A rotorcraft (1) having: a lift rotor (5); a wing (10) extending from a first end (11) carrying a first propulsive propeller (21) to a second end (12) carrying a second propeller (22); landing gear (30); and a tail (40). The rotorcraft (1) is provided with two fuselages (51, 52) secured to said wing (10) between said first and second propulsive propellers (21, 22) in such a manner as to present an inter-fuselage space (60) having no propeller between said fuselages (51, 52), each fuselage (51, 52) including at least one undercarriage of said landing gear (30).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Twin-fuselage rotorcraft


    Beteiligte:
    NICOLA JEAN (Autor:in)

    Erscheinungsdatum :

    19.12.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Aerodynamic Force Computations for Rotorcraft Fuselage

    Singh, R. / Dinavahi, S. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2012


    Aerodynamic Force Computations for Rotorcraft Fuselage

    Singh, Rajneesh / Dinavahi, Surya | AIAA | 2012


    Coupling of Rotorcraft Elastic Fuselage with CFD

    Saberi, Hossein / Hasbun, Matthew / Kim, Jeewoong et al. | British Library Conference Proceedings | 2018


    Unsteady Fuselage Loads on Rotorcraft in Ground Effect

    Ganesh, B. / Komerath, N. / Society of Automotive Engineers | British Library Conference Proceedings | 2005


    Rotorcraft fuselage mass assessment in early design stages

    Schwinn, Dominik B. / Weiand, Peter / Buchwald, Michel | Springer Verlag | 2021

    Freier Zugriff