A fuselage mounted gas turbine engine installation the installation includes at least one propeller stage and a gas turbine core arranged in use to drive the propeller stage. The core is external to the fuselage and the rotational axes of the core and propeller stage are offset with respect to each other.


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    Titel :

    Engine installation


    Beteiligte:

    Erscheinungsdatum :

    24.05.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Engine installation

    BagnallWild, R.K. | Engineering Index Backfile | 1922


    Engine installation

    BagnallWild, R.K. | Engineering Index Backfile | 1922


    Engine installation

    Harrison, H.C. | Engineering Index Backfile | 1956


    ENGINE INSTALLATION APPARATUS

    TERRY MEL | Europäisches Patentamt | 2015

    Freier Zugriff

    Aircraft Engine Installation

    Nutt, Arthur | Emerald Group Publishing | 1930