Repeatable plasma generator and a method therefor
원문보기
IPC분류정보
국가/구분
United States(US) Patent
등록
국제특허분류(IPC7판)
F41A-019/63
F41A-019/60
F42B-003/14
F42B-005/08
F42C-019/12
H05H-001/52
F42C-019/08
출원번호
US-0993585
(2011-11-30)
등록번호
US-9377261
(2016-06-28)
우선권정보
SE-1001194 (2010-12-15)
국제출원번호
PCT/SE2011/000217
(2011-11-30)
§371/§102 date
20131126
(20131126)
국제공개번호
WO2012/082039
(2012-06-21)
발명자
/ 주소
Aberg, Denny
Olsson, Fredrik
출원인 / 주소
BAE Systems Bofors AB
대리인 / 주소
Polsinelli PC
인용정보
피인용 횟수 :
0인용 특허 :
6
초록▼
The invention concerns a method for repeatable ignition of propellant charges in a weapon system, e.g. for firing shells from a barrel weapon, through electrical discharge in a combustion chamber duct (3) containing a combustion chamber substance (30), wherein the filling gas in the combustion chamb
The invention concerns a method for repeatable ignition of propellant charges in a weapon system, e.g. for firing shells from a barrel weapon, through electrical discharge in a combustion chamber duct (3) containing a combustion chamber substance (30), wherein the filling gas in the combustion chamber duct (3) is ionized by the high-voltage potential applied to the ionizing electrode (7), which is connected to a first high-voltage generator (2), thus increasing the electrical conduction capacity in the combustion chamber duct (3) such that an electrical sparkover through electrical discharge via a second high-voltage generator (5) between a rear electrode (22) and a front electrode (21) is generated and produces an effect, with subsequent ionization of the surface of the combustion chamber substance (30), which causes hot gas in a plasma-like state to be expelled from the combustion chamber duct (3). The invention also concerns a plasma generator therefor, and an ammunition unit containing said plasma generator.
대표청구항▼
1. Plasma generator for repeatable ignition of propellant charges in a weapon system through electrical discharge in a combustion chamber enclosure containing a combustion chamber duct and a combustion chamber substance configured in connection with a combustion charge, wherein the plasma generator
1. Plasma generator for repeatable ignition of propellant charges in a weapon system through electrical discharge in a combustion chamber enclosure containing a combustion chamber duct and a combustion chamber substance configured in connection with a combustion charge, wherein the plasma generator contains an ionization electrode connected to a first high-voltage generator for ionization of a filling gas in the combustion chamber duct for producing an electrically conductive gas and a front electrode connected to an electrical ground and a rear electrode electrically connected to a second high-voltage generator configured for electrical discharge in the electrically conductive gas so that hot ignition gas is formed under high pressure. 2. Plasma generator according to claim 1, wherein the electrical discharge from the second high-voltage generator takes place when the conduction capacity in the combustion chamber duct is sufficient to generate electrical sparkover. 3. Plasma generator according to claim 2, wherein ionization of the combustion chamber substance is synchronized with the electrical discharge from the second high-temperature generator so that the electrical discharge via the second high-voltage generator does not take place until the ionization voltage reaches its voltage maximum or 100 μβ before or after the voltage maximum calculated from the voltage maximum. 4. Plasma generator according to claim 2, wherein the ionizing electrode is solidly configured on the combustion chamber substance-, with the ionizing electrode being electrically insulated from the combustion chamber duct and electrically connected to the first high-voltage generator via a passage that is electrically insulated from the combustion chamber enclosure. 5. Plasma generator according to claim 2, wherein the ionizing electrode is solidly configured on the combustion chamber substance, with the ionizing electrode being in open contact against the combustion chamber duct and electrically connected to the first high-voltage generator via a passage that is electrically insulated from the combustion chamber enclosure. 6. Plasma generator according to claim 2, wherein the rear electrode configured at the rear end of the combustion chamber duct is electrically connected to the other high-voltage generator, in that there is a front electrode configured at the front end of the combustion chamber duct, said back and front electrodes being composed of an electrically conductive material, and in that that a gas outlet that leads out towards the propellant charge is configured in the front electrode. 7. Plasma generator according to claim 1, wherein ionization of the combustion chamber substance is synchronized with the electrical discharge from the second high-temperature generator so that the electrical discharge via the second high-voltage generator does not take place until the ionization voltage reaches its voltage maximum or 100 μβ before or after the voltage maximum calculated from the voltage maximum. 8. Plasma generator according to claim 7, wherein the ionizing electrode is solidly configured on the combustion chamber substance, with the ionizing electrode being electrically insulated from the combustion chamber duct and electrically connected to the first high-voltage generator via a passage that is electrically insulated from the combustion chamber enclosure. 9. Plasma generator according to claim 7, wherein the ionizing electrode is solidly configured on the combustion chamber substance, with the ionizing electrode being in open contact against the combustion chamber duct and electrically connected to the first high-voltage generator via a passage that is electrically insulated from the combustion chamber enclosure. 10. Plasma generator according to claim 1, wherein the ionizing electrode is solidly configured on the combustion chamber substance, with the ionizing electrode being electrically insulated from the combustion chamber duct and electrically connected to the first high-voltage generator via a passage that is electrically insulated from the combustion chamber enclosure. 11. Plasma generator according to claim 10, wherein the ionizing electrode is solidly configured on the combustion chamber substance, with the ionizing electrode being in open contact against the combustion chamber duct and electrically connected to the first high-voltage generator via a passage that is electrically insulated from the combustion chamber enclosure. 12. Plasma generator according to claim 1, wherein the ionizing electrode is solidly configured on the combustion chamber substance, with the ionizing electrode being in open contact against the combustion chamber duct and electrically connected to the first high-voltage generator via a passage that is electrically insulated from the combustion chamber enclosure. 13. Plasma generator according to claim 1, wherein the rear electrode configured at the rear end of the combustion chamber duct is electrically connected to the other high-voltage generator, in that there is a front electrode configured at the front end of the combustion chamber duct, said back and front electrodes being composed of an electrically conductive material, and in that that a gas outlet that leads out towards the propellant charge is configured in the front electrode. 14. Plasma generator according to claim 13 wherein the gas outlet is conical. 15. Plasma generator according to claim 1, wherein the combustion chamber substance is tubular and contains a polymer material having a resistivity exceeding 100 ohm-meters. 16. Plasma generator according to claim 1, wherein the combustion chamber substance is divided into several layers. 17. Plasma generator according to claim 1, wherein the combustion chamber substance contains a mixture of polymer and metallic material. 18. Plasma generator according to claim 1, wherein the rear electrode configured at the rear end of the combustion chamber duct is electrically connected to the other high-voltage generator, in that there is a front electrode configured at the front end of the combustion chamber duct, said back and front electrodes being composed of an electrically conductive material, and in that that a gas outlet that leads out towards the propellant charge is configured in the front electrode. 19. Ammunition unit containing a shell casing, a projectile, a propellant charge, and an ignition device wherein said ignition device comprises a plasma generator according to claim 1.
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이 특허에 인용된 특허 (6)
Chryssomallis George (Golden Valley MN) Griffing Robert S. (Andover MN), Combustion augmented plasma pressure amplifier.
Goldstein Yeshayahu S. A. (Gaithersburg MD) Tidman Derek A. (Silver Spring MD) Massey Dennis W. (Manassas VA) Greig Joseph R. (Greenbelt MD), High-pressure having plasma flow transverse to plasma discharge particularly for projectile acceleration.
Goldstein Yeshayahu S. A. (Gaithersburg MD) Tidman Derek A. (Silver Spring MD) Burton Rodney L. (Fairfax Station VA) Massey Dennis W. (Manassas VA) Winsor Niels K. (Alexandria VA), Plasma propulsion apparatus and method.
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