A rotorcraft includes at least one first engine operatively connected to a first rotor, and a second engine operatively connected to at least one of a second rotor or an electrical generator for driving an electrical system, wherein the second engine is a different size than the first engine. The second engine can be smaller than the at least one first engine, for example.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    ENGINE SYSTEMS FOR ROTORCRAFT


    Beteiligte:

    Erscheinungsdatum :

    16.08.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    Engine systems for rotorcraft

    SIMONETTI JOSEPH L / BYSTRY JR MARK D | Europäisches Patentamt | 2020

    Freier Zugriff

    Rotorcraft convertible engine study

    Goldstein, D. N. / Hirschkron, R. / Smith, C. E. | NTRS | 1983


    Rotorcraft Convertible Engine Study

    D. N. Goldstein / R. Hirschkron / C. E. Smith | NTIS | 1983


    Rotorcraft Convertible Engine Study

    J. C. Gill / R. V. Earle / H. M. Mar | NTIS | 1982


    Rotorcraft convertible engine study

    Gill, J. C. / Earle, R. V. / Mar, H. M. | NTRS | 1982