Details of landing gear made primarily of high strength steels; automatic braking system for stopping wheel rotation after takeoff and prior to gear retraction; use of forged aluminum wheels; installation of fuse plugs in wheels to release air pressure at predetermined elevated temperature, prior to tire bursting; tire service life; maintenance procedures and operating instructions. (See also SAE -- Paper n 139B for meeting v 68 n 139 Jan 11-15 1960 9 p)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Landing gear and tire experience with Boeing 707


    Weitere Titelangaben:

    SAE -- J


    Beteiligte:
    Ericksen, W.P. (Autor:in)


    Erscheinungsdatum :

    1960


    Format / Umfang :

    2 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Landing gear and tire experience with Boeing 707

    Ericksen, W.P. | Engineering Index Backfile | 1960


    LANDING GEAR AND TIRE EXPERIENCE WITH THE BOEING 707

    ERICKSEN, W. P. | SAE Technical Papers | 1960


    Boeing-Safran Landing Gear Noise Reduction Project on 2020 Boeing ecoDemonstrator Program

    Nesbitt, Eric / Suzuki, Takao / Daneshvarn, Navid et al. | AIAA | 2022


    CONTROLLED LANDING GEAR TIRE TRACTION SYSTEM

    BARMICHEV SERGEY / BOREN KELLY L | Europäisches Patentamt | 2018

    Freier Zugriff

    Aircraft landing gear tire replacement frame

    BIAN HONGNING / LI YONGMING / KONG XINYI et al. | Europäisches Patentamt | 2023

    Freier Zugriff