Methods used to ensure adequate fatigue life in undercarriage design at Dowty Rotol Ltd; loading conditions to which aircraft landing gear is subjected are much more difficult to define than those applied to majority of aircraft structure; tabulation of basic main landing gear fatigue test spectrum, taken from Agard Report 118, is presented; theoretical design for fatigue life and alternative design philosophies applied, `fail safe' vs `safe life;' fatigue test program, carried out in three phases, local testing, stress evaluation, and full scale fatigue testing is described.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Some fatigue problems encountered in design of aircraft landing gear


    Weitere Titelangaben:

    Aircraft Eng


    Beteiligte:
    Wood, S.W.H. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1968


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    Some Dynamic Problems in Design of Aircraft Landing Gear

    Zhu, D. P. | British Library Online Contents | 1992


    Airplane landing-gear fatigue problems

    MacLean, J.A. | Engineering Index Backfile | 1945


    Fatigue Analysis of Light Aircraft Landing Gear

    Chen, Pu-Woei / Sheen, Quen Yaw / Tan, Harn-Wen et al. | Tema Archiv | 2012


    Landing gear of aircraft and aircraft comprising landing gear

    SAKAMOTO FUMINOBU / KUROSE TOYOTOSHI | Europäisches Patentamt | 2021

    Freier Zugriff