公开(公告)号：US4395001A

公开(公告)日：1983-07-26

申请号：US890099

申请日：1978-03-27

申请人： W. James Stone ,  Vernon D. Burklund ,  Robert B. Dillinger ,  Dennis M. Sorges ,  David A. Reeve

发明人： W. James Stone ,  Vernon D. Burklund ,  Robert B. Dillinger ,  Dennis M. Sorges ,  David A. Reeve

IPC分类号： B64D25/10

CPC分类号： B64D25/10

摘要： A line cutter or discharge valve responsive to aircraft attitude is posited on an aircraft ejection seat to interrupt the gas initiated sustainer rocket system. During inverted ejections, the cutter or valve will either sever or discharge pressure from a tube which leads from the firing squib to the sustainer rocket. Preventing sustainer rocket ignition enhances inverted ejection survivability by reducing crew member velocity toward the ground, thereby lengthening the time available for parachute deployment.

摘要翻译： 响应于飞机姿态的线切割器或排出阀定位在飞行器喷射座上以中断气体启动的维持器火箭系统。 在反向喷射过程中，切割器或阀门将会从管道中切断或排出压力，导管从点火点火器引导到持续火箭。 防止持续火箭点火通过降低乘员对地面的速度提高反向弹射生存能力，从而延长降落伞部署时间。