The aircraft can have an aircraft engine and a cowl, the engine having an engine part disposed within the cowl, the cowl having a cowl section movable relative to a remainder of the cowl, the engine further having a gas path duct internal to the cowl with a first portion and a cooperating second portion, the second portion mounted to the cowl section, the cowl section moveable between a first position in which the first portion and the second portion are in fluid flow communication with one another and a second position in which the cowl section and the second portion are moved away from the first portion, wherein in the first position at least the second portion obstructs external access to the engine part and in the second position at least the second portion is displaced to permit external access to the engine part.


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    Titel :

    Moveable aircraft cowl and bypass section


    Beteiligte:
    WEAVER PAUL (Autor:in) / SMITH SCOTT (Autor:in) / CUNNINGHAM MARK HUZZARD (Autor:in)

    Erscheinungsdatum :

    2021-01-26


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



    MOVEABLE AIRCRAFT COWL AND BYPASS SECTION

    WEAVER PAUL / SMITH SCOTT / CUNNINGHAM MARK HUZZARD | Europäisches Patentamt | 2019

    Freier Zugriff

    MOVEABLE AIRCRAFT COWL AND BYPASS SECTION

    WEAVER PAUL / SMITH SCOTT / CUNNINGHAM MARK | Europäisches Patentamt | 2019

    Freier Zugriff

    Moveable Cowl Control for Increased Hypersonic Performance

    VonEggers Rudd, L. / Rankins, F. / Pines, D. J. et al. | British Library Conference Proceedings | 1998


    Moveable cowl control for increased hypersonic performance

    vonEgger, Lael / Rankins, Falcon / Pines, Darryll | AIAA | 1998


    Testing aircraft cowl fasteners

    Poupitch, O.J. | Engineering Index Backfile | 1942