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    • 1. 发明授权
    • Method and apparatus for cooling an airplane engine
    • 用于冷却飞机发动机的方法和装置
    • US5167117A
    • 1992-12-01
    • US631157
    • 1990-12-20
    • Claus HerzogRainer R. SchwabKlaus RudHarald Mark
    • Claus HerzogRainer R. SchwabKlaus RudHarald Mark
    • B64D33/02F02C7/16F02K7/18
    • B64D33/02F02C7/16F02K7/18B64D2033/026Y02T50/671Y02T50/675
    • An apparatus for cooling components of an airplane engine at least partially operated by a cryogenically stored propellant via cooling air includes an air supply line for supplying the cooling air from an outside environment. A heat exchanger exchanges the cooling air with the propellant to precool the cooling air and includes a condenser having an in-flow and an out-flow side connected to the air supply line for precooling the cooling air. A pump is coupled to a cooling air line for conveying the precooled air in a liquid or vapor state to the components to be cooled wherein the cryogenically stored propellant acts upon the condenser. A propellant tank is connected to the in-flow side of the condenser and stores the cryogenically stored propellant, wherein the out-flow side of the condenser is connected to at least one combustion system of the airplane engine.
    • 至少部分由经低温储存的推进剂通过冷却空气操作的用于冷却飞机发动机部件的装置包括用于从外部环境供应冷却空气的空气供应管线。 热交换器将冷却空气与推进剂交换以预冷却冷却空气,并且包括冷凝器,其具有连接到空气供应管线的流入侧和外流侧,用于预冷却冷却空气。 泵耦合到冷却空气管线,用于将液体或蒸气状态的预冷空气输送到要冷却的部件,其中低温储存的推进剂作用在冷凝器上。 推进剂罐连接到冷凝器的流入侧,并存储低温存储的推进剂,其中冷凝器的外流侧连接到飞机发动机的至少一个燃烧系统。