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- W2370299560 abstract "Hydraulic load system which was used to validate tested aero-engine performance by extracting hydraulic power in flight test bed was developed based on electro-hydraulic servo control. The design requirements and structure of overall system were described. The flight test results show that the system developed is stable and can quantitatively extract hydraulic power of tested engine during air and ground test,and the function is able to fully meet the technical qualification." @default.
- W2370299560 created "2016-06-24" @default.
- W2370299560 creator A5033298835 @default.
- W2370299560 date "2015-01-01" @default.
- W2370299560 modified "2023-09-23" @default.
- W2370299560 title "Hydraulic Load System of Flight Test Bed Based on Electro-hydraulic Servo Control" @default.
- W2370299560 hasPublicationYear "2015" @default.
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