Research on Influence Factors of Landing Gear Retractile Hydraulic System Performance Degradation
2014 ◽
Vol 599-601
◽
pp. 409-412
◽
Keyword(s):
Simulation model of landing gear hydraulic system is built based on AMESim, several key influence factors of performance degradation of landing gear hydraulic system are analyzed, such as changes of restrictor orifice diameter, initial pressure of accumulator, viscosity and gas percentage of oil , etc. The simulation results bring valuable reference to aircraft maintenance.
2012 ◽
Vol 241-244
◽
pp. 709-716
2016 ◽
Vol 7
(4)
◽
pp. 1061
2012 ◽
Vol 229-231
◽
pp. 1684-1687
2010 ◽
Vol 20-23
◽
pp. 294-298
2013 ◽
Vol 765-767
◽
pp. 331-335
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2013 ◽
Vol 321-324
◽
pp. 94-97
Keyword(s):
2014 ◽
Vol 496-500
◽
pp. 1134-1138
2011 ◽
Vol 201-203
◽
pp. 2206-2211
Keyword(s):
2012 ◽
Vol 605-607
◽
pp. 1317-1321
Keyword(s):