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Nose Landing Geer Steering SystemSimulation and Performance Analysis
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AVIC Xi’an aircraft industry company LTD,AVIC Xi’an aircraft industry company LTD,AVIC Xi’an aircraft industry company LTD

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V227 .9 N945.13

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    Abstract:

    This article takes steering system of a certain Domestic plane as study objective, and makes simulation and analysis on steering system through the Virtual.lab and Imagine.lab software co-simulation analysis methods, and confirms the primary factor which affects maximum static steering torque of the landing gear amongst such factors as forward angle, wheel space, castor trails, tire vertical stiffness. Analysis result shows forward angle affects maximum static steering torque of the nose gear primarily.

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ZhangTao, XinYan, ZhangYapin. Nose Landing Geer Steering SystemSimulation and Performance Analysis[J]. Advances in Aeronautical Science and Engineering,2012,3(3):

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History
  • Received:January 15,2012
  • Revised:March 19,2012
  • Adopted:March 26,2012
  • Online: July 17,2012
  • Published: