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    • 10. 发明申请
    • Aircraft auxiliary gas turbine engine and method for operating
    • 飞机辅助燃气轮机及其操作方法
    • US20070175223A1
    • 2007-08-02
    • US11345950
    • 2006-02-02
    • Chellappa BalanKarl Sheldon
    • Chellappa BalanKarl Sheldon
    • F02C7/32
    • B64D41/00B64D2013/0611B64D2041/002F02C7/32F05D2220/50
    • A non-aircraft-propelling auxiliary gas turbine engine installable in an aircraft having a cabin adapted to be pressurized. The auxiliary gas turbine engine includes an auxiliary-gas-turbine-engine compressor having an inlet, wherein the inlet is adapted to receive pressurized air from the cabin. A method for operating a non-aircraft-propelling auxiliary gas turbine engine of an aircraft includes providing pressurized air from the cabin of the aircraft to an inlet of a compressor of the auxiliary gas turbine engine. The method includes providing compressed air from the compressor to a combustor of the auxiliary gas turbine engine and includes providing combustion gases from the combustor to a turbine of the auxiliary gas turbine engine, wherein the turbine is mechanically coupled to the compressor.
    • 可安装在具有适于加压的舱室的飞行器中的非飞机推进辅助燃气涡轮发动机。 辅助燃气涡轮发动机包括具有入口的辅助燃气涡轮发动机压缩机,其中入口适于从舱室接收加压空气。 用于操作飞行器的非飞机推进辅助燃气涡轮发动机的方法包括将来自飞机的舱室的加压空气提供给辅助燃气涡轮发动机的压缩机的入口。 该方法包括将压缩空气从压缩机提供给辅助燃气涡轮发动机的燃烧器,并且包括将来自燃烧器的燃烧气体提供给辅助燃气涡轮发动机的涡轮机,其中涡轮机械地联接到压缩机。