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Publication numberUS3874855 A
Publication typeGrant
Publication dateApr 1, 1975
Filing dateNov 21, 1973
Priority dateJul 22, 1969
Publication numberUS 3874855 A, US 3874855A, US-A-3874855, US3874855 A, US3874855A
InventorsRobert Legrand
Original AssigneeCegedur Gp
Export CitationBiBTeX, EndNote, RefMan
External Links: USPTO, USPTO Assignment, Espacenet
Composite shock resisting bodies
US 3874855 A
Abstract
A shock resisting composite product characterized by maximum resistance with minimum density formed from a wrought alloy of aluminum having cells formed therein which are packed with a hard material in a compact or fritted condition.
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Description  (OCR text may contain errors)

O United States Patent 1 1 1 1 3,874,855 Legrand Apr. 1, 1975 1 COMPOSITE SHOCK RESISTING BODIES 3.609.855 10/1971 Schmidt 29/191 [75] In ento Robert egmnd, ar s France 3.616.115 10/1971 Kllmmek 89/36 X [73] Assignee: Cegedur GP, Paris, France [22] Filed: 21, 1973 Primary Examiner-L. Dewayne Rutledge Assistant Examiner-M. .l. Andrews l l PP -I 4 3,108 Attorney, Agent, or FirmMcDougall, Hersh & Scott Related US. Application Data [63] Continuation-impart of Scr. No. 843.546. July 23.

1969 abandoned.

[57] ABSTRACT [52] U.S.Cl. ..29/l9l.2, 29/1914, 89/36 Z,

109/84 51 1m. 01. E41B 5/04 A Shock reslstmg composlte Product character'zed by [58] Field of Search. 29/1914, 1912 191 1875. maximum resistance with minimum density formed 89/36 R 36 A, 2: 6 83 from a wrought alloy of aluminum having cells formed therein which are packed with a hard material in a [56] References Cited compact or fritted condition.

UNITEDSTATES PATENTS 3.008.884 l 1/1061 Schippcrcit ct a1 29/1912 2 Claims, 1 Drawing Figure COMPOSITE SHOCK RESISTING BODTES This application is a continuation-in-part of applicants application Ser. No. 843.546 filed on July 22. 1969 now abandoned. and entitled Composite Shock Resisting Bodies and Method.

This invention relates to composite shock resisting products. The invention is particularly concerned with products useful as armor plate or other plate or wall constructions which are subject to high velocity impact by pieces of material. for example. fragments which might be thrown against a wall such as turbine blade pieces.

Shock resisting composite products have been previously produced using hard materials such as fritted materials. The hard materials are held together by means of metal cast about the materials to form the composite body. lt has been considered necessary to use high strength cast materials in order to provide suitable mechanical characteristics. The use of lighter materials such as aluminum or alloys of alulninum has not been considered suitable in view of the relatively weak mechanical characteristics of cast aluminum alloys. Accordingly. the prior art has not taken advantage of the light weight ofthe aluminum whereby low density composite products could be obtained.

lt is an object of this invention to produce shock resisting composite products which have a desired maximum resistance to impact by projectiles and the like while also being characterized by a minimum density.

These and other objects of this invention will appear hereinafter and for purposes of illustration. but not of limitation. specific embodiments of the invention are load at break: limit of elasticity: elongation:

30 to 55 kg/mm' 15 to 45 kg/mm'-' The following alloys are representative of aluminum alloys which provide the desired properties:

a. an alloy of aluminum containing 4.871 zinc. 1.2%

magnesium and 0.271 chromium. the remainder aluminum plus minor impurities;

b. an alloy of aluminum containing 8% zinc, 2.771

magnesium. 1.67: copper. 0.271 chromium. the remainder aluminum plus minor impurities;

c. an alloy of aluminum containing 3.8.7! to 4.971 copper, 1.271 to 1.871 magnesium.0.371 to 0.9% manganese. the remainder aluminum plus impurities.

Aluminum-zinc-magnesium alloys and aluminumcopper-silicon-magnesium alloys 7005 and 2014 are particularly suitable when the aluminum body is formed by forcing the heated aluminum through dies dimensioned in accordance with the desired size of the final product. Typical alloys of this type are set forth in the following tables:

Mn Zn Cu Mg max. 0.70

max. 0.10

max. 0.40

shown in the accompanying drawing in which the FlCL URE is a cross-sectional view of a composite product embodying the features of this invention.

The composite product of this invention generally consists of a main body portion comprising an aluminum alloy in wrought condition. The aluminum body is produced with a plurality of cells formed in the body and in the production of the product. these cells are filled with a hard material such as compacted or fritted products having high hardness characteristics.

The product of the invention is characterized by dimensions which provide a combination of reactions upon the receipt of an impact from a projectile or the like. Specifically, products characterized by the features of the invention have a solid aluminum portion on one side of the cells which is of substantial thickness. The opposite side of the aluminum body is thinner, and if a projectile impact is sustained. this thin part is relatively easily pierced by the projectile. Energy absorption does, however, occur due to the presence of the thin wall. and the balance of the energy of the impact is then absorbed between hard material present in the cells as well as the thick remaining portion of the composite body.

1n the case of 7005 alloys, the following mechanical characteristics are obtained:

elastic limit: break load: elongation:

1n the ease of 2014 alloys. the following mechanical characteristics are obtained:

elastic limit: break load: elongation:

41 to 45 hb 4610 50 hh 8 to 14 "/1 heating. after which they are introduced into the cells.

preferably under pressure. The elements are fixed by gluing (e.g.. an epoxy glue or elastomer) or by introduction in a liquid condition of a low melting alloy.

In the case ofceramic. fritted alumina having a Mohr hardness of 9. boron carbide and tungsten oxides are particularly suitable.

The structures of this invention are particularly useful as armor plate for protection against shells including direct impact therefrom or due to impact from fragments or other objects which engage the plate upon the explosion of a shell. Similar uses such as protective plating and the like surrounding mobile parts. for example turbine blades. are also contemplated whereby any of the adverse effects of any explosions or other occurrences which lead to the impact of the plating by objects can be avoided.

Referring to the accompanying drawings. there is illustrated a cross section of a wrought aluminum alloy having a thickness 1. The body defines a plurality of cells 12 which are filled with a hard material [4. These cells may comprise elongated passages which are formed either by machining or in the processing of the body. for example during an extrusion operation.

The cells 14 comprise from 30 to 50 percent of the cross sectional area of the body. The cells are defined by means of a thin outer wall 16 and a thicker inner wall 18 with side walls 20 dividing the respective cells.

The wall 16 preferably has a thickness of from 10 to percent of the thickness 1. The wall 18 preferably has a thickness 0 of from to 60 percent of the thickness 1.

As indicated. the wall 16 is preferably positioned so that this surface of the body 10 will be exposed to impact. This will. in view of the characteristics of the aluminum. will be rather readily penetrated by a projectile or other object while absorbing a portion of the energy of the impact. Upon engagement with the material in the cells 12, and because of the presence of the thick wall portion 18. the balance ofthe energy ofthe impact will be absorbed. I

Aluminum bodies of the type illustrated in the drawing have been prepared from 7005 alloys with the mechanical characteristics being measured as follows:

elastic limit: 34 hbars Break load: 3) hbars elongation at break: in Z 2014 alloys having the following mechanical characteristics have been successfully tested:

elastic limit: 43 hbars break load: 4) hbars elongation at break: l2 7:

In both instances. the cells of the bodies have been filled with alumina and with boron carbide with the material being held together by means of an epoxy resin by means of an alloy of 607! Sn and 407: Pb or similar low melting point alloy.

Typical dimensions ofa cross section produced in aceordance with the concepts of the invention are as follows (referring to the drawing):

In a typical body of the type described, the thickness 1 will be from 20 to 70 mm. and the interconnecting portions 20 will be from 4 to 6 mm. It will be appreciated. however. that actual dimensions may vary depending upon the application involved. It will also be understood that the over-all size of a plate or other structure can be within any practical range since multiplicity of plates can be secured together by welding.

As noted. the structures of the invention may be extruded. and this is the preferred form of the invention since the passages ofthe body can then be formed autt matically through the use of appropriate mandrels. It is understood that by the use of the term wrought, these extruded bodies. as well as other bodies having a substantially similar structure. are included. The passages may of course be formed or finished by machining where desired.

The products of the invention may comprise an assembly of aluminum bodies of the type described and such assemblies may comprise bodies which are welded together by means of known welding techniques.

The superiority of the wrought aluminum bodies of this invention is dramatic when compared with the properties of cast aluminum bodies. Aluminummagnesium. aluminum-copper. and aluminum-silicon castings are 30 to percent less efficient than wrought bodies prepared in accordance with the concepts of this invention. The particular structural design of the bodies illustrated herein is also of maximum impor tance in achieving the desired results.

lt will be understood that various changes and modifications may be made in the above described invention which provide the characteristics of the invention without departing from the spirit thereof particularly as defined in the following claims.

That which is claimed is:

I. An armor plate comprising a composite product consisting of a wrought aluminum alloy body, a plurality of cells defined by said body. and a material of high hardness filling said cells. said body providing a wall portion subject to impact and adapted to be pierced while absorbing a portion of the energy of the impact. the thickness of said wall portion comprising about l0 to 30 percent of the thickness of said body. said hard material and the remainder of said body absorbing the balance of the energy of the impact. said cells comprising from 30 to 50 percent of the cross sectional area of said body. and said body defining a thick wall portion on the side of said cells opposite said thin wall portion, the thickness of said thick wall portion being from 40 to percent of the thickness of said body.

2. A construction in accordance with claim 1 wherein said hard material comprises at least one of the members selected from the group consisting of an alloy of cobalt, chromium and tungsten. the nitrides and carbides of boron. tungsten and vanadium. steel. silica,

Patent Citations
Cited PatentFiling datePublication dateApplicantTitle
US3008884 *Jul 9, 1958Nov 14, 1961Robert M LangProcess for making neutron-absorbing bodies
US3609855 *Apr 25, 1969Oct 5, 1971Us NavyProduction of beryllium ribbon reinforced composites
US3616115 *Sep 24, 1968Oct 26, 1971North American RockwellLightweight ballistic armor
Referenced by
Citing PatentFiling datePublication dateApplicantTitle
US4005255 *Apr 4, 1975Jan 25, 1977Swiss Aluminium Ltd.Extruded composite section
US4547122 *Oct 14, 1983Oct 15, 1985Aeronautical Research Associates Of Princeton, Inc.Method of containing fractured turbine blade fragments
US4926761 *Sep 9, 1988May 22, 1990Usines Et Acieries De Sambre Et MeuseArmor particularly for a safe and a safe thus produced
US5361678 *Sep 21, 1989Nov 8, 1994Aluminum Company Of AmericaCoated ceramic bodies in composite armor
US5377935 *May 14, 1993Jan 3, 1995Interferometrics Inc.Spacecraft ceramic protective shield
US5445688 *Mar 3, 1994Aug 29, 1995General Electric CompanyMethod of making alloy standards having controlled inclusions
US5616421 *May 18, 1995Apr 1, 1997Aluminum Company Of AmericaMetal matrix composites containing electrical insulators
US5686689 *May 17, 1985Nov 11, 1997Aeronautical Research Associates Of Princeton, Inc.Lightweight composite armor
US7077306 *Nov 26, 2003Jul 18, 2006Cercom, Inc.Ceramic armor and method of making by encapsulation in a hot pressed three layer metal assembly
US8202041Oct 31, 2008Jun 19, 2012Pratt & Whitney Canada CorpFan case for turbofan engine
US8500390May 20, 2010Aug 6, 2013Pratt & Whitney Canada Corp.Fan case with rub elements
US8528457 *Feb 2, 2012Sep 10, 2013Cps Technologies CorpMethod of producing a hybrid tile metal matrix composite armor
US8616113 *Aug 19, 2009Dec 31, 2013Kelly Space & Technology, Inc.Encapsulated ballistic protection system
US8628857 *May 5, 2009Jan 14, 2014Gigi SimovichBallistic plate and method of fabrication thereof
US20100077911 *May 5, 2009Apr 1, 2010Gigi SimovichBallistic plate and method of fabrication thereof
US20120174759 *Aug 19, 2009Jul 12, 2012Gallo Michael JEncapsulated ballistic protection system
US20120180974 *Feb 2, 2012Jul 19, 2012Richard AdamsMethod of producing a hybrid tile metal matrix composite armor
DE3942955A1 *Dec 23, 1989Jul 4, 1991Man Technologie GmbhFrangible armour plate - has plate divided into linear zones with fracture regions of reduced strength
DE4005904A1 *Feb 24, 1990Aug 29, 1991Bayerische Motoren Werke AgProtective armour shield for vehicle - is made from individual ceramic blocks cast into aluminium carrier
EP0260235A2 *Aug 20, 1987Mar 16, 1988Sandvik AktiebolagProtecting plate of compound design and method of manufacturing the same
WO1983003895A1 *May 2, 1983Nov 10, 1983Michel PequignotArmouring plate, particularly for lightened armouring
Classifications
U.S. Classification428/550, 428/702, 428/923, 89/36.11, 428/652, 428/614, 109/84, 428/559, 89/36.2, 428/418, 428/651, 428/627, 428/698, 428/539.5
International ClassificationF41H5/04
Cooperative ClassificationY10S428/923, F41H5/0421, F41H5/0492
European ClassificationF41H5/04H, F41H5/04C2