An ice detection system (122) comprising a first group of sensors (148) and a second group of sensors (170). The first group of sensors (148) is located in a first group of locations on an aircraft (100). The first group of sensors (148) in the first group of locations is configured to detect a first type of icing condition for the aircraft (100). The second group of sensors (170) is located in a second group of locations on the aircraft (100). The second group of sensors (170) in the second group of locations is configured to detect a second type of icing condition for the aircraft (100).


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    SUPERCOOLED LARGE DROP ICING CONDITION DETECTION SYSTEM


    Weitere Titelangaben:

    SYSTEME DE DETECTION D'UNE CONDITION DE GIVRAGE A GROSSES GOUTTES SURFONDUES


    Beteiligte:
    MEIS CHARLES S (Autor:in) / BOSETTI CRIS K (Autor:in)

    Erscheinungsdatum :

    26.04.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Supercooled large drop icing condition detection system

    MEIS CHARLES STEVEN / BOSETTI CRIS KEVIN | Europäisches Patentamt | 2015

    Freier Zugriff

    Supercooled large drop icing condition detection system

    MEIS CHARLES S / BOSETTI CRIS K | Europäisches Patentamt | 2016

    Freier Zugriff

    Supercooled large drop icing condition detection system

    MEIS CHARLES STEVEN / BOSETTI CRIS KEVIN | Europäisches Patentamt | 2019

    Freier Zugriff

    SUPERCOOLED LARGE DROP ICING CONDITION DETECTION SYSTEM

    MEIS CHARLES S / BOSETTI CRIS K | Europäisches Patentamt | 2018

    Freier Zugriff

    Supercooled Large Drop Icing Condition Detection System

    MEIS CHARLES STEVEN / BOSETTI CRIS KEVIN | Europäisches Patentamt | 2016

    Freier Zugriff