The invention discloses an engine control mechanism of a double-engine airship. The engine control mechanism comprises an engine control board, two mixing ratio control steel cables, two throttle valve control steel cables and an engine end control assembly. The two engine end mixing ratio control assemblies and the two engine end throttle valve control assemblies are arranged at the engine end of the double-engine airship; the engine control console comprises two mixing ratio control rod assemblies, two throttle valve rod control rod assemblies and a supporting structure. The two mixing ratio control rod assemblies are connected with the two engine end mixing ratio control assemblies through the two mixing ratio control steel cables in a one-to-one correspondence mode, and the two throttle valve rod control rod assemblies are connected with the two engine end throttle valve control assemblies through the two throttle valve control steel cables in a one-to-one correspondence mode. According to the technical scheme, the problem that an existing push-and-pull steel cable type control structure of an airship piston engine is difficult to control the linear motion state of the push-and-pull steel cable, and consequently the engine is difficult to achieve the optimal control effect is solved.

    本发明公开了一种双发飞艇的发动机操纵机构,包括:发动机操纵台、2根混合比操纵钢索、2根节气门操纵钢索,以及发动机端操纵组件;设置在双发飞艇发动机端的2个发动机端混合比操纵组件和2个发动机端节气门操纵组件;发动机操纵台包括:2个混合比操纵杆组件、2个节气门杆操纵杆组件和支撑结构;2个混合比操纵杆组件通过2根混合比操纵钢索一一对应的与2个发动机端混合比操纵组件连接,2个节气门杆操纵杆组件通过2根节气门操纵钢索一一对应的与2个发动机端节气门操纵组件连接。本发明技术方案解决了飞艇活塞发动机的现有推拉钢索式控制结构难以保证对推拉钢索的直线运动状态控制,从而导致发动机难以实现最佳控制效果的问题。


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Engine control mechanism of double-engine airship


    Weitere Titelangaben:

    一种双发飞艇的发动机操纵机构


    Beteiligte:
    TIAN JUN (Autor:in) / WANG GENHUI (Autor:in) / JIN FENG (Autor:in) / LUO JIANGUO (Autor:in) / ZHAO BEIXING (Autor:in) / LONG FEI (Autor:in) / LAI ZHENHUA (Autor:in) / JIANG PENGCHENG (Autor:in)

    Erscheinungsdatum :

    09.04.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64B LIGHTER-THAN-AIR AIRCRAFT , Luftfahrzeuge leichter als Luft / F02D CONTROLLING COMBUSTION ENGINES , Steuern oder Regeln von Brennkraftmaschinen



    The wright 6-cylinder airship engine

    Engineering Index Backfile | 1922


    Packard model 1551 300 hp. airship engine

    Vincent, J.G. | Engineering Index Backfile | 1923




    Vertical control test flight method for manned airship in troposphere without engine power

    WANG BINBIN / TIAN RUI / XI YI et al. | Europäisches Patentamt | 2024

    Freier Zugriff