A helicopter construction is provided in which conventional vertical upward occupant-seat ejection apparatus may be used for ejecting the pilot. A hatch or door is provided in the fuselage above the pilot's seat. Explosive charges are provided so that the hub and its associated rotating blades may be rapidly removed to provide clearance for ejection through the door.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Emergency Removal of Aircraft Sustaining Means


    Beteiligte:
    A. F. Larsen (Autor:in)

    Erscheinungsdatum :

    1966


    Format / Umfang :

    1 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Bending-sustaining joint and aircraft

    SUN WEI / CHEN HONG | Europäisches Patentamt | 2017

    Freier Zugriff

    Rotary systems for sustaining aircraft

    Cardona, P.M. | Engineering Index Backfile | 1931


    BENDING-SUSTAINING JOINT AND AIRCRAFT

    SUN WEI / CHEN HONG | Europäisches Patentamt | 2015

    Freier Zugriff

    Bending-sustaining joint and aircraft

    CHEN HONG / SUN WEI | Europäisches Patentamt | 2015

    Freier Zugriff

    Sustaining Aircraft Structural Integrity: Risk and Value Management

    Wilson, E. / Defence Science and Technology Organisation (Australia); Royal Aeronautical Society; Institution of Engineers Australia | British Library Conference Proceedings | 2011