A rotor ice protection system (RIPS) apparatus for an aircraft to heat aircraft rotor blades is provided. The RIPS apparatus includes circuitry disposed to transmit electrical loads associated with RIPS operations, an indicator unit disposed to alert a pilot of the aircraft to a RIPS condition indicating an operating status of the RIPS operations, a controller configured to actuate the RIPS operations in accordance with current conditions and to issue a command to the indicator unit to alert the pilot to the RIPS operations according to the actuation and a sensor system disposed to sense whether the circuitry is transmitting the electrical loads and to provide a sensing result to the indicator unit. The indicator unit additionally alerts the pilot to the RIPS operations according to the sensing result.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Rotor ice protection system


    Beteiligte:

    Erscheinungsdatum :

    2020-02-11


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G01R Messen elektrischer Größen , MEASURING ELECTRIC VARIABLES



    ROTOR ICE PROTECTION SYSTEM

    LONGLEY JR ROBERT F / FOGARTY MATTHEW | Europäisches Patentamt | 2016

    Freier Zugriff

    ROTOR ICE PROTECTION SYSTEM

    LONGLEY JR ROBERT F / FOGARTY MATTHEW | Europäisches Patentamt | 2017

    Freier Zugriff

    Motor locked-rotor protection system, motor locked-rotor protection method and motor

    YANG KEWEN / XU SHIHUA / WENG SHUN et al. | Europäisches Patentamt | 2020

    Freier Zugriff

    ROTOR BLADE EROSION PROTECTION SYSTEM

    NISSEN JEFFREY P | Europäisches Patentamt | 2017

    Freier Zugriff

    ROTOR BLADE EROSION PROTECTION SYSTEM

    NISSEN JEFFREY P | Europäisches Patentamt | 2020

    Freier Zugriff