• français
    • English
    français
  • Login
Help
View Item 
  •   Home
  • Laboratoire d’Ingénierie des Systèmes Physiques Et Numériques (LISPEN)
  • View Item
  • Home
  • Laboratoire d’Ingénierie des Systèmes Physiques Et Numériques (LISPEN)
  • View Item
JavaScript is disabled for your browser. Some features of this site may not work without it.

Simulation of a helicopter’s main gearbox semiactive suspension with bond graphs

Article dans une revue avec comité de lecture
Author
CARMONA, Jean-Claude
BOUDON, Benjamin
ccMALBURET, François
178374 Laboratoire des Sciences de l'Information et des Systèmes : Ingénierie Numérique des Systèmes Mécaniques [LSIS- INSM]

URI
http://hdl.handle.net/10985/11474
Date
2016
Journal
Multibody System Dynamics

Abstract

This paper presents a bond graph model of a helicopter’s semiactive suspension and the associated simulations. The structural and modular approach proposed with bond graph permits a systematic modeling of mechatronic multibody systems. This approach was carried out thanks to the use of the singular perturbation method, which is a variant of penalty formulation. The model is then built as an assembly of components or modules (rigid bodies and compliant kinematic joints) by following the structure of the actual system. The bond graph model of the passive suspension with fixed flapping masses has been verified with another multibody tool for three different excitations (pumping, roll, and yaw). Next, the passive model, augmented with electrical actuators and controllers, is called the semiactive suspension model. Simulations on the semiactive suspension model have been conducted.

Files in this item

Name:
Multibody_system_dynamics_2016.pdf
Size:
1.067Mb
Format:
PDF
Description:
Article principal
View/Open

Collections

  • Laboratoire d’Ingénierie des Systèmes Physiques Et Numériques (LISPEN)

Related items

Showing items related by title, author, creator and subject.

  • Design methodology of a complex CKC mechanical joint with a representation energetic tool multi-Bond graph: application to the helicopter 
    Chapitre d'ouvrage scientifique
    BOUDON, Benjamin; CARMONA, Jean-Claude; ccMALBURET, François (Springer, 2014)
    Due to the operation of the rotor, the helicopter is subject to important vibration levels affecting namely the fatigue of the mechanical parts and the passenger comfort. Suspensions between the main gear box (MGB) and the ...
  • Nouvelle approche pour l’optimisation de systèmes mécaniques en vue de la récupération d'énergie vibratoire 
    Communication sans acte
    BOUDON, Benjamin; CARMONA, Jean-Claude; ccMALBURET, François (2013)
    La récupération d’énergie à partir des vibrations mécaniques est une préoccupation importante à l’heure actuelle car elle permet de rendre autonome les systèmes de surveillance vibratoire ou de contrôle de vibration ...
  • Bond Graph Modeling and Simulation of a Vibration Absorber System in Helicopters 
    Chapitre d'ouvrage scientifique
    CARMONA, Jean-Claude; BOUDON, Benjamin; ccMALBURET, François (Springer International Publishing, 2017)
    n the last 20 years, computer science has considerably progressed and there has been a resurgence of interest in bond graphs. The evolution of bond graph software has allowed for the full exploitation of its graphical ...
  • 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 ...
  • Control loads reduction through control system architecture optimization – application to a conventional rotor on compound helicopters 
    Communication avec acte
    PARIS, Manuel; EGLIN, Paul; CARMONA, Jean-Claude; ccMALBURET, François (AHS, 2014)
    A kinematic study of a helicopter main rotor control system is carried out to investigate loads in servo actuators and non-rotating scissors during high speed and high load factors maneuvers. The kinematic model is then ...

Browse

All SAMCommunities & CollectionsAuthorsIssue DateCenter / InstitutionThis CollectionAuthorsIssue DateCenter / Institution

Newsletter

Latest newsletterPrevious newsletters

Statistics

Most Popular ItemsStatistics by CountryMost Popular Authors

ÉCOLE NATIONALE SUPERIEURE D'ARTS ET METIERS

  • Contact
  • Mentions légales

ÉCOLE NATIONALE SUPERIEURE D'ARTS ET METIERS

  • Contact
  • Mentions légales