A system and method for controlling bleed air flow into an air cycle machine that includes a bleed air inlet and a conditioned air outlet is provided. The system and method include discharging bleed air from an operating gas turbine engine, sensing exhaust gas temperature (EGT) of the gas turbine engine, sensing conditioned air temperature at the conditioned air outlet, and controlling bleed air flow into the air cycle machine based on the sensed EGT and on the sensed conditioned air temperature.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Aircraft environmental control system inlet flow control


    Beteiligte:
    SHEPARD ERIC (Autor:in) / WOLOWNIK TODD (Autor:in)

    Erscheinungsdatum :

    2015-12-08


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



    Aircraft environmental control system inlet flow control

    SHEPARD ERIC / WOLOWNIK TODD | Europäisches Patentamt | 2016

    Freier Zugriff

    Aircraft ram air inlet system and control method

    HUANG XING / XIE KAI / PENG YING et al. | Europäisches Patentamt | 2023

    Freier Zugriff

    Complex Control System for an Aircraft Supersonic Inlet

    Tudosie, A.N. / Corcau, J.I. / WSEAS (Organization) | British Library Conference Proceedings | 2009


    ENVIRONMENTAL CONTROL SYSTEM WITH LOW INLET PRESSURE

    VIGNALI MARK G | Europäisches Patentamt | 2024

    Freier Zugriff

    ENVIRONMENTAL CONTROL SYSTEM WITH LOW INLET PRESSURE

    VIGNALI MARK G | Europäisches Patentamt | 2024

    Freier Zugriff