The invention provides an aircraft engine construction system integrating a windlass lever principle. The aircraft engine construction system is mainly characterized in that an original engine combustion chamber is divided into three (or six) independent combustion chambers according to the air pressure and power principle in combination with the windlass lever principle, then the air is sprayed into a concave pocket type blade in an annular semi-closed air chamber to drive an air compression blade to rotate around a shaft, and meanwhile air compression spraying is achieved, so that the air pressure and power are achieved to the maximum extent with less fuel consumption.

    本发明提供了一种综合辘轳杠杆原理的飞机发动机构造系统,主要是根据空气压力和动力原理结合辘轳杠杆原理将原有发动机燃烧室独立成三个(或六个),然后喷向轮环状半封闭气室内部凹兜型叶片带动压气叶片绕轴旋转同时实现压气喷发以较少的燃料消耗最大化实现空气压力和动力的发明。


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    Titel :

    Aircraft engine construction system integrating windlass lever principle


    Weitere Titelangaben:

    一种综合辘轳杠杆原理的飞机发动机构造系统


    Beteiligte:
    ZHOU WEIPING (Autor:in)

    Erscheinungsdatum :

    07.12.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    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 / F23R Erzeugen von Verbrennungsprodukten hohen Druckes oder hoher Geschwindigkeit, z.B. Gasturbinenbrennkammern , GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS



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