According to one embodiment, a method of adjusting an aircraft pedal assembly includes providing a pedal linkage coupled between a pedal and an attachment assembly situated proximate to an aircraft instrument panel. A brake cylinder is provided coupled between the pedal and the attachment assembly. The pedal linkage is rotated in response to an adjustment input. The pedal linkage is maintained approximately parallel to the brake cylinder during rotation of the pedal linkage.


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    Titel :

    PILOT CONTROL SYSTEM WITH ADJUSTABLE PEDALS


    Weitere Titelangaben:

    SYSTEME DE COMMANDE PILOTE AVEC PEDALES AJUSTABLES


    Beteiligte:
    YATES TRAVIS L (Autor:in) / LINTON BRADLEY D (Autor:in)

    Erscheinungsdatum :

    2015-05-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G05G CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY , Steuer- oder Regelvorrichtungen oder Steuer- oder Regelsysteme gekennzeichnet ausschließlich durch mechanische Einzelheiten



    Pilot control system with adjustable pedals

    YATES TRAVIS L / LINTON BRADLEY D | Europäisches Patentamt | 2017

    Freier Zugriff

    Adjustable Pedals: A Practical Approach

    Imerman, Roger B. | SAE Technical Papers | 1993


    The Effectiveness of Adjustable Pedals Usage

    Parenteau, C. S. / Shen, W. / Shah, M. et al. | British Library Conference Proceedings | 2000


    The effectiveness of adjustable pedals usage

    Paranteau,C.S. / Shen,W. / Shah,M. et al. | Kraftfahrwesen | 2000


    The Effectiveness of Adjustable Pedals Usage

    Parenteau, Chantal S. / Shah, Minoo / Shen, Wenqi | SAE Technical Papers | 2000