A yaw control system for a helicopter having an airframe that includes a tailboom includes one or more tail rotors rotatably coupled to the tailboom and a flight control computer implementing an airframe protection module. The airframe protection module includes an airframe protection monitoring module configured to monitor one or more flight parameters of the helicopter and an airframe protection command module configured to modify one or more operating parameters of the one or more tail rotors based on the one or more flight parameters of the helicopter, thereby protecting the airframe of the helicopter.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Airframe protection systems for use on rotorcraft


    Beteiligte:
    OUELLET MARC (Autor:in) / BIRON GUILLAUME (Autor:in) / DUGRÉ ALEXIS (Autor:in)

    Erscheinungsdatum :

    2023-08-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



    Airframe Protection Systems for Use on Rotorcraft

    OUELLET MARC / BIRON GUILLAUME / DUGRÉ ALEXIS | Europäisches Patentamt | 2022

    Freier Zugriff


    ROTORCRAFT AND CONNECTING STRUCTURE FOR ARM AND AIRFRAME OF ROTORCRAFT

    PENG BIN / XIAO DINGFENG | Europäisches Patentamt | 2019

    Freier Zugriff

    ROTORCRAFT AND ASSEMBLY AND DISASSEMBLY STRUCTURE FOR FOOT STAND AND AIRFRAME OF ROTORCRAFT

    PENG BIN / XIAO DINGFENG | Europäisches Patentamt | 2019

    Freier Zugriff