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Publication numberUS2546078 A
Publication typeGrant
Publication dateMar 20, 1951
Filing dateNov 23, 1948
Priority dateNov 23, 1948
Publication numberUS 2546078 A, US 2546078A, US-A-2546078, US2546078 A, US2546078A
InventorsRogallo Gertrude Sugden, Rogallo Francis Melvin
Original AssigneeRogallo Gertrude Sugden, Rogallo Francis Melvin
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Flexible kite
US 2546078 A
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Description  (OCR text may contain errors)

March 20, 1951 s. s. ROGALLO ETAL FLEXIBLE KITE Filed Nov. 23, 1948 Illa I N VEN TORS'.

GERTRUDE SUGDEN ROGALLO BY FRANCIS MELVIN ROGALLO Patented Mar. 20, 1951 UNITED STATES PATENT OFFICE FLEXIBLE KITE Gertrude Sugden Rogallo and Francis Melvin V iltogallo, Hampton, Va.

Application ltlovember 23, 1943, Serial No. 61,702

'59 Claims. 1

I This invention relates to kites and more particularly to a kit having completely flexible surfaces. i

It is an object of our invention to provide a kite of "simple and economic construction and wherein the use of reinforcing members may be ordinarily eliminated.

. It is another object of our invention to provide a kite which will be simple to fly and graceful in flight.

It is a further object of our invention to provide akite structure which may bej-e'asily folded or rolled and requires a minimum of space in storage.

It is still another object of ourinvention to provide s.- structure for a kite having improved aerodynamic characteristics.

In general we achieve the above object by constructing a kite of a substantially jquadrilateral piece of fabric, paper or other light and flexible material, having bridle strings attached at various points, and a tail secured to the kite when necessary, so that the stress in the strings exerted at strategic points of the kites surface maintains the kite in proper shape and configuration to be efiectively supported even in a light breeze. Owing to the fact that our kite does not require the use of stiffening members, it is considerably lighter than other kites of the same area and hence more easily flown in a light breeze.

Other objects and features of our invention will be evident from the detailed description which now follows taken in conjunction with the appended drawings in which:

Fig. 1 is a plan view of our novel type struc- .ture :as itrests on a fiat surface prior to flight;

Fi is a plan view of our kite in flight;

Fige-3 is an elevation of our kite in flight showing an appropriate angle of attack;

1 Fig.4 represents the manner inwhich a plurality of ourkites may be coupled in'flight;

Fig. 51s'hows a section through 5-5 of Fig. 2; and Figs. fia-c show sections of various types of reinforcements suitable for use in conjunction with 'ourkite, if desired.

With respect to Figs. 1 through 3, our invention contemplates the use of a substantially square piece of iabric or paper lll forming a body memher having a diagonal fold line [3 provided therein dividing the body into symmetrical sections that may belly upwardly on both sides of the fold line to form lateral support surfaces when aloft. A series of bridle lines l6 through 22 are syminetrically attached to the kite and are brought 2 together and secured to a main control line 26, as shown in Fig. 3.

The bridle lines I 6, HI and 22 are secured to the kite at the fold line I3 in any suitable manner as by punching a hole through the material just above the fold line when the kite is completely folded, and then passing strings through the holes, tying th ends thereof so as to secure the strings in their respective holes. Alternatively, adhesive patches may be utilized to hold the string ends to the kite fabric at the fold line, if desired. The bridle lines I! and I8 are secured to the kite fabric on either side of the center line, while the lines 20 and 2| are fastened substantially at the lateral tips of the square, all of these lines being adjacent respective leading edges of the body. The particular arrangement is indicated on Fig. 1,, wherein is shown exaggeratsdly the string ends passing upwardly through the kite body.

The length relationships of the several lines is such as to provide any desired degree of arcuateness of the body member sections depending on the degree of wind encountered. The relationship shown is suitably proportioned for general purposes.

In strong winds we have found a tail to be essential and we prefer to utilize for this purpose a ribbon-like material of any suitable type such as cloth or aluminum foil, indicated at 30. The tail 3!) is attached through a swivel joint 33 to a pair of lines 35 and 38 which are secured to respective trailing edges of the kite substantially at the mid-portions thereof, as shown in Figs. 1 and 2. Alternatively, the lines 35 and 38 could be secured to the kite substantially at the locations shown for the ends of lines 20 and 2|. It will be appreciated that the particular location for the attaching ends of the tail lines may be changed to suit various conditions, such as the size and weight of the kite, the weight of the tall, the wind encountered, etc. We have found, however, as a matter of actual practice, that the location shown in Figs. 1 and 2 is suitable for general purposes.

One of the pleasing aspects found in flying our kite is the fact that in gusty air or when the string is deliberately jerked the non-rigid structure allows the shape to change in a manner suggesting a flying or swimming creature. Further, in order to enhance the attractiveness of our kite, we may construct it of transparent material, such as cellophane, or cellophane reinforced with a grid of string embedded therein and provide colored pictures of birds, rockets, etc. translucently thereon. In addition, phosphorescent k k 3 paint may be used so as to obtain a startling and pleasing effect when flying our kite at night.

In physical aspect, our kite performs very successfully when constructed of reinforced cellophane paper out as a square with the sides thereof about eighteen inches long. The tail may be attached thereto by a single string terminating at the diagonal line [3, but we prefer the two-string arrangement, hereinabove described. The swivel joint 33- prevents the whipping tail from twisting the strings 35 and 38 about each other.

In Fig. 4 is shown a manner in which a plurality of kites, as hereinabove described, may be coupled for simultaneous flight. It will be appreciated that the kites need not be all of the same size but might be of progressively smaller area, so that the bridle strings 40 would have no angular bends therein, but would represent elements and corners of an inverted pyramid from the juncture point 43 to the points of attachment with the uppermost kite.

While we have shown but one form of the kite insofar as configuration is concerned, other forms are entirely feasible. For example, rectangular and elliptical configurations may be used. Further, while we prefer to utilize non-rigid nonreinforced lifting surfaces, it will be appreciated that reinforcements could be applied as shown in connection with Fig. 6a through 0, depending upon the particular use the kite is to be put and upon the ize thereof.

. Fig. 6a represents a kite following our teaching but utilizing a reinforcement of round cross section which may be applied at the center line l3 and also at the leading and trailing edges. Fig. 6bshows the manner of attachment of a reinforcement of fiat cross section. Fig. 6c is similar to Fig. 60. except that the reinforcement is hollow, and flexible so as to be filled with compressed air, or other gas, for maintaining rigidity. Such reinforcements might conceivabl be comprised of flexible materials such as wood and even more flexible material such as soft rubber tubing or adhesive tape. In any event, the reinforcing material should not be so stiff as to prevent the leading and trailing edges from assuming proper arcuate shape as the material of the kite bellies out in flight, although a rigid reinforcement could be used at the center line, if

desired. In general, the use of reinforcements reduces the required number of bridle strings and considerable latitude may be exercised in the type of reinforcement'used. It should be pointed out that for large kites intended for emergency use, for military or other purposes, the reinforce-v ments. may consist of hollow fabric tubes which are open at their front ends and closed at their rearendsso as to be inflatable by the oncoming wind and maintained in shape thereby. Further, the reinforcement of each edge may consist of a number. of beads strung together and secured along the'edge' so that their mass will provide a degree of stability due to inertia, wi.hout sacrificing flexibility.

Like all kites, our kite obtains its lift from the action of the wind blowing past it. The kite, is maintained at an inclined at -itude relative to the wind, as shown in Fig. 3, by the bridle lines and the weight of the tail. The static pressure of the air on the lower surface of the kite is increased by the airflow and that on the upper surface is decreased, the pressure difference between upper and lower surfaces thereby providing a lift force perpendicular to the wind which supports the k te. Thi sa e; ressu if e ence b tween tional parachute.

upper and lower surfaces, in conjunction with the tension in the lines holds our kite in proper shape to efficiently u.ilize the air current. It is in this latter aspect that our kite distinguishes from those of the prior art, namely, the combination of a suitably flexible body and suitably proportioned bridle lines to effect a degree of arcuateness requisite to effective flight under Widel varying wind conditions.

It is interesting to note the comparison between the principle of our kite and that of the conven- Both structures hold their shapes because of air pressure on a concave surface', but a parachute does not develop lift, it develops only drag, i. e. a force in the direction of the relative wind. Our structure, on the other hand, develops lift, i. e. a force perpendicular to the relative wind due to the wing-like shape in which the kite sections are maintained by'the wind and the bridle lines. Further, we believe theprinciple described herein may be applied to man carrying devices, such as airplanes-,- parachutes and gliders, and in such event stabilizing and control surfaces could be added." We further believe that our principle could be utilized in the constructionof a toy glider or airplane, and-we have met with some experimental success; by at taching a weight in place of the control string 26 and reflexing the. trailing edge-by means of a piece of string between the two ends of the-center line. In this connection itshould be noted that Whatever structure or framework for supporting weights, motors, etc. might be utilized in conjunction with our device, such structure would be hungfrom thekite bodyand not securedto it in a manner which would tendto makethe lifting surface rigid.

An additionalphase of utility of our invention would be the construction of a kite embodying our principle but made of metal foil, either to serve as an antenna or as aradar target.

It will be appreciated that our invention is subject to many modifications Without departing from the spirit thereof and we do not regard ourselves as limited to the specific illustration here-; in, except as set forth in the appended claimsr;

We claim: r I 1 1. .In a'device of the class described the combination of a body of flexible non-rigid material having a center line extending longitudinally thereof, and comprising wing-like sections extending transversely on eitherside of said center line, wherein said center line is eflected-by a crevice at the juncture of said sections and ex.- tends longitudinally the length of said body, and a plurality of bridle strings secured to said sections.- H a y 1 ,v I:

2. ,A kite comprising a body of non-rigid flexible material having a center line effected bythe crevice atthe juncture of symmetrical sectionsof said body, said sections extending outwardly and transversely to forma wing .on eachside of the center line, including a plurality of bridle lines secured to saidsections and symmetrically disposed with respect to said centerline, wherein said bridle lines are connected to each other at a common junctur and are relatively proportioned to effect transverse concavity of said wings in flight, said juncture being disposed relative said wings in flight so as to effect a glide angle there for.

3. A kite comprising a substantially quadrilateral member of flexible non-rigid material having a center line extending diagonally there- .eeipst. rebem a ee i ge s an a a li edge on each side of said center line, and a plurality of bridle lines symmetrically disposed with respect to said center line and secured to respective edges of said quadrilateral member.

4. A kite comprising a substantially quadrilateral member of flexible non-rigid material having a center line extending diagonally thereacross, and a plurality of bridle lines symmetrically disposed with respect to said center line and secured to respective edges of said quadrilateral member, including at least one bridle string secured to said quadrilateral member at said center line.

5. In a device as set forth in claim 3, including a tail member secured to said quadrilateral member and comprising a ribbon-like element having a pair of lines extending therefrom to substantially the midpoints of the trailing edges of said quadrilateral member.

6. A kite comprising a wind supportable body of flexible non-rigid material shaped as a square and having a center line extending diagonally thereacross to divide said body into symmetrical winglike sections, each having a leading and trailing edge, including bridle lines symmetrically disposed and secured to said edges, and a plurality of bridle lines in spaced relation and secured to said body at said center line, said bridle lines having a common juncture at their lower ends whereby a pull may be simultaneously exerted on all bridle lines, the structure being such that in flight the sections are maintained in arcuate shapes substantially symmetrical with respect to the center line due to pressure of the wind acting on their surfaces in conjunction with tensile force exerted on said bridlelines.

7. A kitei'comprising a body member of flexible non-rigid material and having a center line effected by juncture of symmetrical sections of said body extending transversely with respect to the direction of oncoming wind, including a plurality of bridle lines secured to said symmetrical sections and to said body at said center line and having a common juncture, certain of said lines being attached to the outermost portions of said sections, whereby symmetrically arcuate sustaining surfaces are formed in said body member by oncoming wind acting against said sections in conjunction with tensile stress exerted thereon by said bridle lines.

8. In a device as set forth in claim 7, including a tail for said kite, comprising a ribbon-like material and a pair of line secured to said body member symmetrically on opposite sides of said center line, including a swivel joint between said lines and said ribbon like material.

9. In a device as set forth in claim 7, including reinforcements at the edges of said body member and at the center line thereof, said reinforcements being comprised of a, yieldable non-rigid material capable of flexure during flight to a lesser degree than said body material.

GERTRUDE SUGDEN ROGALLO. FRANCIS MELVIN ROGALLO.

REFERENCES CITED The following references are of record in the file of this patent:

UNITED STATES PATENTS Number Name Date 1,029,010 Gulllo June 11, 1912 1,632,822 Dahl June 21, 1927 2,208,786 Astle July 23, 1940 2,258,797 Overbeke Oct. 14, 1941 2,463,135 Bach Mar. 1, 1949

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US1029010 *Dec 23, 1909Jun 11, 1912Forbes Lithograph Mfg CompanyKite.
US1632822 *Jul 17, 1926Jun 21, 1927Robert N BurtonSelf-balancing kite
US2208786 *Dec 3, 1938Jul 23, 1940Astle Percy ThomasKite
US2258797 *Sep 15, 1938Oct 14, 1941Overbeke JohnParachute
US2463135 *May 29, 1947Mar 1, 1949Robert F BachFlying wing kite
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US2737360 *Sep 8, 1950Mar 6, 1956William M AllisonFlexible kite
US2751172 *Nov 17, 1952Jun 19, 1956Rogallo Francis MelvinFlexible kite
US2768803 *Apr 28, 1953Oct 30, 1956Joseph E SmithRotary kite
US3194520 *Oct 5, 1962Jul 13, 1965Daniel C KurkjianKite
US3248075 *Feb 25, 1963Apr 26, 1966Francis V CunninghamKites
US3296617 *Jan 23, 1963Jan 3, 1967Francis M RogalloTarget kite
US3570791 *May 31, 1968Mar 16, 1971Richard R JacksonBattened kite construction
US3697023 *May 12, 1971Oct 10, 1972Richard R JacksonKite
US3949519 *Feb 14, 1975Apr 13, 1976Marvin Glass & AssociatesToy glider
US3994454 *Dec 15, 1975Nov 30, 1976Worsham Lynn MControllable stunt kite having a pair of symmetrical bridles
US4221351 *Apr 13, 1978Sep 9, 1980The Holland CorporationKites
US4892272 *Oct 14, 1988Jan 9, 1990Hadzicki Joseph RKite-like flying device with dual handles and four point control
US5120006 *Jan 8, 1990Jun 9, 1992Hadzicki Joseph RKite-like flying device with independent wing surface control
US5201482 *Oct 30, 1991Apr 13, 1993Ream Stanley MRAM air inflatable gliding wing
US7093803Dec 16, 2003Aug 22, 2006Culp David AApparatus and method for aerodynamic wing
US7336216Apr 18, 2006Feb 26, 2008Rafael Armament Development Authority Ltd.Parachuted radar decoy
US8358027Jul 28, 2008Jan 22, 2013Slingshot Wind Energy Systems Inc.Integrally ribbed Rogallo wing array
USRE30073 *Jun 23, 1977Aug 14, 1979 Controllable stunt kite having a pair of symmetrical bridles
WO2005036941A2 *Oct 4, 2004Apr 28, 2005Rafael Armament Dev AuthorityParachuted radar decoy
WO2007141548A2 *Jun 8, 2007Dec 13, 2007Electromagentic Geoservices AsInstrument for measuring electromagnetic signals
Classifications
U.S. Classification244/153.00R, 342/5, 244/16, 244/902
International ClassificationB64C31/06
Cooperative ClassificationY10S244/902, A63H27/08
European ClassificationA63H27/08