An exemplary rotorcraft lockout system includes a main rotor lockout comprising a base operable to be attached to a bottom surface of a fuselage and a first and a second tension arm operable to be connected to the base and a main rotor hub, and a tail rotor lockout including a clamp operable to connect to a horizontal stabilizer, a rotor arm connector operable to connect to a tail rotor hub, and a tail rotor tension arm operable to interconnect the clamp and the rotor arm connector in tension.


    Access

    Download


    Export, share and cite



    Title :

    ROTORCRAFT LOCKOUT DURING TRANSPORT



    Publication date :

    2022-09-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Rotorcraft lockout during transport

    KNOTT KEVIN / ARAKERI VITTHAL VISHNUTHREETH / JONES ALVIN et al. | European Patent Office | 2023

    Free access

    Rotorcraft Transport Trailer

    FRIEMEL MICHAEL JEROME / FRIEMEL MICHAEL BRETT | European Patent Office | 2018

    Free access

    Rotorcraft transport trailer

    FRIEMEL MICHAEL JEROME / FRIEMEL MICHAEL BRETT | European Patent Office | 2019

    Free access

    Lockout device

    STEPHEN WILLIAM MILLER | European Patent Office | 2025

    Free access

    LOCKOUT DEVICE

    MILLER STEPHEN WILLIAM | European Patent Office | 2025

    Free access