A system for detecting a fault in a locking pin for use in an aircraft includes the locking pin; means for receiving a static air temperature; and a controller; wherein said locking pin comprises an internal heater element and at least one internal temperature sensor provided therein. The system also includes means for transmitting said measured temperature sensor information from said at least internal temperature sensor and said static air temperature information to said controller. The controller is configured to compare the static air temperature information with said locking pin temperature sensor information and determine if a difference between the measurements is above a static v. internal temperature threshold value.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Anti-icing and de-icing heated lock pin system


    Beteiligte:

    Erscheinungsdatum :

    05.08.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    G01K MEASURING TEMPERATURE , Messen der Temperatur / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H05B ELECTRIC HEATING , Elektrische Heizung



    ANTI-ICING AND DE-ICING HEATED LOCK PIN SYSTEM

    BURGESS GRAHAM JAMES / FOSTER DANIEL | Europäisches Patentamt | 2023

    Freier Zugriff

    ANTI-ICING AND DE-ICING HEATED LOCK PIN SYSTEM

    BURGESS GRAHAM JAMES / FOSTER DANIEL | Europäisches Patentamt | 2021

    Freier Zugriff


    MULTIFUNCTIONAL DE-ICING/ANTI-ICING SYSTEM

    NORDIN PONTUS / STRINDBERG GOTE | Europäisches Patentamt | 2017

    Freier Zugriff

    Aircraft anti-icing/de-icing system

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

    Freier Zugriff