Reactive material enhanced projectiles, devices for generating reactive material enhanced projectiles and related methods
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F42B-001/028
F42B-001/032
F42B-012/10
출원번호
US-0510017
(2009-07-27)
등록번호
US-8443731
(2013-05-21)
발명자
/ 주소
Stecher, Frederick P.
Truitt, Richard M.
출원인 / 주소
Alliant Techsystems Inc.
대리인 / 주소
TraskBritt
인용정보
피인용 횟수 :
2인용 특허 :
21
초록▼
A liner assembly for an explosively formed projectile device may include a reactive material liner and a primary liner configured to form into a projectile responsive to initiation of an explosive material. The reactive material liner may be configured and formulated to increase the velocity of the
A liner assembly for an explosively formed projectile device may include a reactive material liner and a primary liner configured to form into a projectile responsive to initiation of an explosive material. The reactive material liner may be configured and formulated to increase the velocity of the projectile after formation thereof. An ordnance device for generating an explosively formed projectile may include a case, an explosive material, and a reactive material liner and a primary liner configured, in combination, to form into a projectile. An explosively formed projectile may include a deformed primary liner and a deformed reactive material liner having an ignited portion increasing the velocity of the projectile. Methods of explosively forming a projectile may include explosively expelling a primary liner and a secondary liner and increasing the velocity of the projectile by combusting at least a portion of the secondary liner.
대표청구항▼
1. A liner assembly for use with a device for forming an explosively formed projectile, the liner assembly comprising: a reactive material liner comprising a reactive material;a primary liner configured to, upon initiation of an explosive material used to form an explosively formed projectile, defor
1. A liner assembly for use with a device for forming an explosively formed projectile, the liner assembly comprising: a reactive material liner comprising a reactive material;a primary liner configured to, upon initiation of an explosive material used to form an explosively formed projectile, deform into an outer portion of the projectile at least partially surrounding a portion of the reactive material liner and wherein at least a portion of the reactive material liner is configured and formulated to increase a velocity of the projectile in excess of a velocity generated by the explosive material; anda control liner comprising a control material, the control liner disposed on at least a portion of the reactive material liner and wherein the control liner is configured and formulated to, upon initiation of the explosive material used to form the explosively formed projectile, deform into a posterior portion of the projectile and to at least partially control a rate of reaction of an ignited portion of the reactive material liner. 2. The liner assembly of claim 1, wherein the primary liner is configured and formulated to, upon initiation of the explosive material used to form the explosively formed projectile, deform into a substantially elongated shaped outer portion of the projectile. 3. The liner assembly of claim 2, wherein the reactive material liner is configured and formulated to deform into a central portion of the projectile. 4. The liner assembly of claim 1, wherein the primary liner is disposed over at least a portion of the reactive material liner and wherein the primary liner and the reactive material liner are each formed to have a substantially curved shape. 5. The liner assembly of claim 1, wherein the primary liner comprises copper material. 6. The liner assembly of claim 5, wherein the reactive material liner comprises a metal material selected from at least one of tungsten, zirconium, aluminum, and nickel. 7. The liner assembly of claim 6, wherein the reactive material liner further comprises an oxidizer material selected from at least one of potassium perchlorate, potassium nitrate, ammonium perchlorate, and cupric oxide. 8. The liner assembly of claim 1, further comprising: a buffer liner comprising a buffer material at least partially disposed on the reactive material liner and configured to, upon initiation of the explosive material used in the explosively formed projectile, deform into a central portion of the projectile; andan additional reactive material liner comprising an additional reactive material disposed on at least a portion of the buffer liner and configured and formulated to, upon initiation of the explosive material used to form the explosively formed projectile, deform into the central portion of the projectile and wherein the buffer liner is configured to at least partially separate the reactive material liner and the additional reactive material liner. 9. The liner assembly of claim 1, wherein at least a portion of the reactive material liner is configured and formulated to ignite when the reactive material liner is deformed. 10. The liner assembly of claim 9, wherein the primary liner is configured to deform into the outer portion of the projectile exposing a portion of the reactive material liner at a posterior end of the projectile. 11. The liner assembly of claim 10, wherein the reactive material liner is configured and formulated to form a propulsive jet created by the ignition of the reactive material liner to increase the velocity of the projectile. 12. An ordnance device for generating an explosively formed projectile comprising: a case;an explosive material at least partially disposed within the case;a reactive material liner comprising a reactive material at least partially disposed within the case; anda primary liner at least partially disposed within the case and abutting at least a portion of a surface of the reactive material liner, the primary liner configured to deform into an outer portion of a projectile at least partially surrounding a portion of the reactive material liner responsive to initiation of the explosive material, and wherein at least a portion of the reactive material liner is configured and formulated to increase a velocity of the projectile in excess of a velocity generated by the explosive material after the projectile has been expelled from the case. 13. The ordnance device of claim 12, wherein the explosive material is configured and formulated to propel the projectile formed by the reactive material liner and the primary liner from the case at a first initial velocity and a portion of the reactive material liner is configured and formulated to accelerate the projectile to a second, increased velocity. 14. The ordnance device of claim 13, wherein the second, increased velocity is at least 10% greater than the first initial velocity. 15. The ordnance device of claim 12, wherein at least a portion of the reactive material liner is configured and formulated to ignite upon being explosively expelled from the case. 16. The ordnance device of claim 12, further comprising a control liner comprising a control material, the control liner at least partially disposed within the case and at least partially disposed between the reactive material liner and the explosive material and wherein the control liner is configured to deform into a posterior portion of the projectile after being explosively expelled from the case and to at least partially control a rate of reaction of a portion of the reactive material liner. 17. An explosively formed projectile comprising: a deformed primary liner substantially forming an outer portion of the projectile; anda deformed reactive material liner at least partially disposed within the deformed primary liner and wherein an ignited portion of the deformed reactive material liner increases a velocity of the projectile in excess of a velocity generated by an explosive material used to form the projectile. 18. The explosively formed projectile of claim 17, wherein the deformed reactive material liner forms a portion of a central portion of the projectile. 19. The explosively formed projectile of claim 18, further comprising a deformed control liner forming a posterior portion of the projectile and at least partially surrounding a portion of the deformed reactive material liner, the deformed control liner at least partially controlling a rate of reaction of the ignited portion of the deformed reactive material liner. 20. The explosively formed projectile of claim 19, further comprising: a deformed buffer liner forming at least a portion of the central portion of the projectile; andan additional deformed reactive material liner forming at least a portion of an anterior portion of the projectile, wherein the deformed buffer liner at least partially separates the deformed reactive material liner and the additional deformed reactive material liner. 21. A method of explosively forming a projectile with the liner assembly of claim 1, the method comprising: explosively expelling the primary liner and the reactive material liner from a case;deforming the primary liner to at least partially surround a portion of the reactive material liner; andincreasing a velocity of the projectile by combusting at least a portion of the reactive material liner. 22. The method of claim 21, further comprising igniting a portion of the reactive material liner as the reactive material liner is explosively expelled from the case.
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이 특허에 인용된 특허 (21)
Rönn, Torsten; Thuman, Christer, Device adjacent to an explosive charge with at least two liners.
Thompson, LaMar; Ng, William; Fong, Richard, Single stage kinetic energy warhead utilizing a barrier-breaching projectile followed by a target-defeating explosively formed projectile.
Stecher, Frederick P.; Truitt, Richard M., Reactive material enhanced projectiles, devices for generating reactive material enhanced projectiles and related methods.
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