|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||F02K-009/26 B60R-021/264 F02K-009/95 F02K-009/94 F42C-019/08 B60R-021/26|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 7|
Electrical ignition of electrically operated propellant in a gas generation system provides an ignition condition at an ignition surface between a pair of electrodes that satisfies three criteria of a current density J that exhibits a decreasing gradient along an axis normal to an ignition surface, is substantially constant across the ignition surface and exceeds an ignition threshold at the ignition surface. These criteria may be satisfied by one or more of an angled electrode configuration, a segmented electrode configuration or an additive to the elec...
1. A gas generation system, comprising: a combustion chamber;an electrically operated propellant within the combustion chamber; anda pair of electrodes configured for coupling with an electrical power source, said electrical power source configured to apply an electrical input across the electrodes creating an ignition condition in which (a) a current density (J) through the propellant between the pair of electrodes on an ignition surface exhibits a decreasing gradient along an axis normal to the ignition surface, (b) a contour of the ignition surface ap...