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SERVO FLOW RECIRCULATION FOR AN ADVANCED THERMAL EFFICIENT AIRCRAFT ENGINE FUEL SYSTEM
SERVO FLOW RECIRCULATION FOR AN ADVANCED THERMAL EFFICIENT AIRCRAFT ENGINE FUEL SYSTEM
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机译:先进热效率飞机发动机燃油系统的伺服流再循环
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摘要
A fuel circulation system and methods are provided. The system includes a supply pump for providing an outlet flow of fuel. The system also includes at least a first and a second servo. The first servo is connected to an outlet of the supply pump. A flow regulation device is interposed between the first and second servos. At least a portion of the outlet flow from the supply pump is directed through the first servo, flow regulation device, and second servo and is returned to an inlet of the supply pump.
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