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Propulsion means for hypersonic flight

机译:高超音速飞行的推进手段

摘要

Propulsion means includes at least one ram-let engine 2 and at least one further engine, e.g. a turbo-jet engine 3, the internal flow channel of which is independent of that of the ram-jet engine. Prior to aircraft take-off the flow channel 8 of each ram-jet engine 2 is sealed at both ends (e.g. by flaps 6 and 7) and filled via filling device 11 with a liquid fuel component 10 provided for lower speed range. This fuel is completely removed (e.g. by suctioning off device 12) and used up by the engine(s) 3, operating at lower speed ranges prior to ignition of the ram-jet engines 2. When the ram-jet is operating, flap 6 may seal the turbo-jet engine intake while flap 7 helps determine the thrust trail contour 19. IMAGE
机译:推进装置包括至少一个冲压发动机2和至少一个另外的发动机,例如发动机。涡轮喷气发动机3,其内部流动通道独立于冲压喷气发动机的内部流动通道。在飞机起飞之前,每个冲压喷气发动机2的流道8在两端被密封(例如,通过襟翼6和7),并且经由填充装置11被填充有为较低速度范围提供的液体燃料组分10。该燃料被完全去除(例如,通过抽吸装置12),并被一个或多个发动机3用尽,在冲压喷气发动机2点火之前以较低的速度范围工作。当冲压喷气运行时,襟翼6可以密封涡轮喷气发动机的进气口,同时襟翼7有助于确定推力轨迹轮廓19。

著录项

  • 公开/公告号GB2235249A

    专利类型

  • 公开/公告日1991-02-27

    原文格式PDF

  • 申请/专利权人 * MESSERSCHMITT-BOELKOW-BLOHM GMBH;

    申请/专利号GB19900012648

  • 发明设计人 CHRISTIAN * MUNDT;

    申请日1990-06-06

  • 分类号F02K7/16;

  • 国家 GB

  • 入库时间 2022-08-22 05:48:00

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