公开(公告)号：US06519928B2

公开(公告)日：2003-02-18

申请号：US09843155

申请日：2001-04-26

申请人： German Munding ,  Wolfgang Müller ,  Joachim Reinecke ,  Peter Gleich

发明人： German Munding ,  Wolfgang Müller ,  Joachim Reinecke ,  Peter Gleich

IPC分类号： C06D504

CPC分类号： F42B10/66

摘要： A process for the production of a transverse thrust in a flying object in which a defined quantity of a monergol propellent substance is introduced into a propulsion unit, which is arranged transversely relative to a longitudinal axis of the flying object to produce a thrust transverse to the longitudinal axis of the flying object. The propulsion unit has a combustion chamber, a supersonic nozzle connected to the combustion chamber and a source of heat to combust the propellant substance and produce the desired thrust for a prescribed time. The monergol propellent substance, introduced tangentially into the combustion chamber to form a film of the propellent substance on an inside surface of a wall of the combustion chamber; and the film of propellent substance on the wall is combusted by a pyrotechnic source of heat arranged in the wall of the combustion chamber in the vicinity of a throat of the supersonic nozzle to produce hot gases by the combustion of the propellant substance and transverse thrust in the supersonic nozzle. An automatically operated non-return valve without moving parts prevents backflow of combustion gases to the inlet valve.

摘要翻译： 一种用于在飞行物体中产生横向推力的方法，其中将限定量的芒果醇推进剂物质引入到推进单元中，该推进单元相对于飞行物体的纵向轴线横向布置以产生横向于 飞行物体的纵轴。 推进单元具有燃烧室，连接到燃烧室的超音速喷嘴和用于燃烧推进剂物质并产生所需推力达规定时间的热源。 所述芒果型推进剂物质切向地引入燃烧室以在燃烧室的壁的内表面上形成推进剂物质的膜; 并且壁上的推进物质膜被布置在燃烧室壁中的烟火源在超音速喷嘴的喉部附近燃烧，以通过推进剂物质的燃烧产生热气体和横向推力 超音速喷嘴。 没有移动部件的自动操作的止回阀防止燃烧气体回流到入口阀。