In multi-brake aircraft landing gear systems, it is common for brake rod bending to participate in brake squeal vibration modes. Experiments have proven that damping the bending mode of the rod can reduce brake vibration. A patented method of doing so with a simple, lightweight, split-tube insert for tubular brake rods is described. Equations for sizing the insert for a given interference pressure are presented, results of bench tests are summarized, and further development is discussed.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Reducing Aircraft Brake Squeal with a Damped Brake-Rod


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    World Aviation Congress & Exposition ; 2000



    Erscheinungsdatum :

    10.10.2000




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Reducing Aircraft Brake Squeal with a Damped Brake-Rod

    Enright, J. J. / Sociewty of Automotive Engineers of New York / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2000



    Brake Squeal

    Popp, K. ;Rudolph, M. | TIBKAT | 2001

    Freier Zugriff

    Brake Squeal

    Popp, K. / Rudolph, M. | TIBKAT


    Brake squeal generation

    Watany,M. / Abouel-Seoud,S. / Saad,A. et al. | Kraftfahrwesen | 1999