An icing protection system comprises a fuel cell, an evaporative cooling system, a thermal deicing device, a control unit and a device for measuring the pressure in the evaporative cooling system. The evaporative cooling system is in thermal contact with the fuel cell and with the thermal deicing device in order to conduct heat from the fuel cell to the thermal deicing device. The control unit controls the electrical power demanded from the evaporatively cooled fuel cell in dependence on a deviation of the pressure measured by the pressure measuring device from a predetermined NOMINAL pressure. In this way, an energetically very efficient and very well controllable icing protection system is made available that can be operated without bleed air supplied by engines or electrical energy provided by engine generators.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Icing protection system for an aircraft and method for operating an icing protection system


    Beteiligte:

    Erscheinungsdatum :

    23.02.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F25B Kältemaschinen, Kälteanlagen oder Kälteverfahren , REFRIGERATION MACHINES, PLANTS, OR SYSTEMS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H01M Verfahren oder Mittel, z.B. Batterien, für die direkte Umwandlung von chemischer in elektrische Energie , PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSION OF CHEMICAL ENERGY INTO ELECTRICAL ENERGY




    METHOD OF AIRCRAFT WING PROTECTION AGAINST ICING AND PROTECTION SYSTEM

    IVANOV VALENTIN IVANOVICH / SKIDANOV SERGEJ NIKOLAEVICH / LEVCHENKO VLADIMIR SERGEEVICH et al. | Europäisches Patentamt | 2021

    Freier Zugriff

    Aircraft anti-icing/de-icing system

    ZHU CHENGXIANG / LI QIANKUN / ZHU CHUNLING et al. | Europäisches Patentamt | 2025

    Freier Zugriff

    Inlet icing protection simulation system

    MEIS CHARLES STEVEN / HASS DAVID CHARLES | Europäisches Patentamt | 2017

    Freier Zugriff

    Inlet icing protection simulation system

    MEIS CHARLES STEVEN / HASS DAVID CHARLES | Europäisches Patentamt | 2015

    Freier Zugriff