Development of flow metering for electric aircraft oil pump

In order to solve the difficulty of flow control in electric aircraft oil pump system, an electric aircraft oil pump was used as research object, with speed range of 2000rpm∼9000rpm, temperature range of 270K∼325K, pressure between the input and output of pump do not exceed 0.6MPa, and aviation 8B a...

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Veröffentlicht in:	Journal of physics. Conference series 2024-05, Vol.2746 (1), p.12011
Hauptverfasser:	Xuepeng, Li, Wenlong, Zhang, Yueming, Cheng, Jianghong, Li
Format:	Artikel
Sprache:	eng
Schlagworte:	Aircraft control Flow control Fly by wire control
Online-Zugang:	Volltext
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