A gas turbine engine for mounting under a wing of an aircraft has a propulsor that rotates on a first axis, and an engine core including a compressor section, a combustor section, and a turbine section, with the turbine section being closer to the propulsor than the compressor section. The engine core is aerodynamically connected to the propulsor and has a second axis. A nacelle is positioned around the propulsor and engine core. The nacelle is attached to the wing of the aircraft. A downstream end of the nacelle has at least one pivoting door with an actuation mechanism to pivot the door between a stowed position and a horizontal deployed position in which the door inhibits a flow to provide a thrust reverse of the flow.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Reverse core engine thrust reverser for under wing


    Beteiligte:
    SUCIU GABRIEL L (Autor:in) / CHANDLER JESSE M (Autor:in) / MERRY BRIAN D (Autor:in)

    Erscheinungsdatum :

    21.02.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Reverse core engine with thrust reverser

    SUCIU GABRIEL L / CHANDLER JESSE M | Europäisches Patentamt | 2017

    Freier Zugriff

    REVERSE CORE ENGINE WITH THRUST REVERSER

    SUCIU GABRIEL L / CHANDLER JESSE M | Europäisches Patentamt | 2016

    Freier Zugriff

    Aircraft engine thrust reverser

    Emerald Group Publishing | 1998


    Engine thrust reverser lock

    WILLETT KENNETH / MEARS JOHN STEPHEN / CONWAY GEORGE et al. | Europäisches Patentamt | 2017

    Freier Zugriff

    Engine Thrust Reverser Lock

    WILLETT KENNETH / MEARS JOHN STEPHEN / CONWAY GEORGE et al. | Europäisches Patentamt | 2015

    Freier Zugriff