A method of operating a multi-engine aircraft (1, Fig. 1a) having two or more gas turbine engines (10, Fig. 1b) includes operating a first engine in a powered mode to provide motive power to the aircraft (1), and, in flight, operating a second engine in either a powered mode to provide motive power to the aircraft (1) or in a standby mode to provide substantially no motive power to the aircraft (1). When operating the second engine in the powered mode, pressurized air is bled from a first bleed location (19) of a compressor (9) of the second engine. When operating the second engine in the standby mode, pressurized air is bled from a second bleed location (21) of the compressor (9) of the second engine and supplying the pressurized air to a bleed air system of the second engine. The second bleed location (21) is downstream of the first bleed location (19) within the compressor (9) of the second engine.


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    Titel :

    AIR SYSTEM SWITCHING SYSTEM TO ALLOW AERO-ENGINES TO OPERATE IN STANDBY MODE


    Weitere Titelangaben:

    LUFTSYSTEM-SCHALTSYSTEM ZUR ERMÖGLICHUNG DES BETRIEBS VON FLUGZEUGTRIEBWERKEN IM BEREITSCHAFTSMODUS
    SYSTÈME DE COMMUTATION DE SYSTÈME D'AIR PERMETTANT AUX MOTEURS AÉRONAUTIQUES DE FONCTIONNER EN MODE VEILLE


    Beteiligte:
    NG KEVIN (Autor:in) / VINSKI JOHNNY (Autor:in) / LOGAN ADAM (Autor:in)

    Erscheinungsdatum :

    2022-05-11


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS



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