The invention discloses a hydrogen-fired hybrid turboprop engine. The hydrogen-fired hybrid turboprop engine comprises a fuel cell power unit, a hydrogen-fired turboprop engine, a propeller and a shared speed reducer, the fuel cell power unit and the hydrogen-fired turboprop engine are respectively connected with the hydrogen fuel storage tank through pipelines; the fuel cell power unit and the hydrogen-fired turboprop engine are respectively connected with the propeller; one end of the shared speed reducer is connected with the propeller, and the other end of the shared speed reducer is connected with the fuel cell power unit and the hydrogen-fired turboprop engine. The advantages of a traditional turboprop engine and a hydrogen fuel cell are integrated, the disadvantages of the traditional turboprop engine and the hydrogen fuel cell are complemented, the same equipment is shared, and the zero-carbon-emission and large-shaft-power output functions are achieved.

    本发明公开了一种燃氢混动涡桨发动机,包括:燃料电池动力单元、燃氢涡桨发动机、螺旋桨和共用减速器;所述燃料电池动力单元和燃氢涡桨发动机分别通过管路与氢燃料储罐连接;所述燃料电池动力单元和燃氢涡桨发动机分别与螺旋桨连接;所述共用减速器一端与螺旋桨连接,另一端分别与燃料电池动力单元和燃氢涡桨发动机连接。本发明整合了传统涡桨发动机和氢燃料电池优势、互补了相互间劣势、共享了相同设备,且具备零碳排放、大轴功率输出功能。


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    Titel :

    Hydrogen-fired hybrid turboprop engine


    Weitere Titelangaben:

    一种燃氢混动涡桨发动机


    Beteiligte:
    LI WEI (Autor:in) / CAO JUN (Autor:in) / XIAO WEI (Autor:in) / ZHANG KUN (Autor:in) / WU MOUBIN (Autor:in) / LIANG ZHENXIN (Autor:in) / PENG FUXIA (Autor:in) / LIU SHANLIN (Autor:in) / YANG ANJIE (Autor:in)

    Erscheinungsdatum :

    22.08.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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