An electrothermal ice protection system (IPS) installed on an aircraft includes a sensor, a parting strip assembly, and a controller. The sensor monitors a direction of a local incident airflow that is imparted on the sensor. The parting strip assembly is coupled to the critical surface and includes a plurality of heating sections. The controller is in signal communication with the sensor and the parting strip assembly. The controller determines a direction of surface airflow incident on a critical surface of the aircraft based on the local incident airflow and selectively concentrates power to at least one targeted heating section among the plurality of heating sections with respect to non-targeted heating sections among the plurality of heating sections based on the direction of the surface airflow.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Adjustable ice protection system parting strip


    Beteiligte:

    Erscheinungsdatum :

    2024-03-12


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    ADJUSTABLE ICE PROTECTION SYSTEM PARTING STRIP

    LOPRESTO VINCENT R / BOTURA GALDEMIR CEZAR | Europäisches Patentamt | 2023

    Freier Zugriff

    ADJUSTABLE ICE PROTECTION SYSTEM PARTING STRIP

    LOPRESTO VINCENT R / BOTURA GALDEMIR CEZAR | Europäisches Patentamt | 2023

    Freier Zugriff

    tail gate parting strip for automobile

    SEOL INHO | Europäisches Patentamt | 2023

    Freier Zugriff

    tail gate parting strip for automobile

    Europäisches Patentamt | 2024

    Freier Zugriff

    Vehicle door C-pillar parting sealing strip structure

    LIU MINGUO | Europäisches Patentamt | 2020

    Freier Zugriff