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US07418821B2 Aircraft gas turbine engines 失效
飞机燃气涡轮发动机

Aircraft gas turbine engines
摘要:
An aircraft gas turbine engine including a first hydraulic pump connected to a starter motor and a second hydraulic pump connected to the high-pressure compressor. The engine being arranged such that during starting the starter motor drives the first pump, to pump hydraulic fluid to operate the second pump as a motor to drive the high pressure compressor. During running the first and second pumps are connected to the aircraft hydraulic system.
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