In the device described, for the purpose of increasing reliability of operation, decreasing labor consumption and simplifying operation of it, the tip of the pipe is made in the form of a bolt with a central hole through it. With this, one end of the bolt has a faired flat head with a flat surface for a wrench and a drain cock with a taper, and the other has threads on its outer surface and cone providing connection of the pipeline to it. The outer panel is rigidly connected to the inner framing, for instance for spar rail, with the bolt-tip.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Cavity Draining Device for Aircraft Fuel System Components


    Beteiligte:

    Erscheinungsdatum :

    1973


    Format / Umfang :

    3 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Small aircraft fuel tank draining valve switch

    TANG XUELIAN / CUI ZHANGDONG / SUN FENGQIN et al. | Europäisches Patentamt | 2015

    Freier Zugriff

    Draining system for fuel tank

    TETER JOHN M / MADERA ROBERT J | Europäisches Patentamt | 2016

    Freier Zugriff

    DRAINING SYSTEM FOR FUEL TANK

    TETER JOHN M / MADERA ROBERT J | Europäisches Patentamt | 2016

    Freier Zugriff


    SYSTEM FOR DRAINING AN AIRCRAFT COMBUSTION ENGINE AND ASSOCIATED AIRCRAFT

    PATRICK FORT / CHRISTOPHE ALBERTINI | Europäisches Patentamt | 2023

    Freier Zugriff