An aircraft is described and includes a fuselage, a wing coupled to the fuselage, and a rotor system including a proprotor system and an engine. An interconnect driveshaft gear is configured to communicate mechanical energy between a gearbox and an interconnect driveshaft. An accessory gear is coplanar with and in mechanical communication with the driveshaft gear. A proprotor gear is coplanar with and in mechanical communication with the interconnect driveshaft gear and the accessory gear and communicates mechanical energy to the proprotor system. An engine gear coplanar and in mechanical communication with the interconnect driveshaft ear, the accessory gear, and the proprotor gear transmits mechanical energy to the proprotor system via the proprotor gear.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    TILTROTOR WITH INBOARD ENGINES


    Beteiligte:
    ROSS BRENT C (Autor:in) / IVANS STEVEN R (Autor:in)

    Erscheinungsdatum :

    2019-03-21


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Tiltrotor with inboard engines

    ROSS BRENT C / IVANS STEVEN R | Europäisches Patentamt | 2019

    Freier Zugriff

    Tiltrotor with inboard engines

    ROSS BRENT C / IVANS STEVEN R | Europäisches Patentamt | 2022

    Freier Zugriff

    Tiltrotor with Inboard Engines

    ROSS BRENT C / IVANS STEVEN R | Europäisches Patentamt | 2017

    Freier Zugriff

    Tiltrotor aircraft with inboard wing mounted fixed engine arrangement

    ROSS BRENT C / BOCKMILLER DAVID R / ISAAC MARK L et al. | Europäisches Patentamt | 2016

    Freier Zugriff

    Inboard marine engines

    Engineering Index Backfile | 1947