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- W2894914127 abstract "This paper deals with system-level temperature of the hydraulic system of the airliner. The power losses in airliner hydraulic system is converted to heat and results in the temperature rise of the hydraulic system. It seriously affects the safety and reliability of the airliner. In order to investigate thoroughly the mechanism of thermal load in airliner hydraulic system and control the temperature rise of airliner hydraulic system within an allowable range, this paper proposes two thermal management schemes which respectively adopt fuel/hydraulic oil heat exchanger or hydraulic pipeline passing through fuel tank. Then towards these two schemes it adopts lumped parameter method to conduct modeling and simulation from the angle of heat generation and dissipation for investigating the ability of thermal management scheme. Finally the simulation results show the temperature variation rule of hydraulic oil and demonstrate the validity of modeling method." @default.
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- W2894914127 date "2018-01-01" @default.
- W2894914127 modified "2023-09-24" @default.
- W2894914127 title "Modeling and Simulation of System-Level Temperature for Airliner Hydraulic System in a Full Flight Mission Profile" @default.
- W2894914127 doi "https://doi.org/10.1049/cp.2018.0092" @default.
- W2894914127 hasPublicationYear "2018" @default.
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