The present invention discloses a gas turbine engine comprising: a compressor; a combustor that shares a rotating shaft with the compressor and mixes and combusts gas and fuel supplied from the compressor; a starter disposed in the combustor to start the combustor; and a speed regulator that is connected to a rotating shaft of the combustor and adjusts the speed of the rotating shaft of the combustor according to the internal state of the combustor. The gas turbine engine according to embodiments of the present invention can rapidly restart when a part of the combustor does not operate.

    본 발명은 가스터빈 엔진을 개시한다. 본 발명은, 압축기와, 상기 압축기와 회전축을 공유하며, 상기 압축기에서 공급된 기체와 연료를 혼합하여 연소시키는 연소기와, 상기 연소기에 배치되어 상기 연소기를 시동하는 시동기와, 상기 연소기의 회전축에 연결되며, 상기 연소기 내부의 상태에 따라 상기 연소기의 회전축의 속도를 조절하는 속도조절부를 포함한다.


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    Titel :

    Gas turbine engine


    Weitere Titelangaben:

    가스터빈 엔진


    Beteiligte:
    PARK SOO YOUL (Autor:in)

    Erscheinungsdatum :

    2021-09-23


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Koreanisch


    Klassifikation :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES



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