Design and test of a friction damper to reduce engine vibrations on a space launcher

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• 作者：Denis Brizard (1)
  Sébastien Besset (1)
  Louis Jézéquel (1)
  Bernard Troclet (2)
  
• 关键词：Space launcher ; Damping ; Vibration testing ; Friction damper
• 刊名：Archive of Applied Mechanics (Ingenieur Archiv)
• 出版年：2013
• 出版时间：May 2013
• 年：2013
• 卷：83
• 期：5
• 页码：799-815
• 全文大小：1233KB
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• 作者单位：Denis Brizard (1)
  Sébastien Besset (1)
  Louis Jézéquel (1)
  Bernard Troclet (2)
  
  1. Laboratoire de Tribologie et Dynamique des Systèmes, UMR-CNRS 5513, école Centrale de Lyon, 36 Avenue Guy de Collongue, 69134, Ecully Cedex, France
  2. EADS Astrium, 66, Route de Verneuil, 78133, Les Mureaux, France
  
• ISSN：1432-0681

文摘

Space launchers are submitted to complex vibration environments and this can impact the payload it is carrying. Ensuring the protection of the payload therefore requires the addition of a secondary system. In this paper, a rapid design method for the dimensioning of a friction damper is developed, based on the equivalent energy dissipation with that of a viscous damper. A friction damper is designed and a prototype is built. The friction damper is first characterised alone and it is then mounted inside a scale model of a launcher last stage. The friction damper is adequately modelled by a spring in series with a friction element. The damper prototype proves to efficiently damp the rocket engine vibrations, and the design method used for dimensioning the friction damper gives a good approximation for the optimal sliding force of the damper.