Thermal Analysis and Simulation of Aircraft Hydraulic System

Xi Zhang; Jing Li; Yao Bao Yin

doi:10.4028/www.scientific.net/AMR.204-210.1984

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HomeAdvanced Materials ResearchAdvanced Materials Research Vols. 204-210Thermal Analysis and Simulation of Aircraft...

Thermal Analysis and Simulation of Aircraft Hydraulic System

Abstract:

Thermal analysis of aircraft hydraulic systems is an important subject for system’s design. Heat generation and dissipation of aircraft hydraulic systems had been discussed in this article. Heat exchange was calculated based on heat transfer theory. A formula of temperature variation was derived based on the assumption that oil flow in the hydraulic system was one-dimension unsteady flow. Take the hydraulic system of a certain commercial aircraft for example, a model was established to simulate the temperature change of aircraft hydraulic systems based on AMESim. The simulation results are in consistent with test data.

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Periodical:

Advanced Materials Research (Volumes 204-210)

Pages:

1984-1989

DOI:

https://doi.org/10.4028/www.scientific.net/AMR.204-210.1984

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Online since:

February 2011

Authors:

Xi Zhang, Jing Li, Yao Bao Yin

Keywords:

Aircraft Hydraulic System, AMEsim, Simulation, Thermal Analysis

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References

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