A rotary wing aircraft includes a rotor assembly includes a rotor sensor generating a rotor sensor time domain signal; a rotor transform module converting the rotor sensor time domain signal to a rotor sensor frequency domain signal; and a rotor transceiver for transmitting the rotor sensor frequency domain signal over a transfer medium; an airframe assembly including: an airframe transceiver receiving the rotor sensor frequency domain signal; and an airframe transform module converting the rotor sensor frequency domain signal to the rotor sensor time domain signal. Signals from the airframe assembly may also be converted to the frequency domain prior to transfer over the transfer medium to the rotor assembly.


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    Titel :

    Harmonic data transfer in rotary wing aircraft


    Beteiligte:
    SANE HARSHAD S (Autor:in) / MATALANIS CLAUDE G (Autor:in) / GEIGER DEREK (Autor:in) / FOWLER DONALD W (Autor:in)

    Erscheinungsdatum :

    01.12.2015


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / H04B TRANSMISSION , Übertragung



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