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    • 1. 发明申请
    • GAS GENERATING EJECT MOTOR
    • 燃气发电机
    • WO0034731A3
    • 2000-10-12
    • PCT/US9926455
    • 1999-11-10
    • CORDANT TECH INCDOLL DANIEL WLUND GARY KHUGHES CRAIG DHALL MARC AMACON DAVID J
    • DOLL DANIEL WLUND GARY KHUGHES CRAIG DHALL MARC AMACON DAVID J
    • C06D5/06F02K9/10F02K9/36F02K9/76F02K9/95F42B3/04F42B5/10
    • C06D5/06F02K9/10F02K9/36F02K9/763F02K9/95F42B3/04F42B5/105
    • A gas generating eject motor (10) includes a case (12) containing an ignitable low temperature gas generant material (24) that does not produce toxic gases upon the combustion thereof. The gas generant material is generally contained with a screen enclosure (26, 30) housed within the case. An igniter (70) is disposed within the gas generant material for selectively igniting the gas generant to thereby generate combustion gases. A nozzle (40) is disposed within an open aft end of the case for focusing and directing the combustion gases generated by the ignited gas generant material. The case is constructed and arranged to be separaly attached to the aft end of a rocket (90) to be launched from a launch platform (80), so that, upon ignition of the gas generant, the combustion gases focused by the nozzle will apply a thrust to the rocket and thereby propel, or eject, the rocket from the launch platform, at which time the combustible propellant of the rocket motor will ignite and the eject motor will be separated from the rocket.
    • 气体发生喷射电动机(10)包括容纳可燃低温气体发生剂材料(24)的壳体(12),其在其燃烧时不产生有毒气体。 气体发生剂材料通常包含容纳在壳体内的筛网外壳(26,30)。 点火器(70)设置在气体发生剂材料内,用于选择性地点燃气体发生剂从而产生燃烧气体。 喷嘴(40)设置在壳体的开口后端,用于聚焦和引导由点燃气体发生剂材料产生的燃烧气体。 壳体被构造和布置成分离连接到从发射平台(80)发射的火箭(90)的后端,使得当燃气发生器点燃时,由喷嘴聚焦的燃烧气体将应用 推动火箭从而推动或弹出火箭从发射平台,此时火箭发动机的可燃推进剂将点燃,弹出电机将与火箭分离。