The impact response of an airplane pneumatic suspension

• Autorzy: Ossowski A.
• Konferencja: Symposium Vibrations In Physical Systems (23 ; 28-31.05.2008 ; Będlewo koło Poznania ; Polska)
• Języki publikacji: EN

Abstrakty

EN

Pneumatic suspensions, because of their significant advantages in comparison to classical suspension systems containing mechanical springs and hydraulic attenuators, are widely applied in road and railway vehicles. They also seem to be applicable in airplanes due to their advantageous impact properties. In this paper a simple one-wheel dynamical model of the pneumatic suspension is described. Impact properties of the model are studied in the context of the application in airplanes. Results of theoretical analysis and computer simulations are presented and compared with experimental data.

Słowa kluczowe

EN

impact response; pneumatic suspension

PL

zawieszenie pneumatyczne; zawieszenie samolotu

• Wydawca: Poznan University of Technology. Institute of Applied Mechanics
• Czasopismo: Vibrations in Physical Systems
• Rocznik: 2008
• Tom: Vol. 23
• Strony: 315--320
• Opis fizyczny: Bibliogr. 2 poz., 1 rys., 1 wykr.

Twórcy

autor

Ossowski A.

• Institute of Fundamental Technological Research, PAS, ul. Świętokrzyska 21, 00-049 Warszawa

Bibliografia

• 1. Docquier-N; Fisette-P; Jeanmart-H, Multiphysic modelling of railway vehicles equipped with pneumatic suspension, Vehicle System Dynamics, 45(6): 505-24, June 2007.
• 2. Wang Yun chao; Gao Xiu hua; Guo Jian hua; Zhang Chun qiu, Research on virtual prototype of hydro-pneumatic suspension, Journal of System Simulation, 18(8): 2183-6, Aug. 2006.