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Publication numberUS1198035 A
Publication typeGrant
Publication dateSep 12, 1916
Filing dateDec 14, 1915
Priority dateDec 14, 1915
Publication numberUS 1198035 A, US 1198035A, US-A-1198035, US1198035 A, US1198035A
InventorsWilliam Caldwell Huntington
Original AssigneeWilliam Caldwell Huntington
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
US 1198035 A
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Description  (OCR text may contain errors)



APPLICATION mio nic.14. 1915.

Patented Sept. 12, 1916.


D STATES -Parenti? vermee.



To all whom, 'it may concern.'

Be it known that I, WILLIAM CALDWELL HUNTINGTON a citizen of the United States,


residing at Ilinsdale, in the county of Dupage and State of Illinois, have invented new and useful Improvements in Projectiles, of which the following is a full, clear, and exact description.

My invention relates to projectiles both for ordnance and smaller ire arms, and particularly anti-air-craft projectiles.

The objects of myl invention are, primarily, to provide a projectile that contains a number of independent parts which are tied together, and which,` when the projectile is discharged from the gun or cannon, separate the length of the wires, chains or other exible sinuate means connecting them and thus covera comparatively large 2@ |area and enables the said parts to tear and break the planes the frame and stays of the air-craft it may strike, so badly, as to incapacitate it for further flight. This I ac complish by the means hereinafter described, and as particularly pointed out in the claims.

In the drawings: Figure 1 is a side view of the projectile embodying my improvements partially inclosed by its casing which is shown in section. Fig. 2 is a transverse section thereof taken on dotted line 2 2,v Fig. 1. 2 Fig. 3 is a diagrammatical view of' said projectile as lit appears when describing its trajectory. Figs. 4, 5 and 6 are, re-

spectively, views similar to Figs. 1, 2`and 3 showlng a modified form of my invention. Figs. 7, 8, and 9 are, respectively, views similar to Figs. 1, 2 and 3 showing another modified form of my invention. Figs. 10, 11 and 12 are, respectively, views similar to Figs. 1, 2 and 3 showing yet another modification of my invention. Figs. 13, 14 and 15 are, respectively, also views similar to Figs. 1, 2 and 3, illustrating a fourth modif fcation of myinvention. Figs. 16, 17 and 18 are, respectively, views similar to Figs. 1, 2 and 3 of a ifth modification of my invention. Y

rlhe preferred form of my invention, shown in the first three figures of the drawings, comprises a substantially cylindrical shell having a conical head and having the diameter of its base reduced. The outer surface of this reduced portion isrslightly tapered from the shoulder a resulting from this reduction to the rear end of the projec- Specieation of Letters Patent. YPatented Sept, 1 2, 1916 Application filed December 14, 1915. Serial No. 66,711. y

to the outer curved surface thereof near the l shoulder a. These tethers are, preferably,

`all ofthe same length and have their other ends securely fastened to a circular anchorplate or diaphragm c near the outer circumference thereof at equal distances apart, and between said diaphragm and their opposite ends said tethers are wound around said Shanks when the sections are in their asf sembled position.

The assembled section 'may be tied to- Y gether in any suitable manner, but I prefer to keep them in their relative positions until red from the gun or cannon by a cylindrical casing D of brass or other' suitable material, the upper, portion of which in-V closes the cylindrical portion of the shell. The base d of this casing is closedand the.

upper side thereof is bored to provide a chamber E which is filled with a suitable explosive, and a time fuse F is tapped through the center of said base into chamber E.

vWhen the shell is` properly placed in itscasing diaphragm c is seated on base d and covers over and closes chamber E, and the Shanks of the sections of the projectile and the tethers occupy the space betweenJ the diaphragm and shoulder a of the same.

When the projectile, hereinbefore described, is fired from a cannon, it will con- ,tinue on its flight until `the fuse F ignites the explosive in chamber E, whereupon it explodes and the sections of the projectile separate and iy apart as they continue at an accelerated speedtoward the air-craft (say) at which they wereaimed and, particularly if the cannon was riied, will revolve about the diaphragm, 'and cover an area twice the length of the tethers and should they strikeythe object tear and break the parts ofsaid aircraft so badly that further Hight thereof is impossible.

In Figs. 4, 5 and 6, I show a modified construction of my invention in which the dia-- phragm is eliminated, and in which the shanks of the sections 15, securely fastened to a ball 16 much less in diameter than stead of one projectile divided into sections,

- contained in achamber covered over by said the casing 17. The sections 15 of thismodi'- ication are secured in casing 17 by pressing the upper edges of the latter into a suit- .casing below the projectile is filled with a suitable explosive 18.

In Figs. 7, 8 and 9, I show another modification of my improvements in which, in-

I employ seven, or any other suitable number of smaller solid bullet. shaped projectiles 19v 19. These bullets are securely held in the upper part of a vcasing 20, similar to that shown in Figs. 1 and 2 Vof the drawings, and the tethers 21 are secured .to the points? of'said bullets and from thence ass down between the same to the space elow the same and above ltheldiaphragm 22 where they are coiled lengthwise the casing and have their lower ends secured equi-distant apart to the diaphragm. The'explosive is diaphragm, and a suitable fuse penetrates through the bottom of this chamber in the same manner as shown in Figs. 1, 2 and 3 of the drawings. In order to provide a point Afor this modified projectile, I have provided a cap 23 of the same shape as the head of the assembled projectile shown in said Figs. 1, 2 and 3, which fits over the upper end of the casing Aand has' its edge lapped over and secured to the upper edge of the same.

In Figs. 10, 11 and 12, I. illustrate yet 'another modification of my improved projectile which is similar in every respect to that shown in Figs. 7, 8 and 9 except that the bullets 24 have Shanks 25 depending therefrom concentrically to their axes and the tethers 26 'thereof have one end connected tov the upper portions of said Shanks 25 and then are wound each around the shank to which it is attached and have their opposite ends hunched and tied securely together in any suitable manner, independently of the diaphragm.

In Figs. 13, 14 and 15 of the drawings, I

show a modification which differs from that' shown in said Figs. 10, 11 and 12 only in the shape of the bullets 27, 27. These bullets are pointed at both ends and their tethers 28 are attached to their lower points and are loosely coiled in the s ace between the bullets and above the diap ragm, and have directly around the -bodies of said sections. The tethering'wires 30, 30 of this modification have their ends opposite those attached to said sections tied together; the diaphragm 31 is nnt seated upon thev base, but simply /separates the lower portion of the bore of the casing 23 in which the explosive 33 is contained from the upper portion of the same, and the casing is provided with a cap L 34 similar to that shown in Figs. 7, 8 and 9 of the drawings. It will be'understood that in the manufacture of my invention, v'I will utilize all the means for improving the same that have been developed by' recent advances in the science of ordnance and projectiles" to which my invention belongs. All such changes as may be requiredin order to enable me to do this, I desire to beunderstood as coming within the scope. of my i11- vention.

What I claim as`ne`w is: 1. In combination, a projectileA divided longitudinally in sections, and flexible means which by being wound around the projectile hold the sections `together n ormally and also formconnecting members between the ,sections after said sections have separated.

2. In combinationfj a' projectile divided longitudinally into separable sections-having their rear ends reduced, and means wound upon the exterior of said reduced ends to bind said sections together when asin which the base of said projectile and said sinuate connecting means are retained.

5. In combinatlon, a projectile comprising a number of corresponding parts nested around the axis thereof, flexlble sinuate means for connecting-said parts, a common element distinct from the parts of the projectile to which said sinuate means are connected, and a shell in which the base of said parts, said sinuate means `and said common element are inclosed. e

6. In combination, a rojectilel divided longitudinally and centra y into a suitable number of corresponding sections nested around a common axis, and iexible sinuate means coiled around the ends of and connecting dilerent sections.

' 7. In combination, a projectile divided longitudinally into a sultable number of corresponding sections, each having a shank .of transversely reduced dimensions, and

flexible sinuate tethers the ends of which are connected to said Shanks, and between their ends are coiled upon said Shanks.

8. In combination, a projectile divided longitudinally and centrally into a suitablel number of corresponding'sections each having a shank of reduced transverse dimensions, flexible sinuate tethers the endsfof which are connected to said sections, and a common coupling element to which said tethers are connected and between which 1I WILLIAM CALDWELL HUNTINGTON.



Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US3085510 *Aug 11, 1960Apr 16, 1963Campbell John KPattern control for buckshot charges
US4664034 *Apr 23, 1985May 12, 1987Christian Dale WFettered shot
US5315932 *May 25, 1993May 31, 1994Bertram Charles HProjectile system incorporated into a shot shell
US5750918 *Oct 17, 1995May 12, 1998Foster-Miller, Inc.Ballistically deployed restraining net
US6910423Jun 6, 2003Jun 28, 2005Raytheon CompanyKinetic energy rod warhead with lower deployment angles
US6920827Oct 31, 2003Jul 26, 2005Raytheon CompanyVehicle-borne system and method for countering an incoming threat
US6931994Nov 21, 2002Aug 23, 2005Raytheon CompanyTandem warhead
US6973878Jun 5, 2003Dec 13, 2005Raytheon CompanyWarhead with aligned projectiles
US7017496Mar 10, 2003Mar 28, 2006Raytheon CompanyKinetic energy rod warhead with imploding charge for isotropic firing of the penetrators
US7143698May 13, 2005Dec 5, 2006Raytheon CompanyTandem warhead
US7412916Jan 18, 2006Aug 19, 2008Raytheon CompanyFixed deployed net for hit-to-kill vehicle
US7415917 *Mar 10, 2003Aug 26, 2008Raytheon CompanyFixed deployed net for hit-to-kill vehicle
US7441511Feb 27, 2006Oct 28, 2008Foster-Miller, Inc.Watercraft arresting system
US7621222Feb 17, 2005Nov 24, 2009Raytheon CompanyKinetic energy rod warhead with lower deployment angles
US7624682Feb 17, 2005Dec 1, 2009Raytheon CompanyKinetic energy rod warhead with lower deployment angles
US7624683Jul 20, 2005Dec 1, 2009Raytheon CompanyKinetic energy rod warhead with projectile spacing
US7717042Jan 6, 2005May 18, 2010Raytheon CompanyWide area dispersal warhead
US7726244Jul 20, 2007Jun 1, 2010Raytheon CompanyMine counter measure system
US7866250Feb 9, 2006Jan 11, 2011Foster-Miller, Inc.Vehicle protection system
US7900548Aug 8, 2007Mar 8, 2011Foster Miller, Inc.Protection system including a net
US8011285Apr 14, 2009Sep 6, 2011Foster-Miller, Inc.Vehicle and structure shield
US8042449Aug 19, 2010Oct 25, 2011Foster-Miller, Inc.Vehicle protection system
US8127686Jul 20, 2005Mar 6, 2012Raytheon CompanyKinetic energy rod warhead with aiming mechanism
US8141470Apr 28, 2011Mar 27, 2012Foster-Miller, Inc.Vehicle protection method
US8141493Nov 2, 2010Mar 27, 2012Todd KuchmanProjectile for use with a rifled barrel
US8245620Mar 30, 2011Aug 21, 2012QinetiQ North America, Inc.Low breaking strength vehicle and structure shield net/frame arrangement
US8245621Jul 27, 2011Aug 21, 2012Qinetiq North AmericaVehicle and structure shield
US8245622Jul 27, 2011Aug 21, 2012QinetiQ North America, Inc.Vehicle and structure shield method
US8281702Sep 28, 2011Oct 9, 2012Foster-Miller, Inc.Protection system
US8418623Apr 2, 2010Apr 16, 2013Raytheon CompanyMulti-point time spacing kinetic energy rod warhead and system
US8443709Sep 8, 2010May 21, 2013QinetiQ North America, Inc.Vehicle and structure shield hard point
US8453552Aug 16, 2011Jun 4, 2013QinetiQ North America, Inc.Method of designing an RPG shield
US8464627Nov 14, 2011Jun 18, 2013QinetiQ North America, Inc.Vehicle and structure shield with improved hard points
US8468927Sep 22, 2011Jun 25, 2013QinetiQ North America, Inc.Vehicle and structure shield with a cable frame
US8539875Aug 28, 2012Sep 24, 2013Foster-Miller, Inc.Protection system
US8607685Nov 14, 2011Dec 17, 2013QinetiQ North America, Inc.Load sharing hard point net
US8615851Apr 12, 2011Dec 31, 2013Foster-Miller, Inc.Net patching devices
US8677882Aug 15, 2012Mar 25, 2014QinetiQ North America, Inc.Vehicle and structure shield with flexible frame
US8733225Sep 21, 2012May 27, 2014QinteiQ Nörth America, Inc.RPG defeat method and system
WO2007100835A2 *Feb 27, 2007Sep 7, 2007Michael D FarinellaWatercraft arresting system
WO2012033513A1 *Aug 19, 2011Mar 15, 2012Foster-Miller, Inc.Vehicle and structure shield net/frame arrangement
WO2012060822A1 *Nov 2, 2010May 10, 2012Advanced Ballistic Concepts LlcProjectile for use with a rifled barrel
WO2012064313A1 *Nov 9, 2010May 18, 2012Sexton Richard FMethod for the simultaneous dispersion of projectiles
U.S. Classification102/504
Cooperative ClassificationF42B12/66