The tilt rotor concept is introduced and the performance capabilities and noise characteristics of the XV-15 aircraft are discussed. In hover, the aircraft is lifted by the two wing tip mounted rotors with the nacelles in the vertical position. In this flight mode, the vehicle is a twin rotor helicopter and is controlled by rotor cyclic and collective controls. The aircraft can fly as a helicopter or tilt the nacelle to the propeller mode and operate as a fixed-wing twin turboprop airplane. It is also possible to stop the conversion at any intermediate angle and fly continuously or reconvert. The rotors are powered by two modified T-53 engines and the power train includes a cross shaft located in the wing, to allow for the engine failure case and still retain power to both rotors.


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    Titel :

    The tilt rotor research aircraft (XV-15) program


    Beteiligte:
    Magee, J. P. (Autor:in)


    Erscheinungsdatum :

    01.02.1983


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    XV-15 Tilt Rotor Research Aircraft - Program report

    MAGEE, J. / WERNICKE, K. | AIAA | 1979


    XV-15 Tilt Rotor Research Aircraft - Program report

    Magee, J. P. / Wernicke, K. G. | NTRS | 1979


    Tilt rotor aircraft

    XU SHENGMING / SHANG LIYING / MING YALI et al. | Europäisches Patentamt | 2025

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