DocumentCode
3363930
Title
An estimation method of the fluid temperature for commercial aircraft hydraulic systems
Author
Li Jing ; Xu Jiaolong ; Zhang Xi ; Yin Yaobao
Author_Institution
Coll. of Mech. Eng., Tongji Univ., Shanghai, China
fYear
2010
fDate
26-28 June 2010
Firstpage
2962
Lastpage
2965
Abstract
This paper introduces an estimation method of the fluid temperature of commercial aircraft hydraulic systems. The hydraulic systems of aircraft are subjected to be investigated. Under this method, the average temperature of the fluid in the reservoir is calculated according to the flight profile. The calculating results are coincided with the actual values and reveal the varying tendency of the fluid temperature in the reservoir. This method provides a quick approach to the thermal management of the commercial aircraft hydraulic systems.
Keywords
aerospace engineering; aircraft; estimation theory; hydraulic systems; commercial aircraft hydraulic system; estimation method; flight profile; fluid temperature; reservoir; thermal management; Aerospace control; Aircraft propulsion; Equations; Hydraulic systems; Power system modeling; Pumps; Reservoirs; Temperature; Thermal management; Valves; Aircraft; average fluid temperature; estimation method; hydraulic systems;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechanic Automation and Control Engineering (MACE), 2010 International Conference on
Conference_Location
Wuhan
Print_ISBN
978-1-4244-7737-1
Type
conf
DOI
10.1109/MACE.2010.5536487
Filename
5536487
Link To Document