IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0128580
(2005-05-13)
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등록번호 |
US-7387072
(2008-06-17)
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발명자
/ 주소 |
- Hunn,David L.
- Milam,Ben T.
- Havens,Kenneth W.
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출원인 / 주소 |
- Lockheed Martin Corporation
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대리인 / 주소 |
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인용정보 |
피인용 횟수 :
1 인용 특허 :
10 |
초록
▼
A fluid jet apparatus includes a housing defining a propellant cavity, a fluid cavity, and a passage through the housing in fluid communication with the fluid cavity. The apparatus further includes a membrane separating the propellant cavity and the fluid cavity, a propellant disposed in the propell
A fluid jet apparatus includes a housing defining a propellant cavity, a fluid cavity, and a passage through the housing in fluid communication with the fluid cavity. The apparatus further includes a membrane separating the propellant cavity and the fluid cavity, a propellant disposed in the propellant cavity, and a fluid retained in the fluid cavity. The propellant urges the fluid from the fluid cavity through the passage upon initiation of the propellant. A munition system includes a munition and at least one fluid jet apparatus adapted to vent the munition. A method includes initiating a propellant to produce a rapidly expanding gas and urging a fluid through a passageway with the gas to produce a fluid jet.
대표청구항
▼
What is claimed is: 1. A munition system, comprising: a munition; and at least one fluid jet apparatus external to said munition and adapted to vent the munition, the at least one fluid jet apparatus comprising: a housing defining a propellant cavity, a fluid cavity, and a passage through the housi
What is claimed is: 1. A munition system, comprising: a munition; and at least one fluid jet apparatus external to said munition and adapted to vent the munition, the at least one fluid jet apparatus comprising: a housing defining a propellant cavity, a fluid cavity, and a passage through the housing in fluid communication with the fluid cavity; a breachable membrane separating the propellant cavity and the fluid cavity; a propellant disposed in the propellant cavity; and a fluid retained in the fluid cavity, wherein the propellant urges the fluid from the fluid cavity through the passage upon initiation of the propellant. 2. The munition system according to claim 1, further comprising: an initiator for initiating the propellant. 3. The munition system according to claim 2, wherein the initiator is an electrical initiator. 4. The munition system according to claim 2, wherein the initiator is a thermal initiator. 5. The munition system according to claim 2, wherein the initiator comprises: at least one of Cs2B12H12/BKNO3, lead azide, hexanitrostilbene (HNS), and ammonium perchlorate. 6. The munition system according to claim 2, further comprising: a booster disposed between the initiator and the propellant. 7. The munition system according to claim 6, wherein the booster is more energetic than the initiator and comprises: at least one of Cs2B12H12/BKNO3, lead azide, hexanitrostilbene (HNS), and ammonium perchlorate. 8. The munition system according to claim 1, wherein the passage extends obliquely through the housing. 9. The munition system according to claim 1, wherein the passage extends normally through the housing. 10. The munition system according to claim 1, wherein the propellant comprises: at least one of gunpowder, black powder, an explosive mixture of ammonium perchlorate, an explosive mixture of perchlorate, an explosive mixture of potassium nitrate, and a pyrotechnic composition. 11. The munition system according to claim 1, wherein the fluid comprises: at least one of water, a combination of water and alcohol, a combination of water and ethylene glycol, a combination of water and propylene glycol, a combination of water and methyl cellulose, a combination of water and methacrylamide, ammonia, and a combination of water and ammonia. 12. The munition system according to claim 1, wherein the fluid includes abrasive particles. 13. The munition system according to claim 1, further comprising: a jewel disposed in the passage and defining an orifice therethrough. 14. The munition system according to claim 1, wherein the passage is a slot. 15. The munition system according to claim 1, wherein the at least one includes a plurality of fluid jet apparatuses operably associated with the munition. 16. The munition system according to claim 1, wherein the at least one includes a plurality of fluid jet apparatuses disposed generally along a length of the munition. 17. The munition system according to claim 1, wherein the at least one fluid jet apparatus is adapted to produce a slot in the munition when the fluid jet apparatus is activated. 18. The munition system according to claim 1, wherein the at least one fluid jet apparatus is disposed relative to the munition such that a fluid jet produced by the fluid jet apparatus impinges the munition at an oblique angle when the fluid jet apparatus is activated. 19. The munition system according to claim 1, further comprising: a sabot in which the fluid jet apparatus is disposed.
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