Provided are a power unit control system, a power unit control method, and a recording medium capable of suppressing an increase in size, weight, and cost of a device and improving the life of a gas turbine. This power unit control system is provided with: a gas turbine having a turbine rotor; an energy converter capable of operating as a generator that generates power by rotation of the gas turbine; a battery for storing the power generated by the energy converter; a reception unit that receives a signal transmitted from a device control unit that operates by the power stored in the battery or the power emitted by the energy converter; and a control unit that performs rotational speed increase control for increasing the rotational speed of the gas turbine to a predetermined rotational speed when the reception unit receives a predetermined first signal.

    提供一种能够抑制装置的大型化、重量化以及成本增大并且能够改善燃气轮机的寿命的动力单元控制系统、动力单元控制方法以及记录介质。动力单元控制系统具备:燃气轮机,其具有轮机旋翼;能量转换器,其能够作为通过所述燃气轮机的旋转而发电的发电机进行动作;电池,其对由所述能量转换器发出的电力进行蓄积;接收部,其接收从装置控制部发送的信号,该装置控制部通过所述电池中蓄积的所述电力或由所述能量转换器发出的电力而工作的装置;以及控制部,其在由所述接收部接收到规定的第一信号的情况下,进行使所述燃气轮机的转速上升至规定的转速的转速上升控制。


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    Titel :

    Power unit control system, power unit control method, and recording medium


    Weitere Titelangaben:

    动力单元控制系统、动力单元控制方法以及记录介质


    Beteiligte:
    TSUTSUMI HIROTAKA (Autor:in) / ETO MASASHI (Autor:in) / SAWAMURA HIROSHI (Autor:in)

    Erscheinungsdatum :

    08.09.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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