A rotary wing aircraft and a rotor assembly of a rotary wind aircraft is disclosed. The rotary wing aircraft includes at least one engine, and the rotor assembly is coupled to the at least one engine. The rotor assembly includes a first rotor hub, a second rotor hub, and a shaft fairing between the first rotor hub to the second rotor hub, the shaft fairing defined by a chord that varies between the first rotor hub and the second rotor hub.


    Access

    Download


    Export, share and cite



    Title :

    Low drag sail fairing for coaxial rotor



    Publication date :

    2022-06-28


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    LOW DRAG SAIL FAIRING FOR COAXIAL ROTOR

    BOWLES PATRICK ORMANDE / BATTISTI MARGARET G / WAKE BRIAN ERNEST et al. | European Patent Office | 2020

    Free access

    Computational Analysis of Coaxial Rotor Hub and Sail Fairing Wake

    Deore, N. / Mobley, F. / Coder, J. | British Library Conference Proceedings | 2023


    PIVOTING SAIL FAIRING

    WITT JONATHAN | European Patent Office | 2021

    Free access

    Low-drag fairing and rotor assembly

    SHIMEK GLENN ALAN / PAULSON JARED MARK / DONOVAN TOM et al. | European Patent Office | 2021

    Free access

    LOW-DRAG FAIRING AND ROTOR ASSEMBLY

    SHIMEK GLENN ALAN / PAULSON JARED MARK / DONOVAN TOM et al. | European Patent Office | 2020

    Free access