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Experimental analysis and simulation of the dynamix response of a propeller pitch change actuator

Communication avec acte
Auteur
LECLERCQ, Maxime
ccMALBURET, François
178374 Laboratoire des Sciences de l'Information et des Systèmes : Ingénierie Numérique des Systèmes Mécaniques [LSIS- INSM]
ccVERON, Philippe

URI
http://hdl.handle.net/10985/9718
Date
2012

Résumé

This paper focuses specifically on the control of the propeller pitch change mechanisms and their associated dynamics. The subject of this article is restricted to the mechanisms using a hydraulic single acting actuator. They function asymmetrically and are subject to important varying external loads under the full flight envelope. This phenomenon has an impact on their dynamic response. The question of the dynamics of these systems is rarely dealt with because, usually for aircraft applications, there is no real requirement for propeller pitch dynamic control. But, in the case of some applications, such as the Eurocopter X3, this dynamic control aspect and the safety aspect of the propeller pitch change mechanism are particularly important, because this mechanism is fully involved in aircraft safety, control and handling qualities. Firstly, this paper gives an explanation of the phenomena applied to the propeller pitch change mechanism and their contributions to its dynamic response. Then, a model of the dynamic response is proposed. Finally, an experimental identification of the pitch change mechanism dynamics concludes this article.

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Fin d'embargo:
2017-07-06
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  • Laboratoire d’Ingénierie des Systèmes Physiques Et Numériques (LISPEN)

Documents liés

Visualiser des documents liés par titre, auteur, créateur et sujet.

  • Experimental analysis and simulation of the dynamic response of a propeller pitch change actuator 
    Communication avec acte
    LECLERCQ, Maxime; ccMALBURET, François; ccVERON, Philippe (ASME, 2012)
    This paper focuses specifically on the control of the propeller pitch change mechanisms and their associated dynamics. The subject of this article is restricted to the mechanisms using a hydraulic single acting actuator. ...
  • Distributeur hydraulique, dispositif de réglage du pas de pales, aéronef muni d'un tel distributeur hydraulique 
    Brevet
    LECLERCQ, Maxime; GEMMATI, Bernard; ccMALBURET, François; ccVERON, Philippe (2014)
    La présente invention concerne un distributeur hydraulique (10) muni d'au moins un corps (11) comportant une chemise (12) pourvue d'un orifice d'alimentation (13). Ce dispositif hydraulique (10) a une tige de transfert ...
  • A Robust and Versatile Pipeline for Automatic Photogrammetric-Based Registration of Multimodal Cultural Heritage Documentation 
    Article dans une revue avec comité de lecture
    PAMART, Anthony; MORLET, François; DE LUCA, Livio; ccVERON, Philippe (MDPI, 2020)
    Imaging techniques and Image Based-Modeling (IBM) practices in the field of Cultural Heritage (CH) studies are nowadays no longer used as one-shot applications but as various and complex scenarios involving multiple ...
  • Understanding pilot biodynamical feedthrough coupling in helicopter adverse roll axis instability via lateral cyclic feedback control 
    Article dans une revue avec comité de lecture
    TOD, Georges; PAVEL, Marilena; BARRE, Pierre-Jean; ccGOMAND, Julien; ccMALBURET, François (Elsevier, 2016)
    The paper reassesses the mechanism of biodynamical feedthrough coupling to helicopter body motion in lateral-roll helicopter tasks. An analytical bio-aeroelastic pilot–vehicle model is first developed and tested for various ...
  • On a robust modeling of piezo-systems 
    Article dans une revue avec comité de lecture
    CORBIER, Christophe; BOUKARI, Abdou Fadel; CARMONA, Jean-Claude; MARTINEZ, Victor Alvarado; MORARU, George; ccMALBURET, François (American Society of Mechanical Engineers, 2012)
    This paper proposes a new modeling approach which is experimentally validated on piezo-electric systems in order to provide a robust Black-box model for complex systems control. Industrial applications such as vibration ...

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