 shows a preferred embodiment of the present invention which includes aerial gunnery target 42 comprising a visual auglnenter'44, vented inflator 56, extension device 46 and forebody assembly 48. Visual augmenter 44 is preferably cylindrical in shape having an open forward end 50 and a com~letel-y open or partially open aft end 52. ~ length of about 16 feet and an external diameter of 30 inc,hes has proven satisfactory for the purposes of this invention. Visual W~/12996 I'CT/US90/n224l . ~
augmenter 44 is preferably formed of meshed netting 54, the details oL whicll are-discussed hereafter.
~ t the forefront Gf v'isua] augmenter 44 is connected vented i,nflator 56 which i~cludes a plurality of spaced fleY~ible panels 58 atta.ched between forward hoop 62 and aEt hoop 60. ~uspension lines 64 are attached at one end to forward-hoop 6.2 and at their other end to riser lines 66. S,uspension lines 64 preferably are in sets of four that diverge outwardly from fixation point 68 which coincides with the rearward end of each of the riser lines 66. The rearwardmost ends of suspension lines 54 are spaced radially around forward hoop 62 and in between panels 58. The connection of the suspension'lines 64 to hoop 62 is preferably SUCIl that'suspension'lines 64 retain their position without sliding along hoop 62. The forward end of each of riser lines 66 àre connected to the extremities of bran.ches 70 forming part of frame 72.
Shaft 74 is attached at the locus of fram'e 72 and to the rear end of forebody assembly 4~. For,added stability, bracing members 76 extend between branches 70 and the rear end of forebody assembly ~8.
Forebody assembly 48 includes tow line connector 78 to which tow line 80 connects. The opposite end of tow line 80 is attached to reeling device 82 positioned either on the wing or the fuselage of towing aircraft 24.
~ ig. 3 sllows another prior art aerial gunnery target havi.ng visual augmenter 84 comprised of WO ~U/12996 21131521 rCl'/US90/0224l individual strands 86 similar to those found in Fig. 1.
Forebody assembly 8~3 includes frame 90 and braces 92 which are in direct contact with the forward end of visual augmenter ~4. ~rame 90 acts~to maintain the forward end of visual augmenter 84 in an open position.
Figs. 4 and 5 further illustrate the visual augmenter of the present invention shown ~eing towed in Fig. 2. Forebody assembly 48 includes radar capability which allows for radar zone R2 (partially shown) to be set up for scoring purposes.
Visual augrnenter 44 includes mesh netting M, only a portion of which is shown ir. detail for draftman's convenience. Fig. 6 shows in g'reater detail the arrangement of mesh netting M. Mesh netting M is formed of a plurality of interconnecting strands 94. Each of the strands 94 are formed of a p]ura]ity of knitted threads preferably comp'rised of nylon although other materials such as" hut not limited to, cotton, polypropylene, polyethylene, or rayon might also be relied upon. ~t the points of lntersection 96 of pairs of strands 94, the individua] strands 94 are connected together by way of a knitting process which knits certain of the threads makiny up one of the two intersecting strands 94 with certain threads of the other interconnected strand g4. The lndividual threads which are knitted to~et:her tG forrn strands 94 are preferably made from 1~90 denier nylon thread. Various other ways of joining strands 94 together are also contemplated. I''or example, strands 94 can be joined ~ /12~ 20 31 S 21 rcT/us90/n224l , ~
together by knotting one strand to the other at their point of intersection. '~ knitted connection is, however, more preferable as it piaces less stress on the individual threads.
Strands 94 forming mesh netting M intersect one another at ang],e which is prefera'bly about 30O so as to create a plurality of diamond shaped openings 98.
The longitudinal apex-to-ape~ length,L of each diamond is preferably within a range oI; about 1.22 to 1.28 inches or about 1-1/4 inches when mesh netting M is in a collapsed state (i.e., when length X and length Y are essentially planar). In addition,^the lateral apex-to-apex length ~ of each diamond when mesh netting M is in an untensioned state is preferab]y within a range of about .320 to .340 of an inch and more preferably about 1/3 of an inch. Nylot1 dia;nond mesh netting suitable for the purposes of ~he presen- invention is a product of Blue Mountain Industries located in Blue Mountain, Alabama. The netting sold by Blue Mountain Industries is referred to as "1-1/4 inch strength No. 189 knotless nylon netting".
The use of a plurality of-knitted threads to form the individual strands and the joining of the strands by a knitting process to form mesh netting M, also provides an advantage with respect to reducing drag. ~ir flowing along the length of the visual augmenter causes the augmenter to assume a tensioned or st,retched state.
While in a tensioned state the individual threads of strands 94 compress together, thus decreasing the W~9U/12996 2 0 31 5 21 1'CT/US90/~2241 - surface area in contact with the on ~ushing air stream.
In addition, tlle arranyement o~ the interconnected strands of mesh netting M, with the diamond shaped openings, leads to one strand drawing an adjacent strand both rearwardly and closer to itself. This arrangement tends to compress the entire body of augmenter 44 inwardly thereby lesse1lir,g the degree of drag caused by the visual augmenter. Further1nore, the angular orientat1on of the rearwardly extendiny strands, wit11 respect to the on rushing air stream, is such that as the augmenter stretches further rearwardly at increased speeds the individual strands 94 tend to assume a position more and more in line with the direction of the on rushing air. This featur~ enables the augmenter to inherently adjust the degre(~ of drag with increases in tow speed. Direction arrow 100 illustrates the direction of the air as it passes along the length of visual augmenter ~4.
Fig. 5 shows vented inf]ator 56 in an inflated condition. In this condition, vented inLlator 56 provides the necessary tension in hoops 60, 62 to form an inlet for a highly porous visual body such as visual body 45 formed of mesh netting M. Vented inflator 56 also performs the function bf obtaining and maintaining a cylindrical shape in the visual augmen~er by utilizing the local airstream as the energy so~rce.
As more fully illustrated in Figs. 5A and 5B, vented inflator 56 includes a number of p~nels 58 attached to forward hoop 62 and aft hoop 60. Hoops 60 wo ~ . r~/ussu/02241 and 62 are preferably formed of.a flexible cable comprised of a materia] such as nylon. In a preferred embodiment the cable is ,made up of a plurality of braided nylon ~it)ers wllicl1 when comblned provide a cable-having a cross-sectional diameter be~ween about 3,/16 of an inch to 1/4 of an inch. A diameter for hoops 60 and 62 which is suitable for t}-e purpose of the invention is about 32.6+.5 and 30.0+.5 inches, respectively. E~oops 60, 62 are also preferably formed in circular or ring-like fashion. The diameter of forw,ard hoop 62 is larger than the diameter of aft hoop 60 bv an amount which causes panels 58 to assume'an angle of attack that preferably falls within a range of a~out 12 to 18 degrees and more preferably is approY~imately 15 relative to the direc~ion of the local airflow. various other angles woul~ also be possible depending on the variables involved such as antlcipated towing speeds, hoop dimensions, etc. In achievinq a 15 angle of attack, forward hoop 62 would preferably have a diameter which is larger than that of aft hoop 60 by a ratio of about 1.087 to 1Ø
The positioning of panels, 58 at an angle of attack of about 15 (see Fig. 115 provides sufficient hoop tension (brought about by aerodynamic forces acting on the panels) to keep the forward end of a cylindrical visual augmenter open and thus enable the visual augmenter to remain in an inflated condition.
Furthermore, a 15 angle of attacr~ provides sufficient aerodynamic loading to provid~ the required hoop tension W~/12996 2 0 3 1 5 2 1 1'CT/US91~/02241 - 19 _ while at the same time minimi7ir,g the drag or force in the actual direction.of the ~isual augmenter.
In a preferr~d ~mbodiment vented inflator 56 includes 16 trunca~d triangular shaped panels 58.
Panels 58 are uniformly positioned with space between each panel and attac11ed to hoops 60, G2 to provide a porosity ratio ~panel area/t:otal ar.ea) of about .5 for the inflator and more preferabi.y about 0.484.
Fig. 7 shows th~ flnished flat pattern for a preferred embodimenL, as well a.s the spacial location relative to 1/16 of the area of ~ented inflator 56, which is equivalent to a 22.5 degree segment of the inflator. Each truncated panel 58 has its forward edge looped over and sewn or fastened to form a passageway for accepting forward hoop cable 62. ~fter cable 62 has been inserted through the loops of panels 58, each panel is positioned with an equal separation space which, with a 32.6 inch diameter .~orward hoop, proves to be about 2.4 inches. The ends of the cable for hoop 62 are then securely fastened together to form the final configuration of hoop 62. Similarly, the cable for aft hoop 60 is inserted through lo~ps formed in the aft end of each panel wit11 equal separation spaces of about 3.9 inches and the ends of the cable. forming aft hoop 60 are joined to form the final configuration of aft hoop 60. ~
Fig. 7B illustrates the manner in which the forward and rearward ends of panels 59 are looped about forward and aft hoops 60,62. ~ .bo~-stitching or the W~ ~U/12~J~ /US90/02241 like is provided which creates ~ snug connection between hoops 60, G2 and the looped portlons of panels 58. In this way, panels 58 do not shift in position with respect to hoops 60, G2. I'urther contem^plated methods for ensuring that panels 58 remain i~-fixed position with respect to ;lOOpS 60, 62 include having threads pass through the braided cable as well as the ends of panel 58 when the loops are formed. ~lternatively, adhesives could be used to prevent slipp~ge of panels 58. The rearward edge 104 of-panel 58 is preferably about half the lengtl- of forward edge 10~ or about two inches. The distance between forward edge 102 and rearward edge 104 as shown in Eig. 7 is preferably about 5 inches.
Various other dimetlsions are also possible depending upon factors such as, for example, the anticipated speeds of towing, the si'ze of the visual augmenter and the materials relied upon.
Panels 58 are contempla~ed as being made of a high strength fiber material. A vinyl nylon cloth referred to as "U.S. ~overnment Part No. 13ZZ7E0131:MIL-C-20696 Type II, Class 1" having a breaking strength equal to about 225 lb for one inch wide strip is contemplated for use in the present invention. Eig. 7C
shows in cross-section a preferred embodiment of panel 58 wherein two vinyl layers Z00 are layered about a cloth (or fiber) weave or mesh ZOZ. This arrangement further ensures that panels'S8 are of sufficient strength to handle the forces that develop during high speed runs. An alternative approach contemplated is to W~90/l~996 ~ I'Cr/U~9~/0224l apply a viny]. coating on both sides-Aof a layer of mesh or cloth.
Vented inflator 56 is attached to suspension lines 64 as best illustrated in ~`'i.g. 7. Suspension lines 64 have their ends iooped ~bout forward hoop 62 and box stitched to snug].y fit about hoop 62 so as not to slide thereon. Additionally, various other means such as adhesives can be used~to ensure no slippage of suspension lines 64 with respect t~ hooF 62. Visual augmenter 44 has at its forward edge a strip of material 204 which is connected to the individual strands forming the mesh pattern M. This strip of material is joined to aft cable 60 by lacing 206 which e~tends through the diamond mesh netting and around aft ca~le 60 and stri.p 204 in the open areas between adjacent panels 58.
Lacing 206 is preferably formed of a wa~ed coated nylon material with the wax avoiding undue slippage while wrapping and knotting lacing 206 about both strip 204 and aft cable 60.
Fig. 11 provides a force dlagram for panels 58 while in a tension state due to drag created by visual augmenter 44 and the tension placed on_suspension lines 64. Fig. 11 also illustrates a 15 degree anqle of attack for panel 58 shown in cross section. As can be seen in Fig. 11, panel 58 !-as its forward and rearward ends looped about hoops 60, 62. The forward and aft hoops 60, 62 are in tension resulting from the normal force created by the aerodynamic loading of panels 58.
As a result of the largeF diameter of forward hoop 62, WO 9U/12996 I'CI /US91)/02241 2031~2^1 in relation to the diametex of aft hcop 60, panels 58 are positioned within an approY~imate angle of attack of 15O relative to incoming air. The aerodynamic norma]
force of the panel can be broken down into two orthogonal components; the radial component (i.e. hoop tension) and the axial or drag~ component. The longitudinal tension required to maintain the preferred 5 inch separation distance between forward and aft hoops 60, 62 is provided by Ihe opposi:ng s~ispension line 64 tension acting forward and the visual augmenter 44 drag acting to the rear.
The spacial arrange~ent for panels 58 is configured to provide nearly equal size openings between each panel 58. With this arrangement, separation and the resulting turbulence of t'ne local air stream over and around the panels is minimized. The spacial arrangement of the openings betwéen the panels also provides a means for tailoring or optimizing the desired hoop tension over a wide varlety of alrspeed operations.
The spacial arrangement of the panels 58 could vary in accordance with the specific requirements desired of the visual augmenter. ~ preferred embodiment has sixteen panels 58 spaced equally about forward and aft hoops 60,62.
Tow harness 106 (shown in Figs. 12~ and 12B) is comprised of a plurali'y of riser lines 66 and suspension lines 64. In the embodiment shown in Fig. 2, four riser lines 6G are attached to frame structure at 72. Riser lines 66 are preferably about 5 feet in ~V~ ' l'CT/US90/0224l ~ .
length and made from 1.75 inch wide U.S. Government nylon webbing designated ~ W-4088 Type VIII, Class 2 with a described breaking strength of 3500 lbs. I'o fixation point 68 (Figs. 12A and 1?B), is attached four suspension lines 64 each preferably made from 1/2 inch commercial grade nylon webbing having a described breaking strengtl1 of 500 'lb. The four suspension lines 64, are attached to one-of the I'our riser lines 66 at fixation point 68. This attaehm~nt is shown in Fig. 12 and Fig. 1 2B to be made by use of a box stitch.
Similarly, suspensior- lines 64 are connected to forward hoop 62 by wrapping the end o~ suspension line 64 about hoop 62 and using a box -stitch to keep it in place. The forward end of riser line 66 also includes loop section 108 which is connected to cable 116 (Fig. 16) that attaches to one of the bra'nches of frame 72.
Fig. 8, which is based on calculations, depicts graphically the reduced drag made possible by the present invention. In Fig. 8 line 110 shows the increase in drag whicl1 would occur if a prior art visual augmenter such as that shown'ln ~ig. 3 was increased an additional 10 feet. By utillzat~ol1 of suspension lines 64 and riser lines 66 each of about 5 feet in length, the entire length of the visual augmenter can be increased by about 10 feet. As set forth previously, the reliance on the combination of mesh netting M, vented inflator 56 and t~w hàrness 106 allows for extension of the aerial qunnerv target of the present invention while maintaining a re~uced drag value. The ~uYU~ CT/US9U/0224l aerial gunnery target of the present invention also enhances visual acuity o~ the target. The enhancement in visual acuity is macle posslbl~ by.the added lengtll and, more importantly, the ability of the augmenter 44 to maintain a relatively uniform and condensed body which contrasts sharply agai.nst the environmental background. l`lle vented i.nflator 5.6 assists in inflating visual augmenter 44 so as to maintain a g~nerally cylindrical shape. Moreover, the passage of incoming air through vente(l inLlator 56 and- through the length of visual augmenter 44 helps prevent o~cillation caused by external forces acting on the vlsual augmenter.
Fig. 9 whi.cll is based on calculations depicts, graphically, the normal and drag`forces which would be expected to develop in panels 58 in relat~on to the velocity of the towed visual augmenter. The limit value M shown in Fig. 9 is represented as .95 Mach or 448 KCAS
[knots calibrated ai.r speed~. Fi.g. 9 represents the normal and drag forces acting on panels 56 when at an attack angle of 15O. The materlal forming panels 56 as well as the manner of attachment to hoops 60, 62 must be capable of withstanding the forces shown in Fig. 9.
Fig. 10 shows tlle calculated drag which can be e~pected due to the addition of vented inflator 56 to visual auqmenter 4~. Fig. 1~ also.revea~.s that th~ dr.~-~developed by including the vented inflator remains relatively low even up in.the higher maxi.mum speed regions.
~ /l2~ ' 2 0 315 21 rCT/US90/0224l - 2'. -Returning to ~ig. 2, reeling mact1ine 82 isattached to the underside of one of the towing aircraft's wings. The r~eLing'machine includes a releasable attachment device 112~that is capable of S releasing forebody assembly 48 upon command of the pilot. In normal operation' visual augmenter 44 and towing harness 1~6 are contained within deployment bag 114 (Fig. 15) prior to deployment. Whlle in flight above the predeterrnined target area, cutter mechanism 116 (Fig. 15) is activated (e;g. by an electronic signal) so as to cut the deployment line'118. Once deployment line is cut, branches 70 begin to extend outwardly and dep]oyment bag 114 is-drawn from its covering position. ~fte'r hag 114 is drawn off by drag forces, the drag forces further act to deploy visual augmenter 44. Thereafter, forebody 48 is detached from attachment device 112 and reeled outwardly a'long tow line 80 (Fig. 2) until the visual augmenter 44 is the desired length awa~ from th~ towing aircraft (e.g. ~,000 feet).
In operating an aerial gunnery target such as that of the present irivention it is'necessary to exclude the use of radar reflective type material within the scoring pattern envelope, i.e., visual augmenter 44 and the surrounding area within-radar zone R2. If radar reflective material is used in the; visual augmenter, vented inflator or in the towing harness it is highly probable that the unsteady highly cyclic vibrational type motion of the augmenter w ll-result in false W~90/12996 ~'' rCT/US9U/02241 - 2( -scoring outputs of the radar scorlng system. The radar return of this motion-can easily be misinterpreted by the scoring system as munition rounds'passing through the scoring envelope., ~ccordingly, the present invention relies on a towing harness and visual augmenter formed of material which lS not radar reflective. The foregoing discussion indicates that various materials such as~nylon have proven suitable for the purposes of the present invention.
Referring again to Flg. 15, it is apparent that storage volume constraints alsG influence the design concept of a visual augmenter inflator. The flexible panel/hoop cable design of the vented inflator 56 provides a non-rigid highly fle~ible structure that can be folded or packed into virtually any shaped storage container or storage envelope so as to minimize storage volume requirernents. The fleY.ible riser and suspension lines are also easily folded up within storage container 114.
Following the desire-] target practice, the gunnery target is reeled -in until forebody 48 becomes reattached to attachment device 11 ? Visual augmenter 44 and towing harness 106 are then released and allowed to drop to the ground or body of water below.
Fig. 16 illustrates,the manner in which towing harness 106 is disconnected from frame assembly 72 which is attached to shaft 74. To release tow harness 106, shaft 74 is drawn inwardly into the rear end of forebody assembly 48. This inward rr,ovement of,shaft 74 causes W~/12~ 2 03152 1 l'CI/V~90/02241 branches 70 to collapse inwardly and in the rearward direction. Consequently, cable loops-116 and attached lead weights 118 are able to slide ou~t of notches formed in branches tO and becollle released as illustrated in S dashed lines in Fic~. 20. Vicu~] augmenters 44 are then picked up upon landing on the ground or, if target practice is to take place over a body of water, visual augmenters 44 fall below the surface of the water and tend to remain entirely in c~ntact witl1 the underwater bottom surface.
Figs. 17~ and 17B illustrate various sized openings at the aft end of visual augmenter 44. Air flowing through visua] augmenter 44 in the direction of line 118 passes through opening 120. Drag can be increased by decreasinQ the size of opening 120. Hence, for slow speeds where it is desired to increase the drag of visual augmenter 44 so as to maintain proper positioning, the aft end opening 120 can be decreased in size as shown in Fig. 17~. Va-iations in the size of aft opening 120 are made possib]e by adjustment device 122 which includes a nylon cord 126 (or the like) passing within a sleeve provided at the aft end of mesh netting M. Cord 126 is shown as having two free ends which pass through adjustmènt clip 128. By drawin<~ the free ends of cord 126 awày from adjustment clip 128, the aft end opening 120 is made smaller.
Figs. 13 and 14 show two alternate embodiments of the present invention. In Fig. 13, swivel connector 134 allows for visual augmenter 136~and e~tension device 138 ' w~ () l'CT/US~()/0224l ` 2031~21 - 2~ -~ '.
to freely rotate with respect to forebody assembly 48.
Other than the swivel connector hetween forebody assembly 48 anc'l e~tensiol1 device 138, all other features are similar ~o that of the visual augmenter illustrated in Fig. 2. Fig. 14 is essential~y the same as Fig.17 except for the addition of dra~ line 140 between forebody assembly 48 and swivel connector 134. In utilizing the embodiments of Figs. 13 and 14, detachment of visual augmenter 44 is made~s1mple in that all that is required is a release of the swlvel connector 134 or, alternatively, connection device 210 shown in Fig. 14.
As can be seen, the ad~it'ion of vented inflator at the forefront of,the visual augmenter provides a great deal of freedom in determining how the visual augmenter is to be attached to a forebody assembly or, alternatively, directly t~o the end of a tow cable. The vented inflator makes unnecessar~ the use of frame structures to maintain the front opening of a visual augmenter in an open state. Moreover, the vented inflator of the present invention allows for non-rigid and non-radar reflective material to provide the required opening at the front of a visual augmenter.
FIG. 18 shows a side,view of an--alternate embodiment of the present invention. In FIG. 18, aerial gunnery target 298 features suspension line assembly 301 with suspension lines ~99. Attached to the rearward end of suspension line assemb]y 301 is vented inflator 302 which includes hoop sh~ped forward connection means 303 and hoop shaped rearward connect,ion means 305 wo ~0/12996 rCr/l~S90/0224l 20315`21 longltudinally displaced from one another. A plurality of attachment members 304 e~ter-d between the forward and rearward conncctiol1 rncal1s.
l~IG. 19 shows the front view of aerial gunnery target 298 having suspension line assembly 301 with suspension lines 299 e.~tending~to a common connection point. At the forward portion of vented inflator 302 is bead 307. As shown, at:tachment members 304 incline inwardly to connect Witl1 rearward connection means 305 to form a plurality of alr vents 312.
FIG. 20 illustrates in gre~ter detail the forward end o2-- aerial gunnery targèt 298. Suspension line 299 includes loop 313 which is conr.ected to loop 314 (FIG.
21A) formed in the forward end of each of the attachment members 304. 13ead 307 i 9 shown to extend through loop 314 and includes threacl 308 which interconnects bead 307 with the visual augmenter represented by mesh netting M
by looping and lacing thread 308 about bead 307 and the mesh netting's edge. Webbing strip 306 is` shown to be positioned inside of mesh netting ~. and-- to the outside of a portion of attachment member 304.
FIGS. 21A and 21B show in greater detail the forward end of aerial gunnery target 298. As shown, attachment members 30~ e~tend at an incline from rearward connec'cion means 305. The end portion of attachment members 304 are connected to rearward connection means 305 by extending th~ er.d portion about both sides of rearward connection means 305 and stitching the combination together. Rearward connection WO ~()/l2$~6 2 0 315 21 l'Cr/US90/0224l - 3(~ -means 305 is posi'ioned at an incline to confront in rushing air and to assist in infiating the forward end of the gunnery target~.
The degree of incline is adjustable for intended 5 use with the preferred incline being 40 to 50 as represented by angle "y" in FIG. 211~. As also shown in FIG. 21a, the preLerred angle "s~" for the incline of attachment members 304 is 15 i:o 30.
As best shown in I~IG. 21B first we~bing member 310 is positioned externally of end po~-tion 316 of attachment members 304. The visual au~menter netting M
is positioned below end portion 316 while second webbing member 306 is positioned below mesh netting M. Body portion 318 of attachmenL members 304 are positioned directly below second webbing member 306 and the entire combination of body portion 318~ second webbing member 306, mesh netting M, end portion 316 and first webbing member 310 are joined together preferably by box stitching, adhesive or a combination thereof.
Z0 In a preferred embodiment, first webbing member 310, second webbing member 306, attachment members 304, rearward connection means 305, bead 307 and thread 308 are all formed of a nylon material. The preferred dimensions include first webbing member having a two-inch width; rearward connection means having a width of to 2 inches; second w-ebbing member having a width of3 inches; and attachment member having a width of 2 to 3 inches. Nylon thread 308 is preferably of 40 lb.
strength.
~v~u~ Y~ . I ~/US90/()224l - 31 _ FIG. 22A shows the-mar.ner in which lines 299 are brought together at their end. As shown wrap 318 is secured by a stitchin9 process o the ends of four suspension lines doubled over to.provide eight lines extending outwardly. The susp~nsion lines 299 are preferably formed of 3/16 diameter nylon rope (900 lbs).
FIG. 22B shows one of the suspension lines shown in FIG. 22A having a hraided rope loop 309.
FIG. 23~ shows a side view of that which is shown in ~IG. 22A. As sl1own the eight suspension lines are formed by doubling over four suspension lines and attaching web member 318 to hold the suspension lines together at a connection point. FIG. 23B shows a side view of the line shown in FIG. 23B.
~ lthouqh tlie preferred embodiments of the present invention have been describ~d Witll reference to the accompanying drawings many modifi.cati.ons and changes may be effected by those skilled in the art without departing from tl1e scope and spirlt of the invention as appended hereinafter.
Such targets have proven to be susceptlble to flagging and oscillation when dragged at high speeds.
U.S. Patent No. 4,205,848 discloses a banner proposed for use as an aerial gunnery target which includes a plurality of single strands extendingbetween forward and aft frame structures. This type of prior art target is described as avoiding the prior art problems of flagging and oscillatiny at high speeds due .
~U~YYO 2031521 I'C~/US90~0~4l to the elimination of transmitted forces between the individual strands e~tendi-ng along t~l^e length of the target.
Nonetheless, single strands also tend to whip and flag and snap in a manne~ similar to a whip cracking.
This whipping action tends to break the ends of the strands thus shortening tlle length of the augmenter.
Also, the use of individua1ized strands creates a problem of target survivability after epeated hits by the pursuing plane. Once the individ-ualized strands are hit they tend to freely flow about thus degrading the visual acuity of the target and i-ts performance.
Moreover, the positioning of the radar or scoring device close to the forward end of the target makes the device susceptible to destruction due to hits by the pursuing aircraft.
The various visual augmenters such as the banners, sleeves, and interconnected strands discussed above, have also presented tlie problem of environmental impact. For those visual augmenters which are released before landing of the to~^ting aircraft, there lies the possibility of the visual augmenter dropping into a body of water. This is especially true for the lighter banners which are more apt to be influenced by ~tind currents. The visual augmenters which fall into a body of water and are formed of relatively buoyant material such as polypropelene preser,t a problem to fishermen and the like in that the visual augmenters tend to tangle up in the netting used by fish-ermen and the propellers of w~/l2~6 l'C1/US9l~/0224l both commercial and recreation boats. Prior art attempts to solve this problem have included the positioning of weights on the forward end of the vi!;ual augmenter. Ilowever, even with the weights attached to the forward end of tl1e visual augmenter, portions of the visual augmenter tend to float upwardly towards the surface of t:h(' water theret-y causing even n greater hazard due to difficulty in spotting ti1e augmenters.
In addition, the visual augmenters of the prior art were pronc to be c1ifficult to visually detect due to a lack of visual acuity. This problem in visual detection being especially true for the individual strand configuration of the prior art as often the individual strands bellow outwardly decreasing contrast between the augmenter and the environmental background.
sur1M~Ry O~ TIIE INV~NTION
The presen~ invention, among other things, presents a solution to the a-forementioned problems associated with the prior art. In so doing, the present invention provides for the visual augmenter to be spaced well away from the forebody assembly carrying the radar or scoring device. To achieve this spacing, an extension device is utilized wl1ich has a front end attached to the rear end of a forebody assembly and a rear end attached to the visual augmenter. Hence, the extension device places the forebody assembly in a position which is less likely to be subjected to hits by pursuing aircraft. The extension device inc]udes one or ~ V YU/ I L~ CT /US90/0224l 2031~21- -.
more riser lines extending either from a frame or swivel connection attached to the forebody assembly. A
plurality of suspension lines extend from the end of each of the riser lines. The suspension lines extend outwardly away from the riser lines and are attached to a vented inflator which is attached to the forefront of the visual augmenter.
In the prior art system~ refèrred to, the visua]
augmenter was connected to a frame structure which gave the front, open end of thè visual augmenter the desired shape. This feature of using the frame structure attached to the forebody is not available when utilizing the present invention's flexible extension device which extends far from the frame. In other words, without a frame structure connected directly to the forwar~ end of the visual augmenter, there exists the possibility of the visual augmenter losing its shape at the forward end.
The vented inflator of the present invention avoids this problem by creating the aerodynamic forces necessary to keep the forward end of a cylindrical type visual augmenter open and in an inflated condition. The vented inflator includes a forward hoop and a rearward hoop joined together by a plurality of flexible panels connected between the forward and rearward hoops. The panels are spaced from one another along the periphery of each of the hoops so as -to create air vents between adjacent panels. The panels are also preferably connected to the hoops in a manner which prevents W~/12~96 rcT/us90/n224l 203i521 slippage of the panels along the ho~p. Also, the forward hoop is larger than the rearward hoop such that when the forward ancl rearward hoops are tensioned the panels form a frusto conica1 rim at the forward end of the visual augmenter. The vented inflator thus acts to maintain the forward end of the visual augmenter in an open position.
The visual augmel1t~r is generally cylindrical with an open front end and an open aft end which includes an adjusting dcvice that enables the size of the aft opening to be adjusted. This adjustment feature allows for manipulation of the drag created by the visual augmenter. For situations in which the visual augmenter is to be towed at high speeds, it is preferable that the adjusting device create a large opening at the aft end of the visual augmenter. If lower speeds are anticipated then the adjustment device is preferably manipulated to c-eate less of an opening at the aft end.
The visual augmenter is formed of mesh netting that is comprised of a plurality of strands which intersect one another to form a plurality of longitudinally extending diamond sha~ed openings. The strands are comprised of knitted threads and at the point of intersection of each strand some or all of the knitted threads (forming each strand) are knitted together so as to create the diamond shaped mesh netting. The arrangement of the inter-connected strands forming the mesh netting tends ~o reduce the drag of the ~ ~ YU/ I L~ C1 /US90/0224l 6 -- ~
~ visual augmenter. This reduced dr~g is due in part to the compression of tl1e interconnecting strands caused by the wind forces acti,ng on the visual augmenter. The mesh netting also tends to improve visual acuity by maintaining a compacted condition rather,than a bellowing configuration as exp,erienced in the prior art.
The mesh netting also increases the useful life of the visual augmenter even after re,peated hits. In the event that a hit tends to puncture a hole or sever a strand in the mesh netting there is no adverse affect on the netting which surrounds the point of impact and holds the device together. The visual augmenter of the present invention is also not as susc~ptible to flo~ting when material such as nylon is used as the threads for knitting the individual strands that are loined together to form the mesh nettlng. The mesh netting also tends to become entangled along its entire length with the various elements lying on ,the underwater surface. The use of lead weights further ensures that the visual augmenter will not easily drift with the wind currents and will remain.on the bottom of a-body of water into which the visual augmenter drops.
One embodiment of the invention has, by way of wind tunnel tests, proven particularly suited for aircraft which are capable of travellin~ at speeds between 240-500 KNTS during a dragging run. In this embodiment, the vented inflator includes forward and rearward connection means that, when in opération, assume a circular configuration. The forward connection ..~,u,I'Y~ I'Cl`/US90/02241 - 2031~21 -- 7 -- .
~ means features a first webbing member circular in shape and preferably itl the Lorm of.a strap made of nylon.
The forward connection means can .also include a second webbing member also pre~erabJy in the form of a strap made of nylon.
The rearward connection means features a nylon strap having a circular config~lration which is of a lesser diameter than that of the first a~d second webbing members.
A plurality of attachment memb`ers extend longitudinally and in spaced relationship between the forward and rearward connectlon means. One end of the attachment members is attached to the nylon strap forming the rearward connection means. 'rhe attachment members include a body section which is attached to the forward connection means as well as a second end which is also attached to the conllected means such that a loop is formed which extends out away from both said forward and rearward connection mears.
Because the rearward connection.means is of a lesser diameter than the forward connection means, the attachment members are at an incline as they extend between the forward and rearward ccnnectiGn means. In addition, the securement of the end of t.he attachment members and the rearward connectlon means is such that the strap member of the rea~ward.connection means is inclined so as to have a planar surface cor.fronting the air rushing into the vented.inflator.
2 0 3 1 5 2 1 l'~/U~9(~t(l224l A visual augmenter, which is preferably the same as the mesh netting previously described, is sandwiched hetween the first and second webbing members. In addition, the attacl~ er1t members ar~ arranged to have a first portion sandwiched between the Elrst and second webbinq members, a second portion which forms the aforementioned loop and a thir-d portion attached to the underside of the second web~ing member. The two webbing members, the mesh netting and the first and third portion of the attachrnent members are joined together such as by way oE a stitching process.
A bead, which can be a circular nylon rope, is positioned forwardly tG one-side of the first and second webbing members and attached to the mesh netting such as by a thread looping through the mesh netting and around the bead.
A plurality of suspension lines include loops which extend through the looped second po~tion of the attachment members. Tl1e suspension members can be made to converge to a common point for ease in interconnection with a dragging line or tow cable.
While in operation, the in rushing air acts to inflate the vented inflator and also the forward end of the visual augmenter wher~in the entire visual augmenter can then be inflated as well. The incline of the attachment members and rearwar~ connection means assist in ensuring the visual augmenter is inflated and maintained inflated. The visual augmenter is also, however, designed to keep drag to a mlnimum and the air U/12~ . 2 0 3 1 ~ 2 1 1'CT/US90/02241 - '3 -, vents formed between the attachment members allows for use of tlle target with hi,gher speed aircraft without early degradation of tl-e target. Tlius, the target can be used for repeated and extended runs which can reduce substantially the cost.of target practice and allow for prolonged pursuit.
~RI~F DFSCRI~TION C~ TllE DRAWINGS
The present invention will be more fully understood from th~ detailed description given hereinbelow and the accompanyinc3 drawings which are given by way of illustration only, and thus are not limitative of the present invention, and wherein:
FIG. 1 is a side v].ew of a prior art aerial gunnery target being towed by,a towing aircraft;
FIG. 2 is a side view of an embodiment of the present invention being towed by a towi.ng aircraft;
FIG. 3 is a side view of a prior art aerial gunnery target;
FIG. 4 is a side view of an embodiment of the present invention; ..
FIG. 5 is a perspective, partially cut-away view of the embodiment showri in Fig. 4;
W~/12~96 2 0~ 1521 1'ClJUS90/02241 FIG. 5A and 5~ are partially cut-away views of the vented inflator shown in Fig. 5;
FIG. G is a close-up of the mesh netting forming the visual augmenter;
FIG. 7 is a planar view of one of the panels forming the vented inflator sh-own in Figs. 5A and 5B;
FIG. 7B shows a cross-sectional side view of a panel and the manner in which the panel is connected to the hoops.
FIG. 7C shows a cross-sectional cut-away view of material forming the vented inflator panels.
FIG. 8 is a graph which illustrates a calculated comparison of the drag experieneed by an increased length visual augmenter wit11 the drag of the present invention;
FIG. 9 shows an inflator panel's normal force and drag with respect to velocity;
FIG. 10 shows the additional calculated drag increment resulting from the addition of a vented inflator.
WO90/12996 rCT/US90/0224l 203iS2~
FIG. 11 shows a force diagram for the vented inflator panels wl1ile in a state of tension;.
I'IGS. 1~-12~ show a cu~-away view of the riser and suspension lines featured in Fig. 5;
FIG. 13 shows an alternate embodiment of the present invention whlch utilizes a swivel connection between the forebody assembly and the riser lines;
FIG. 14 shows another embodiment of the present invention which has a swive] connecti~n and a dracT line connecting the forebody assembiy to the riser lines;
FIG. 15 shows the visual augmenter in a non-deployed state;
FIG. 16 shows a close-~p view of the frame assembly positioned behin(3 the forebody assembly; and FIGS. 17A and 17B show the aft end of the visual augmenter cut-away from the remainder of the visual augmenter as well as the adjusting~devlce positioned at the aft end.
FIG. 18 shows a side view of an alternate embodiment of the present invention;
- ~Y~J ~U~ J~rcr/usso/0224l 2031~21 FIG. 19 sl1ows a front v~ew of that which is shown in FIG~ 18; ..
I'IG. 20 shows a cll~awc~y view Or the interior of the visual augmenter shown in rIG. 18;
5FIG. 21~ shows a crocs-sectional and cutaway view of the forward end of that whicl1 is shown in FI~. 18;
FIG. 21B shows in greater detail that which is shown in FIG. 21A;
FIG. 22~ shows in planar view the forwardmost end of the suspension line a~sembly shown in I'IG, 18;
FIG., 22B shows the rearward, looped end of one of suspension ].ines shown in EIG. 22A;
FIG. 23A shows.in side view tha~ which is shown in FIG. 22A; and -15FIG. 23B shows a side view of that which is shown in FIG. 22B.
DET/~ILED DESCRIPTION OF TIIE PRLFERRED EMBODIMENTS
Fig. 1 shows a prior art aeri.al gunnery target 22being towed by towing aircraft 24. Aerial gunnery t:arget 22 includes visual augmenter 2~ formed of a plurality of individual strands 28 which are connected W~/129~6 rCT/US90/0224l ~_ - 13 -to the branclles of frame 30.. ~ plurality of the individual strands are arrarlc3ed in series along each of the branche.~ ~r ~ ralrl~ ~() alld .e~l-end rearwardly to a point of connectio,n made possible by cap 32. Radar detecti.on device 34 is posi.ti.oned at the center of fràme 30 anc3 create.s radar zone R. A pursuing aircraft (not shown) pursues the usually brightly colored visual augmenter 22 and attempts to shoot within zone R while preferably avoidlng direct hi.ts to vi,sual augmenter 22 and the other components of visual augmenter 2Z. Scorinc3 ~s achieved electronically by determining the position and number of shots passing through the radar zone R. Ra,dar clevice 34 is attached at its forward end to tow line 36 which is attached to reeling mechclnislll 3~. Tow line 36 usually extends to about 2,000 feet behind.the towing aircraft. During take-off, aerial gunnery target 22 is stored in canister 40 and at some poi.nt during ~liglit canister 40 is opened and aerial gunnery ~arget 22 is deployed.
Fig. 2 shows a preferred embodiment of the present invention which includes aerial gunnery target 42 comprising a visual auglnenter'44, vented inflator 56, extension device 46 and forebody assembly 48. Visual augmenter 44 is preferably cylindrical in shape having an open forward end 50 and a com~letel-y open or partially open aft end 52. ~ length of about 16 feet and an external diameter of 30 inc,hes has proven satisfactory for the purposes of this invention. Visual W~/12996 I'CT/US90/n224l . ~
augmenter 44 is preferably formed of meshed netting 54, the details oL whicll are-discussed hereafter.
~ t the forefront Gf v'isua] augmenter 44 is connected vented i,nflator 56 which i~cludes a plurality of spaced fleY~ible panels 58 atta.ched between forward hoop 62 and aEt hoop 60. ~uspension lines 64 are attached at one end to forward-hoop 6.2 and at their other end to riser lines 66. S,uspension lines 64 preferably are in sets of four that diverge outwardly from fixation point 68 which coincides with the rearward end of each of the riser lines 66. The rearwardmost ends of suspension lines 54 are spaced radially around forward hoop 62 and in between panels 58. The connection of the suspension'lines 64 to hoop 62 is preferably SUCIl that'suspension'lines 64 retain their position without sliding along hoop 62. The forward end of each of riser lines 66 àre connected to the extremities of bran.ches 70 forming part of frame 72.
Shaft 74 is attached at the locus of fram'e 72 and to the rear end of forebody assembly 4~. For,added stability, bracing members 76 extend between branches 70 and the rear end of forebody assembly ~8.
Forebody assembly 48 includes tow line connector 78 to which tow line 80 connects. The opposite end of tow line 80 is attached to reeling device 82 positioned either on the wing or the fuselage of towing aircraft 24.
~ ig. 3 sllows another prior art aerial gunnery target havi.ng visual augmenter 84 comprised of WO ~U/12996 21131521 rCl'/US90/0224l individual strands 86 similar to those found in Fig. 1.
Forebody assembly 8~3 includes frame 90 and braces 92 which are in direct contact with the forward end of visual augmenter ~4. ~rame 90 acts~to maintain the forward end of visual augmenter 84 in an open position.
Figs. 4 and 5 further illustrate the visual augmenter of the present invention shown ~eing towed in Fig. 2. Forebody assembly 48 includes radar capability which allows for radar zone R2 (partially shown) to be set up for scoring purposes.
Visual augrnenter 44 includes mesh netting M, only a portion of which is shown ir. detail for draftman's convenience. Fig. 6 shows in g'reater detail the arrangement of mesh netting M. Mesh netting M is formed of a plurality of interconnecting strands 94. Each of the strands 94 are formed of a p]ura]ity of knitted threads preferably comp'rised of nylon although other materials such as" hut not limited to, cotton, polypropylene, polyethylene, or rayon might also be relied upon. ~t the points of lntersection 96 of pairs of strands 94, the individua] strands 94 are connected together by way of a knitting process which knits certain of the threads makiny up one of the two intersecting strands 94 with certain threads of the other interconnected strand g4. The lndividual threads which are knitted to~et:her tG forrn strands 94 are preferably made from 1~90 denier nylon thread. Various other ways of joining strands 94 together are also contemplated. I''or example, strands 94 can be joined ~ /12~ 20 31 S 21 rcT/us90/n224l , ~
together by knotting one strand to the other at their point of intersection. '~ knitted connection is, however, more preferable as it piaces less stress on the individual threads.
Strands 94 forming mesh netting M intersect one another at ang],e which is prefera'bly about 30O so as to create a plurality of diamond shaped openings 98.
The longitudinal apex-to-ape~ length,L of each diamond is preferably within a range oI; about 1.22 to 1.28 inches or about 1-1/4 inches when mesh netting M is in a collapsed state (i.e., when length X and length Y are essentially planar). In addition,^the lateral apex-to-apex length ~ of each diamond when mesh netting M is in an untensioned state is preferab]y within a range of about .320 to .340 of an inch and more preferably about 1/3 of an inch. Nylot1 dia;nond mesh netting suitable for the purposes of ~he presen- invention is a product of Blue Mountain Industries located in Blue Mountain, Alabama. The netting sold by Blue Mountain Industries is referred to as "1-1/4 inch strength No. 189 knotless nylon netting".
The use of a plurality of-knitted threads to form the individual strands and the joining of the strands by a knitting process to form mesh netting M, also provides an advantage with respect to reducing drag. ~ir flowing along the length of the visual augmenter causes the augmenter to assume a tensioned or st,retched state.
While in a tensioned state the individual threads of strands 94 compress together, thus decreasing the W~9U/12996 2 0 31 5 21 1'CT/US90/~2241 - surface area in contact with the on ~ushing air stream.
In addition, tlle arranyement o~ the interconnected strands of mesh netting M, with the diamond shaped openings, leads to one strand drawing an adjacent strand both rearwardly and closer to itself. This arrangement tends to compress the entire body of augmenter 44 inwardly thereby lesse1lir,g the degree of drag caused by the visual augmenter. Further1nore, the angular orientat1on of the rearwardly extendiny strands, wit11 respect to the on rushing air stream, is such that as the augmenter stretches further rearwardly at increased speeds the individual strands 94 tend to assume a position more and more in line with the direction of the on rushing air. This featur~ enables the augmenter to inherently adjust the degre(~ of drag with increases in tow speed. Direction arrow 100 illustrates the direction of the air as it passes along the length of visual augmenter ~4.
Fig. 5 shows vented inf]ator 56 in an inflated condition. In this condition, vented inLlator 56 provides the necessary tension in hoops 60, 62 to form an inlet for a highly porous visual body such as visual body 45 formed of mesh netting M. Vented inflator 56 also performs the function bf obtaining and maintaining a cylindrical shape in the visual augmen~er by utilizing the local airstream as the energy so~rce.
As more fully illustrated in Figs. 5A and 5B, vented inflator 56 includes a number of p~nels 58 attached to forward hoop 62 and aft hoop 60. Hoops 60 wo ~ . r~/ussu/02241 and 62 are preferably formed of.a flexible cable comprised of a materia] such as nylon. In a preferred embodiment the cable is ,made up of a plurality of braided nylon ~it)ers wllicl1 when comblned provide a cable-having a cross-sectional diameter be~ween about 3,/16 of an inch to 1/4 of an inch. A diameter for hoops 60 and 62 which is suitable for t}-e purpose of the invention is about 32.6+.5 and 30.0+.5 inches, respectively. E~oops 60, 62 are also preferably formed in circular or ring-like fashion. The diameter of forw,ard hoop 62 is larger than the diameter of aft hoop 60 bv an amount which causes panels 58 to assume'an angle of attack that preferably falls within a range of a~out 12 to 18 degrees and more preferably is approY~imately 15 relative to the direc~ion of the local airflow. various other angles woul~ also be possible depending on the variables involved such as antlcipated towing speeds, hoop dimensions, etc. In achievinq a 15 angle of attack, forward hoop 62 would preferably have a diameter which is larger than that of aft hoop 60 by a ratio of about 1.087 to 1Ø
The positioning of panels, 58 at an angle of attack of about 15 (see Fig. 115 provides sufficient hoop tension (brought about by aerodynamic forces acting on the panels) to keep the forward end of a cylindrical visual augmenter open and thus enable the visual augmenter to remain in an inflated condition.
Furthermore, a 15 angle of attacr~ provides sufficient aerodynamic loading to provid~ the required hoop tension W~/12996 2 0 3 1 5 2 1 1'CT/US91~/02241 - 19 _ while at the same time minimi7ir,g the drag or force in the actual direction.of the ~isual augmenter.
In a preferr~d ~mbodiment vented inflator 56 includes 16 trunca~d triangular shaped panels 58.
Panels 58 are uniformly positioned with space between each panel and attac11ed to hoops 60, G2 to provide a porosity ratio ~panel area/t:otal ar.ea) of about .5 for the inflator and more preferabi.y about 0.484.
Fig. 7 shows th~ flnished flat pattern for a preferred embodimenL, as well a.s the spacial location relative to 1/16 of the area of ~ented inflator 56, which is equivalent to a 22.5 degree segment of the inflator. Each truncated panel 58 has its forward edge looped over and sewn or fastened to form a passageway for accepting forward hoop cable 62. ~fter cable 62 has been inserted through the loops of panels 58, each panel is positioned with an equal separation space which, with a 32.6 inch diameter .~orward hoop, proves to be about 2.4 inches. The ends of the cable for hoop 62 are then securely fastened together to form the final configuration of hoop 62. Similarly, the cable for aft hoop 60 is inserted through lo~ps formed in the aft end of each panel wit11 equal separation spaces of about 3.9 inches and the ends of the cable. forming aft hoop 60 are joined to form the final configuration of aft hoop 60. ~
Fig. 7B illustrates the manner in which the forward and rearward ends of panels 59 are looped about forward and aft hoops 60,62. ~ .bo~-stitching or the W~ ~U/12~J~ /US90/02241 like is provided which creates ~ snug connection between hoops 60, G2 and the looped portlons of panels 58. In this way, panels 58 do not shift in position with respect to hoops 60, G2. I'urther contem^plated methods for ensuring that panels 58 remain i~-fixed position with respect to ;lOOpS 60, 62 include having threads pass through the braided cable as well as the ends of panel 58 when the loops are formed. ~lternatively, adhesives could be used to prevent slipp~ge of panels 58. The rearward edge 104 of-panel 58 is preferably about half the lengtl- of forward edge 10~ or about two inches. The distance between forward edge 102 and rearward edge 104 as shown in Eig. 7 is preferably about 5 inches.
Various other dimetlsions are also possible depending upon factors such as, for example, the anticipated speeds of towing, the si'ze of the visual augmenter and the materials relied upon.
Panels 58 are contempla~ed as being made of a high strength fiber material. A vinyl nylon cloth referred to as "U.S. ~overnment Part No. 13ZZ7E0131:MIL-C-20696 Type II, Class 1" having a breaking strength equal to about 225 lb for one inch wide strip is contemplated for use in the present invention. Eig. 7C
shows in cross-section a preferred embodiment of panel 58 wherein two vinyl layers Z00 are layered about a cloth (or fiber) weave or mesh ZOZ. This arrangement further ensures that panels'S8 are of sufficient strength to handle the forces that develop during high speed runs. An alternative approach contemplated is to W~90/l~996 ~ I'Cr/U~9~/0224l apply a viny]. coating on both sides-Aof a layer of mesh or cloth.
Vented inflator 56 is attached to suspension lines 64 as best illustrated in ~`'i.g. 7. Suspension lines 64 have their ends iooped ~bout forward hoop 62 and box stitched to snug].y fit about hoop 62 so as not to slide thereon. Additionally, various other means such as adhesives can be used~to ensure no slippage of suspension lines 64 with respect t~ hooF 62. Visual augmenter 44 has at its forward edge a strip of material 204 which is connected to the individual strands forming the mesh pattern M. This strip of material is joined to aft cable 60 by lacing 206 which e~tends through the diamond mesh netting and around aft ca~le 60 and stri.p 204 in the open areas between adjacent panels 58.
Lacing 206 is preferably formed of a wa~ed coated nylon material with the wax avoiding undue slippage while wrapping and knotting lacing 206 about both strip 204 and aft cable 60.
Fig. 11 provides a force dlagram for panels 58 while in a tension state due to drag created by visual augmenter 44 and the tension placed on_suspension lines 64. Fig. 11 also illustrates a 15 degree anqle of attack for panel 58 shown in cross section. As can be seen in Fig. 11, panel 58 !-as its forward and rearward ends looped about hoops 60, 62. The forward and aft hoops 60, 62 are in tension resulting from the normal force created by the aerodynamic loading of panels 58.
As a result of the largeF diameter of forward hoop 62, WO 9U/12996 I'CI /US91)/02241 2031~2^1 in relation to the diametex of aft hcop 60, panels 58 are positioned within an approY~imate angle of attack of 15O relative to incoming air. The aerodynamic norma]
force of the panel can be broken down into two orthogonal components; the radial component (i.e. hoop tension) and the axial or drag~ component. The longitudinal tension required to maintain the preferred 5 inch separation distance between forward and aft hoops 60, 62 is provided by Ihe opposi:ng s~ispension line 64 tension acting forward and the visual augmenter 44 drag acting to the rear.
The spacial arrange~ent for panels 58 is configured to provide nearly equal size openings between each panel 58. With this arrangement, separation and the resulting turbulence of t'ne local air stream over and around the panels is minimized. The spacial arrangement of the openings betwéen the panels also provides a means for tailoring or optimizing the desired hoop tension over a wide varlety of alrspeed operations.
The spacial arrangement of the panels 58 could vary in accordance with the specific requirements desired of the visual augmenter. ~ preferred embodiment has sixteen panels 58 spaced equally about forward and aft hoops 60,62.
Tow harness 106 (shown in Figs. 12~ and 12B) is comprised of a plurali'y of riser lines 66 and suspension lines 64. In the embodiment shown in Fig. 2, four riser lines 6G are attached to frame structure at 72. Riser lines 66 are preferably about 5 feet in ~V~ ' l'CT/US90/0224l ~ .
length and made from 1.75 inch wide U.S. Government nylon webbing designated ~ W-4088 Type VIII, Class 2 with a described breaking strength of 3500 lbs. I'o fixation point 68 (Figs. 12A and 1?B), is attached four suspension lines 64 each preferably made from 1/2 inch commercial grade nylon webbing having a described breaking strengtl1 of 500 'lb. The four suspension lines 64, are attached to one-of the I'our riser lines 66 at fixation point 68. This attaehm~nt is shown in Fig. 12 and Fig. 1 2B to be made by use of a box stitch.
Similarly, suspensior- lines 64 are connected to forward hoop 62 by wrapping the end o~ suspension line 64 about hoop 62 and using a box -stitch to keep it in place. The forward end of riser line 66 also includes loop section 108 which is connected to cable 116 (Fig. 16) that attaches to one of the bra'nches of frame 72.
Fig. 8, which is based on calculations, depicts graphically the reduced drag made possible by the present invention. In Fig. 8 line 110 shows the increase in drag whicl1 would occur if a prior art visual augmenter such as that shown'ln ~ig. 3 was increased an additional 10 feet. By utillzat~ol1 of suspension lines 64 and riser lines 66 each of about 5 feet in length, the entire length of the visual augmenter can be increased by about 10 feet. As set forth previously, the reliance on the combination of mesh netting M, vented inflator 56 and t~w hàrness 106 allows for extension of the aerial qunnerv target of the present invention while maintaining a re~uced drag value. The ~uYU~ CT/US9U/0224l aerial gunnery target of the present invention also enhances visual acuity o~ the target. The enhancement in visual acuity is macle posslbl~ by.the added lengtll and, more importantly, the ability of the augmenter 44 to maintain a relatively uniform and condensed body which contrasts sharply agai.nst the environmental background. l`lle vented i.nflator 5.6 assists in inflating visual augmenter 44 so as to maintain a g~nerally cylindrical shape. Moreover, the passage of incoming air through vente(l inLlator 56 and- through the length of visual augmenter 44 helps prevent o~cillation caused by external forces acting on the vlsual augmenter.
Fig. 9 whi.cll is based on calculations depicts, graphically, the normal and drag`forces which would be expected to develop in panels 58 in relat~on to the velocity of the towed visual augmenter. The limit value M shown in Fig. 9 is represented as .95 Mach or 448 KCAS
[knots calibrated ai.r speed~. Fi.g. 9 represents the normal and drag forces acting on panels 56 when at an attack angle of 15O. The materlal forming panels 56 as well as the manner of attachment to hoops 60, 62 must be capable of withstanding the forces shown in Fig. 9.
Fig. 10 shows tlle calculated drag which can be e~pected due to the addition of vented inflator 56 to visual auqmenter 4~. Fig. 1~ also.revea~.s that th~ dr.~-~developed by including the vented inflator remains relatively low even up in.the higher maxi.mum speed regions.
~ /l2~ ' 2 0 315 21 rCT/US90/0224l - 2'. -Returning to ~ig. 2, reeling mact1ine 82 isattached to the underside of one of the towing aircraft's wings. The r~eLing'machine includes a releasable attachment device 112~that is capable of S releasing forebody assembly 48 upon command of the pilot. In normal operation' visual augmenter 44 and towing harness 1~6 are contained within deployment bag 114 (Fig. 15) prior to deployment. Whlle in flight above the predeterrnined target area, cutter mechanism 116 (Fig. 15) is activated (e;g. by an electronic signal) so as to cut the deployment line'118. Once deployment line is cut, branches 70 begin to extend outwardly and dep]oyment bag 114 is-drawn from its covering position. ~fte'r hag 114 is drawn off by drag forces, the drag forces further act to deploy visual augmenter 44. Thereafter, forebody 48 is detached from attachment device 112 and reeled outwardly a'long tow line 80 (Fig. 2) until the visual augmenter 44 is the desired length awa~ from th~ towing aircraft (e.g. ~,000 feet).
In operating an aerial gunnery target such as that of the present irivention it is'necessary to exclude the use of radar reflective type material within the scoring pattern envelope, i.e., visual augmenter 44 and the surrounding area within-radar zone R2. If radar reflective material is used in the; visual augmenter, vented inflator or in the towing harness it is highly probable that the unsteady highly cyclic vibrational type motion of the augmenter w ll-result in false W~90/12996 ~'' rCT/US9U/02241 - 2( -scoring outputs of the radar scorlng system. The radar return of this motion-can easily be misinterpreted by the scoring system as munition rounds'passing through the scoring envelope., ~ccordingly, the present invention relies on a towing harness and visual augmenter formed of material which lS not radar reflective. The foregoing discussion indicates that various materials such as~nylon have proven suitable for the purposes of the present invention.
Referring again to Flg. 15, it is apparent that storage volume constraints alsG influence the design concept of a visual augmenter inflator. The flexible panel/hoop cable design of the vented inflator 56 provides a non-rigid highly fle~ible structure that can be folded or packed into virtually any shaped storage container or storage envelope so as to minimize storage volume requirernents. The fleY.ible riser and suspension lines are also easily folded up within storage container 114.
Following the desire-] target practice, the gunnery target is reeled -in until forebody 48 becomes reattached to attachment device 11 ? Visual augmenter 44 and towing harness 106 are then released and allowed to drop to the ground or body of water below.
Fig. 16 illustrates,the manner in which towing harness 106 is disconnected from frame assembly 72 which is attached to shaft 74. To release tow harness 106, shaft 74 is drawn inwardly into the rear end of forebody assembly 48. This inward rr,ovement of,shaft 74 causes W~/12~ 2 03152 1 l'CI/V~90/02241 branches 70 to collapse inwardly and in the rearward direction. Consequently, cable loops-116 and attached lead weights 118 are able to slide ou~t of notches formed in branches tO and becollle released as illustrated in S dashed lines in Fic~. 20. Vicu~] augmenters 44 are then picked up upon landing on the ground or, if target practice is to take place over a body of water, visual augmenters 44 fall below the surface of the water and tend to remain entirely in c~ntact witl1 the underwater bottom surface.
Figs. 17~ and 17B illustrate various sized openings at the aft end of visual augmenter 44. Air flowing through visua] augmenter 44 in the direction of line 118 passes through opening 120. Drag can be increased by decreasinQ the size of opening 120. Hence, for slow speeds where it is desired to increase the drag of visual augmenter 44 so as to maintain proper positioning, the aft end opening 120 can be decreased in size as shown in Fig. 17~. Va-iations in the size of aft opening 120 are made possib]e by adjustment device 122 which includes a nylon cord 126 (or the like) passing within a sleeve provided at the aft end of mesh netting M. Cord 126 is shown as having two free ends which pass through adjustmènt clip 128. By drawin<~ the free ends of cord 126 awày from adjustment clip 128, the aft end opening 120 is made smaller.
Figs. 13 and 14 show two alternate embodiments of the present invention. In Fig. 13, swivel connector 134 allows for visual augmenter 136~and e~tension device 138 ' w~ () l'CT/US~()/0224l ` 2031~21 - 2~ -~ '.
to freely rotate with respect to forebody assembly 48.
Other than the swivel connector hetween forebody assembly 48 anc'l e~tensiol1 device 138, all other features are similar ~o that of the visual augmenter illustrated in Fig. 2. Fig. 14 is essential~y the same as Fig.17 except for the addition of dra~ line 140 between forebody assembly 48 and swivel connector 134. In utilizing the embodiments of Figs. 13 and 14, detachment of visual augmenter 44 is made~s1mple in that all that is required is a release of the swlvel connector 134 or, alternatively, connection device 210 shown in Fig. 14.
As can be seen, the ad~it'ion of vented inflator at the forefront of,the visual augmenter provides a great deal of freedom in determining how the visual augmenter is to be attached to a forebody assembly or, alternatively, directly t~o the end of a tow cable. The vented inflator makes unnecessar~ the use of frame structures to maintain the front opening of a visual augmenter in an open state. Moreover, the vented inflator of the present invention allows for non-rigid and non-radar reflective material to provide the required opening at the front of a visual augmenter.
FIG. 18 shows a side,view of an--alternate embodiment of the present invention. In FIG. 18, aerial gunnery target 298 features suspension line assembly 301 with suspension lines ~99. Attached to the rearward end of suspension line assemb]y 301 is vented inflator 302 which includes hoop sh~ped forward connection means 303 and hoop shaped rearward connect,ion means 305 wo ~0/12996 rCr/l~S90/0224l 20315`21 longltudinally displaced from one another. A plurality of attachment members 304 e~ter-d between the forward and rearward conncctiol1 rncal1s.
l~IG. 19 shows the front view of aerial gunnery target 298 having suspension line assembly 301 with suspension lines 299 e.~tending~to a common connection point. At the forward portion of vented inflator 302 is bead 307. As shown, at:tachment members 304 incline inwardly to connect Witl1 rearward connection means 305 to form a plurality of alr vents 312.
FIG. 20 illustrates in gre~ter detail the forward end o2-- aerial gunnery targèt 298. Suspension line 299 includes loop 313 which is conr.ected to loop 314 (FIG.
21A) formed in the forward end of each of the attachment members 304. 13ead 307 i 9 shown to extend through loop 314 and includes threacl 308 which interconnects bead 307 with the visual augmenter represented by mesh netting M
by looping and lacing thread 308 about bead 307 and the mesh netting's edge. Webbing strip 306 is` shown to be positioned inside of mesh netting ~. and-- to the outside of a portion of attachment member 304.
FIGS. 21A and 21B show in greater detail the forward end of aerial gunnery target 298. As shown, attachment members 30~ e~tend at an incline from rearward connec'cion means 305. The end portion of attachment members 304 are connected to rearward connection means 305 by extending th~ er.d portion about both sides of rearward connection means 305 and stitching the combination together. Rearward connection WO ~()/l2$~6 2 0 315 21 l'Cr/US90/0224l - 3(~ -means 305 is posi'ioned at an incline to confront in rushing air and to assist in infiating the forward end of the gunnery target~.
The degree of incline is adjustable for intended 5 use with the preferred incline being 40 to 50 as represented by angle "y" in FIG. 211~. As also shown in FIG. 21a, the preLerred angle "s~" for the incline of attachment members 304 is 15 i:o 30.
As best shown in I~IG. 21B first we~bing member 310 is positioned externally of end po~-tion 316 of attachment members 304. The visual au~menter netting M
is positioned below end portion 316 while second webbing member 306 is positioned below mesh netting M. Body portion 318 of attachmenL members 304 are positioned directly below second webbing member 306 and the entire combination of body portion 318~ second webbing member 306, mesh netting M, end portion 316 and first webbing member 310 are joined together preferably by box stitching, adhesive or a combination thereof.
Z0 In a preferred embodiment, first webbing member 310, second webbing member 306, attachment members 304, rearward connection means 305, bead 307 and thread 308 are all formed of a nylon material. The preferred dimensions include first webbing member having a two-inch width; rearward connection means having a width of to 2 inches; second w-ebbing member having a width of3 inches; and attachment member having a width of 2 to 3 inches. Nylon thread 308 is preferably of 40 lb.
strength.
~v~u~ Y~ . I ~/US90/()224l - 31 _ FIG. 22A shows the-mar.ner in which lines 299 are brought together at their end. As shown wrap 318 is secured by a stitchin9 process o the ends of four suspension lines doubled over to.provide eight lines extending outwardly. The susp~nsion lines 299 are preferably formed of 3/16 diameter nylon rope (900 lbs).
FIG. 22B shows one of the suspension lines shown in FIG. 22A having a hraided rope loop 309.
FIG. 23~ shows a side view of that which is shown in ~IG. 22A. As sl1own the eight suspension lines are formed by doubling over four suspension lines and attaching web member 318 to hold the suspension lines together at a connection point. FIG. 23B shows a side view of the line shown in FIG. 23B.
~ lthouqh tlie preferred embodiments of the present invention have been describ~d Witll reference to the accompanying drawings many modifi.cati.ons and changes may be effected by those skilled in the art without departing from tl1e scope and spirlt of the invention as appended hereinafter.
Claims (33)
1. An aerial gunnery target, comprising:
a forebody assembly;
a visual augmenter formed of mesh netting, said mesh netting having interconnected strands which are joined together at points of intersection by knitting; and attachment means for attaching said visual augmenter to said forebody assembly.
a forebody assembly;
a visual augmenter formed of mesh netting, said mesh netting having interconnected strands which are joined together at points of intersection by knitting; and attachment means for attaching said visual augmenter to said forebody assembly.
2. A target as recited in claim 1, wherein said visual augmenter, when deployed, assumes a generally cylindrical shape with an open forward end and a partially closed aft end.
3. A target as recited in claim 2, wherein said interconnected strands intersect one another to form diamond shaped openings.
4. A target as recited in claim 3, wherein said interconnected strands are formed of a plurality of knitted threads and said interconnected strands are joined together at a point of intersection by knitting the knitted threads of one interconnected strand to the knitted threads of another interconnected strand.
5. An aerial gunnery target, comprising:
a visual augmenter;
means for securing said visual augmenter to a towing device, said means for securing including a vented inflator, said vented inflator having a first and a second hoop longitudinally displaced from one another with flexible connectors extending between said hoops, and said second hoop connected to the forward end of said visual augmenter.
a visual augmenter;
means for securing said visual augmenter to a towing device, said means for securing including a vented inflator, said vented inflator having a first and a second hoop longitudinally displaced from one another with flexible connectors extending between said hoops, and said second hoop connected to the forward end of said visual augmenter.
6. A target as recited in claim 5, wherein said flexible connectors are panels arranged between said hoops such that an air vent is formed between adjacent panels.
7. A target as recited in claim 6, wherein the opening defined by said first hoop is larger in diameter than the opening defined by said second hoop such that each panel, when in a tensioned state, forms an angle of attack with respect to incoming air of about 12 to 18 degrees.
8. A target as recited in claim 6, wherein said panels have a forward and a rearward edge in attachment with respective ones of said hoops such that the forward edge is about twice the width of the rearward edge.
9. A target as recited in claim 5 wherein said means for securing said visual augmenter to a towing device includes a forebody assembly having a scoring device.
10. An aerial gunnery target, comprising:
a forebody assembly;
a vented inflator having a longitudinally spaced forward and rearward hoop and means to interconnect said longitudinally spaced forward and rearward hoops;
a visual augmenter having a front portion attached to said vented inflator; and attachment means for attaching said vented inflator to said forebody assembly, said attachments means comprising a frame secured to said forebody assembly having branches extending axially from a common locus, risers extending rearwardly off and attached to a free end of said branches, and sets of suspension lines with each set including a plurality of suspension lines and each set of suspension lines being attached to a respective one of said risers, and said suspension lines extending divergently outward for connection to said vented inflator.
a forebody assembly;
a vented inflator having a longitudinally spaced forward and rearward hoop and means to interconnect said longitudinally spaced forward and rearward hoops;
a visual augmenter having a front portion attached to said vented inflator; and attachment means for attaching said vented inflator to said forebody assembly, said attachments means comprising a frame secured to said forebody assembly having branches extending axially from a common locus, risers extending rearwardly off and attached to a free end of said branches, and sets of suspension lines with each set including a plurality of suspension lines and each set of suspension lines being attached to a respective one of said risers, and said suspension lines extending divergently outward for connection to said vented inflator.
11. A target as recited in claim 10, wherein said means to interconnect said longitudinally spaced forward and rearward hoop includes a plurality of flexible panels positioned between said forward and rearward hoops, said panels being spaced uniformly from one another about said hoops so as to form a plurality of air vents, said suspension lines each having a rearward end attached to said forward hoop between adjacent panels.
12. A target as recited in claim 11, wherein said risers, suspension lines and hoops are formed of non-metallic material.
13. An aerial gunnery target, comprising:
a forebody assembly;
a vented inflator having a longitudinally spaced forward and rearward hoop and interconnection means to interconnect said longitudinally spaced forward and rearward hoops;
a visual augmenter attached to said vented inflator;
attachment means for attaching said vented inflator to said forebody assembly, and said attachments means comprising:
a connection device secured to said forebody assembly;
risers each having a forward end in attachment with said connection device; and sets of suspension lines with each set including a plurality of suspension lines and each set of suspension lines being attached to a respective one of said risers, and said suspension lines extending divergently out away from the rearward end of said risers and being connected to said vented inflator.
a forebody assembly;
a vented inflator having a longitudinally spaced forward and rearward hoop and interconnection means to interconnect said longitudinally spaced forward and rearward hoops;
a visual augmenter attached to said vented inflator;
attachment means for attaching said vented inflator to said forebody assembly, and said attachments means comprising:
a connection device secured to said forebody assembly;
risers each having a forward end in attachment with said connection device; and sets of suspension lines with each set including a plurality of suspension lines and each set of suspension lines being attached to a respective one of said risers, and said suspension lines extending divergently out away from the rearward end of said risers and being connected to said vented inflator.
14. A target as recited in claim 13, wherein said interconnection means has a plurality of flexible panels positioned between said forward and rearward hoops, said panels being spaced uniformly from one another about said hoops so as to form a plurality of air vents, and said suspension lines each having a rearward end attached to said forward hoop between adjacent panels, and said rearward hoop being connected to said visual augmenter.
15. A target as recited in claim 13, wherein said attachment device includes a drag line having a forward end connected to the rear end of said forebody assembly and a rearward end attached to said connection device so as to increase the distance between said forebody assembly and said visual augmenter.
16. An aerial gunnery target, comprising:
a visual augmenter having an elongated body and an open forward and aft end; and a vented inflator attached to the forward end of said visual augmenter, said vented inflator including first and second connection means and means to interconnect said first and second connection means such that a plurality of air vents are formed, and said first and second connection means defining different size openings such that said interconnection means is inclined with respect to air rushing into said different size openings.
a visual augmenter having an elongated body and an open forward and aft end; and a vented inflator attached to the forward end of said visual augmenter, said vented inflator including first and second connection means and means to interconnect said first and second connection means such that a plurality of air vents are formed, and said first and second connection means defining different size openings such that said interconnection means is inclined with respect to air rushing into said different size openings.
17. A target as recited in claim 16, wherein said first and second connection means are ring shaped hoops longitudinally spaced forward and aft at the forefront of said visual augmenter and said forward hoop defining a greater internal diameter than said aft hoop.
18. A target as recited in claim 17, wherein the forward end of said visual augmenter is secured to said aft hoop.
19. A target as recited in claim 16, wherein said interconnection means includes a plurality of flexible panels spaced along said first and second connection means so as to define air vents.
20. An aerial gunnery target, comprising:
a visual augmenter having a forward and a rearward end;
securement means for securing said visual augmenter to a towing device, said securement means including a vented inflator connected to the forward end of said visual augmenter, said vented inflator formed of a flexible material and having a plurality of air vent openings formed therein, and said vented inflator, when in an inflated state, being inclined with respect to incoming air such that the forward end of said visual augmenter is placed in a tensioned state.
a visual augmenter having a forward and a rearward end;
securement means for securing said visual augmenter to a towing device, said securement means including a vented inflator connected to the forward end of said visual augmenter, said vented inflator formed of a flexible material and having a plurality of air vent openings formed therein, and said vented inflator, when in an inflated state, being inclined with respect to incoming air such that the forward end of said visual augmenter is placed in a tensioned state.
21. An aerial gunnery target, comprising:
suspension lines;
a vented inflator including forward connection means and rearward connection means longitudinally spaced from one another, said vented inflator further including attachment members extending between said forward and rearward connection means and said attachment members being spaced from one another, said attachment members being secured to said forward and rearward connection means and said attachment members each being attached to a respective one of said suspension lines;
said forward and rearward connection means being essentially circular in configuration, and said forward connection means being larger in diameter than said rearward connection means such that said attachment members are at an incline in extending between said forward and rearward connection means; and a visual augmenter secured to said vented inflator.
suspension lines;
a vented inflator including forward connection means and rearward connection means longitudinally spaced from one another, said vented inflator further including attachment members extending between said forward and rearward connection means and said attachment members being spaced from one another, said attachment members being secured to said forward and rearward connection means and said attachment members each being attached to a respective one of said suspension lines;
said forward and rearward connection means being essentially circular in configuration, and said forward connection means being larger in diameter than said rearward connection means such that said attachment members are at an incline in extending between said forward and rearward connection means; and a visual augmenter secured to said vented inflator.
22. An aerial gunnery target as recited in claim 21, wherein said visual augmenter is secured to said forward connection means.
23. An aerial gunnery target as recited in claim 21, wherein said forward connection means comprises a first webbing member having a circular configuration and a circular bead in attachment with said visual augmenter and spaced to one side of said first webbing means.
24. An aerial gunnery target as recited in claim 23, wherein said forward connection means further comprises a second webbing member having a circular configuration and spaced below said first webbing member, said visual augmenter positioned between said first and second webbing members and being attached to said first and second webbing members.
25. An aerial gunnery target as recited in claim 24, wherein said attachment members extend between said first and second webbing members and are affixed between said first and second webbing members, said attachment members being looped about said bead and affixed to the side of said second webbing member which is further from said first webbing member.
26. An aerial gunnery target as recited in claim 23, wherein said rearward connection means includes a strap member having a planar interior surface inclined such that in rushing air creates an outward tension in said circular strap member.
27. An aerial gunnery target comprising:
a visual augmenter;
a vented inflator attached to said visual augmenter, said vented inflator comprising a circular web and a circular webbing member longitudinally spaced from said circular web and having a diameter less than said circular web, a plurality of strap members having a first end, a body portion and a second end, said circu-lar web attached to the body portion of said strap mem-ber, said strap member extending at an incline between said web and said webbing member, said webbing member attached to the second end of said strap member and the first end of said strap member including a loop section extending out away from said web and said webbing mem-ber.
a visual augmenter;
a vented inflator attached to said visual augmenter, said vented inflator comprising a circular web and a circular webbing member longitudinally spaced from said circular web and having a diameter less than said circular web, a plurality of strap members having a first end, a body portion and a second end, said circu-lar web attached to the body portion of said strap mem-ber, said strap member extending at an incline between said web and said webbing member, said webbing member attached to the second end of said strap member and the first end of said strap member including a loop section extending out away from said web and said webbing mem-ber.
28. An aerial gunnery target, comprising:
a visual augmenter with a front end and a rear end;
a vented inflator connected to the front end of said visual augmenter, said vented inflator in-cluding a first hoop and a second hoop longitudinally spaced from said first hoop as well as interconnection means which interconnects said first and second hoops and defines a plurality of air ports in said vented in-flator between said first and second hoops, and said vented inflator being dimensioned and arranged with re-spect to said visual augmenter so as to inflate the front end of said visual augmenter when placed in an air stream.
a visual augmenter with a front end and a rear end;
a vented inflator connected to the front end of said visual augmenter, said vented inflator in-cluding a first hoop and a second hoop longitudinally spaced from said first hoop as well as interconnection means which interconnects said first and second hoops and defines a plurality of air ports in said vented in-flator between said first and second hoops, and said vented inflator being dimensioned and arranged with re-spect to said visual augmenter so as to inflate the front end of said visual augmenter when placed in an air stream.
29. An aerial gunnery target as recited in claim 28 wherein said hoops are circular in configura-tion with the first hoop being more forward and larger in diameter than said second hoop.
30. An aerial gunnery target as recited in claim 28 wherein said interconnection means is comprised of a plurality of panels that are formed of flexible ma-terial and spaced about the circumference of the hoops, and said visual augmenter is connected to said first hoop.
31. An aerial gunnery target as recited in claim 28 wherein said interconnection means is comprised of a plurality of panels that are formed of flexible ma-terial and spaced about the circumference of the hoops, and said visual augmenter is connected to said second hoop.
32. An aerial gunnery target as recited in claim 28 further comprising a forebody and means for connecting said vented inflator to said forebody.
33. An aerial gunnery target as recited in claim 32 wherein said means for connecting includes a swivel connector.
Applications Claiming Priority (4)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US343,438 | 1989-04-26 | ||
| US07/343,438 US5026073A (en) | 1989-04-26 | 1989-04-26 | Aerial gunnery target |
| USPCT/US90/02241 | 1990-04-25 | ||
| PCT/US1990/002241 WO1990012996A1 (en) | 1989-04-26 | 1990-04-25 | Aerial gunnery target |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CA2031521A1 CA2031521A1 (en) | 1990-10-27 |
| CA2031521C true CA2031521C (en) | 1994-10-18 |
Family
ID=23346117
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA002031521A Expired - Fee Related CA2031521C (en) | 1989-04-26 | 1990-04-25 | Aerial gunnery target |
Country Status (9)
| Country | Link |
|---|---|
| US (1) | US5026073A (en) |
| EP (1) | EP0422207B1 (en) |
| JP (1) | JP2562518B2 (en) |
| KR (1) | KR940010381B1 (en) |
| AU (1) | AU5632190A (en) |
| CA (1) | CA2031521C (en) |
| DE (1) | DE69007581T2 (en) |
| ES (1) | ES2023098A4 (en) |
| WO (1) | WO1990012996A1 (en) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5078406A (en) * | 1989-04-26 | 1992-01-07 | Teledyne Industries, Inc. | Aerial gunnery target |
| US5102145A (en) * | 1991-04-16 | 1992-04-07 | Teledyne Industries, Inc. | Aerial gunnery target system |
| US5365685A (en) * | 1993-04-09 | 1994-11-22 | Shank Lynn D | Aerial advertising wind tube |
| DE4420206A1 (en) * | 1994-06-10 | 1995-12-14 | Dornier Gmbh | Visibility banner deployment system for towed airborne target |
| US10260844B2 (en) * | 2008-03-17 | 2019-04-16 | Israel Aerospace Industries, Ltd. | Method for performing exo-atmospheric missile's interception trial |
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| BE561830A (en) * | ||||
| FR496230A (en) * | 1918-02-13 | 1919-10-30 | Haeberlin Emilie | Objective sleeve for aerial shots |
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| US1901885A (en) * | 1930-07-08 | 1933-03-21 | Natural Gas Hydrogen Corp | Process for the manufacture of industrial hydrogen |
| US1860982A (en) * | 1931-03-27 | 1932-05-31 | John A Binnie | Aerial device |
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| US2153562A (en) * | 1933-11-22 | 1939-04-11 | Kellett Autogiro Corp | Aerial advertising banner |
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| US1974039A (en) * | 1934-04-21 | 1934-09-18 | William A Bohannon | Aerial banner |
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| US2238875A (en) * | 1939-08-14 | 1941-04-15 | Frank G Manson | Aerial trailer |
| US2238876A (en) * | 1939-08-14 | 1941-04-15 | Frank G Manson | Aerial trailer |
| FR865970A (en) * | 1940-02-21 | 1941-06-11 | Mademoiselle Marguerite | Aircraft towed aerial target |
| FR865109A (en) * | 1940-04-23 | 1941-05-14 | Improvements to target panels for aircraft shooting | |
| US2270884A (en) * | 1940-11-12 | 1942-01-27 | Frank G Manson | Aerial trailer |
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| US2402156A (en) * | 1944-05-27 | 1946-06-18 | John W Griesinger | Astern attack tow target |
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| US2486999A (en) * | 1945-07-25 | 1949-11-01 | North Carolina Navigation Comp | Paying out device for aircraft towing targets, picking up objects, etc. |
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| FR1570025A (en) * | 1968-04-24 | 1969-06-06 | ||
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-
1989
- 1989-04-26 US US07/343,438 patent/US5026073A/en not_active Expired - Fee Related
-
1990
- 1990-04-25 JP JP2507245A patent/JP2562518B2/en not_active Expired - Lifetime
- 1990-04-25 KR KR1019900702656A patent/KR940010381B1/en not_active IP Right Cessation
- 1990-04-25 EP EP90907892A patent/EP0422207B1/en not_active Expired - Lifetime
- 1990-04-25 AU AU56321/90A patent/AU5632190A/en not_active Abandoned
- 1990-04-25 CA CA002031521A patent/CA2031521C/en not_active Expired - Fee Related
- 1990-04-25 WO PCT/US1990/002241 patent/WO1990012996A1/en active IP Right Grant
- 1990-04-25 ES ES90907892T patent/ES2023098A4/en active Pending
- 1990-04-25 DE DE69007581T patent/DE69007581T2/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| EP0422207A1 (en) | 1991-04-17 |
| KR920700385A (en) | 1992-02-19 |
| JP2562518B2 (en) | 1996-12-11 |
| DE69007581T2 (en) | 1994-10-06 |
| WO1990012996A1 (en) | 1990-11-01 |
| EP0422207A4 (en) | 1991-11-27 |
| JPH03505626A (en) | 1991-12-05 |
| EP0422207B1 (en) | 1994-03-23 |
| CA2031521A1 (en) | 1990-10-27 |
| AU5632190A (en) | 1990-11-16 |
| ES2023098A4 (en) | 1992-01-01 |
| DE69007581D1 (en) | 1994-04-28 |
| US5026073A (en) | 1991-06-25 |
| KR940010381B1 (en) | 1994-10-22 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request | ||
| MKLA | Lapsed | ||
| MKLA | Lapsed |
Effective date: 20000425 |