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Analysis of Performances of a Semi-Active Suspension Implemented on a Landing Gear

[+] Author Affiliations
Marta I. Ocaña, Eva Novillo, Esteban Morante, Eduardo Chamorro

Compañía Española de Sistemas Aeronáuticos, CESA (S.A.), Madrid, Spain

Paper No. IMECE2014-37024, pp. V001T01A050; 5 pages
doi:10.1115/IMECE2014-37024
From:
  • ASME 2014 International Mechanical Engineering Congress and Exposition
  • Volume 1: Advances in Aerospace Technology
  • Montreal, Quebec, Canada, November 14–20, 2014
  • Conference Sponsors: ASME
  • ISBN: 978-0-7918-4642-1
  • Copyright © 2014 by ASME

abstract

Semi-active suspensions are able to adapt their behavior to the specific necessities of each operation phase of the vehicle. Their application in the aerospace industry is very attractive, specifically in landing gear actuators. However, according to Ref. [1], no examples of commercial use of this technology in this industry are reported in recent reviews of the state of the art.

In this paper, the real capabilities of a magneto-rheological semi-active suspension implemented on an UAV nose landing gear designed and manufactured by CESA are introduced by the analysis of the performances obtained by test when it is submitted to quasi-static and dynamic working conditions.

Copyright © 2014 by ASME
Topics: Gears

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