To provide a combined engine that can smoothly perform flow path switching, and an aircraft.SOLUTION: A combined engine, which is mounted on an aircraft, comprises: a first engine corresponding to a first speed range; a second engine corresponding to a second speed range faster than the first speed range; a flow path part having a first flow path which is an air flow path in the first engine, and a second flow path which is an air flow path in the second engine; and a switching part which can switch opening/closing of the first flow path in the flow path part. The switching part has: a rotation component which is rotatable between a first position at which the first flow path is opened and a second position at which the first flow path is closed; and a slide component which slides thereby rotating the rotation component between the first position and the second position.SELECTED DRAWING: Figure 3

    【課題】流路の切替をスムーズに行うことが可能な複合エンジンおよび航空機を提供する。【解決手段】複合エンジンは、航空機に搭載される複合エンジンであって、第1速度域に対応する第1エンジンと、第1速度域よりも速い第2速度域に対応する第2エンジンと、第1エンジンの空気流路である第1流路と、前記第2エンジンの空気流路である第2流路とを有する流路部と、流路部における第1流路の開放/閉塞を切替可能な切替部と、を備え、切替部は、第1流路を開放する第1位置と、第1流路を閉塞する第2位置との間を回動可能な回動部材と、スライド移動することで、回動部材を第1位置と第2位置との間を回動させるスライド部材と、を有する。【選択図】図3


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    Title :

    COMBINED ENGINE AND AIRCRAFT


    Additional title:

    複合エンジンおよび航空機


    Contributors:

    Publication date :

    2025-01-17


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Japanese


    Classification :

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



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