An airspeed indicator display for an aircraft having a main rotor system and a translational thrust system includes a first indicator operable to display an actual airspeed of the aircraft and a second indicator positioned adjacent the first indicator. The second indicator is operable to display an actual pitch angle of the translational thrust system.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    COMPOSITE AIRSPEED INDICATOR DISPLAY FOR COMPOUND AIRCRAFTS


    Beteiligte:
    ADAMS DAVID L (Autor:in) / FIMBERS KEVIN RON (Autor:in)

    Erscheinungsdatum :

    18.04.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G01C Messen von Entfernungen, Höhen, Neigungen oder Richtungen , MEASURING DISTANCES, LEVELS OR BEARINGS



    Composite airspeed indicator display for compound aircrafts

    ADAMS DAVID L / FIMBERS KEVIN RON | Europäisches Patentamt | 2020

    Freier Zugriff

    Composite airspeed indicator display for compound aircrafts

    ADAMS DAVID L / FIMBERS KEVIN RON | Europäisches Patentamt | 2020

    Freier Zugriff

    COMPOSITE AIRSPEED INDICATOR DISPLAY FOR COMPOUND AIRCRAFTS

    ADAMS DAVID L / FIMBERS KEVIN RON | Europäisches Patentamt | 2019

    Freier Zugriff

    An alternative neural airspeed computation method for aircrafts

    Turkmen, Ilke | Emerald Group Publishing | 2018


    AIRSPEED INDICATOR (PITOT STATIC)

    SAE Technical Papers | 1947