会员体验
专利管家(专利管理)
工作空间(专利管理)
风险监控(情报监控)
数据分析(专利分析)
侵权分析(诉讼无效)
联系我们
交流群
官方交流:
QQ群: 891211   
微信请扫码    >>>
现在联系顾问~
热词
    • 1. 发明授权
    • Combination propulsion system for a flying craft
    • 飞行器组合推进系统
    • US5014508A
    • 1991-05-14
    • US494990
    • 1990-03-16
    • Hans Lifka
    • Hans Lifka
    • B64G1/00B64G1/40F02C3/073F02C3/13F02K3/072F02K7/16F02K7/18F02K9/48F02K9/74F02K9/78
    • B64G1/401F02C3/073F02C3/13F02K3/072F02K7/16F02K7/18F02K9/78B64G1/402
    • A combination engine for a flying craft capable of flying at speeds within a wide range from subsonic speeds to hypersonic speeds, is equipped with a rocket engine section that is independent of an atmospheric air supply, and a turbo air jet engine section having a compressor which is driven by a turbine that is also independent of an external air supply. The combination may further include extra fuel supply nozzles for operation as a ram jet which uses the same flow channel as the turbo air jet engine section. A gas generator equipped with two valving mechanisms is arranged coaxially with the rocket engine section. The valving mechanisms are controllable to open the gas generator chamber to the rocket combustion chamber while closing off gas flow to the turbo air jet section or vice versa. Either section can work alone or in parallel and simultaneously with the other section. Each turbine wheel forms with one compressor wheel a free wheeling rotor without any intermediate guide wheels, whereby the turbine blades extend either radially inwardly or radially outside of the compressor blades. A gas mixer or distributor is arranged downstream of the turbine and leads into the combustion chamber of the turbo or ram jet section to mix external air with the turbine propellant gases.
    • 用于能够以亚音速到超音速的广泛范围内飞行的飞行器的组合引擎配备有独立于大气供应的火箭发动机部分和具有压缩机的涡轮喷气发动机部分 由涡轮机驱动,涡轮机也独立于外部空气供应。 该组合可以进一步包括用作作为涡轮喷气发动机部分使用相同流动通道的冲压喷射器的额外的燃料供应喷嘴。 配备有两个阀机构的气体发生器与火箭发动机部分同轴布置。 阀门机构是可控制的,以将气体发生器室打开到火箭燃烧室,同时关闭到涡轮空气喷射部分的气流,反之亦然。 任何一个部分可以单独工作或与其他部分并行工作。 每个涡轮机叶轮与一个压缩机叶轮一起形成一个没有任何中间导向轮的空转轮,由此涡轮机叶片在压缩机叶片的径向向内或径向外延伸。 气体混合器或分配器布置在涡轮机的下游,并进入涡轮或冲压射流部分的燃烧室,以将外部空气与涡轮推进剂气体混合。