An embodiment rotorcraft includes a main rotor, one or more flight controls connected to the main rotor and operational to control flight characteristics of the main rotor by pitching a nose of the rotorcraft upward, and a flight control computer (FCC) operable to determine an attitude command and to generate an adjusted attitude command by adjusting a magnitude of the attitude command according to an above ground level (AGL) altitude of the rotorcraft. The FCC is further operable to control a flight characteristic of the rotorcraft by sending the adjusted attitude command to one or more flight controls.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    System and method for automatic rotorcraft tail strike protection


    Beteiligte:

    Erscheinungsdatum :

    2020-12-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



    SYSTEM AND METHOD FOR AUTOMATIC ROTORCRAFT TAIL STRIKE PROTECTION

    GILLETT LUKE DAFYDD | Europäisches Patentamt | 2023

    Freier Zugriff

    System and Method for Automatic Rotorcraft Tail Strike Protection

    GILLETT LUKE DAFYDD | Europäisches Patentamt | 2019

    Freier Zugriff

    Rotorcraft tail boom, and a rotorcraft

    LEUSINK DEBBIE / ALFANO DAVID | Europäisches Patentamt | 2021

    Freier Zugriff

    TAIL BOOM OF A ROTORCRAFT AND ROTORCRAFT

    LEUSINK DEBBIE / ALFANO DAVID | Europäisches Patentamt | 2017

    Freier Zugriff

    A ROTORCRAFT TAIL BOOM, AND A ROTORCRAFT

    LEUSINK DEBBIE / ALFANO DAVID | Europäisches Patentamt | 2017

    Freier Zugriff