The invention discloses a module rotor engine, and relates to the technical field of airspace engines. According to the thought of the invention, the stability and the precession of the gyroscope adopting the split rotor module (4) are different from those of a common gyroscope, when the split rotor module (4) rotates along with the connecting rod (6) in the vertical stage (15), the stability and the precession of the gyroscope act, which is opposite to the result of the common gyroscope, so that the stability and the precession of the gyroscope are improved. The precession moment separates the rotating surface of the pendulum bob (10) from the rotating surface of the split rotor module (4) to generate intersection, so that the connecting rod (6) needs a larger force to overcome the stability of the gyroscope when rotating in the vertical stage (15), thereby generating a larger upward counter-acting force.

    本发明公开了模块转子引擎,涉及航天发动机技术领域。本发明的思路是采用分体式转子模块(4)的陀螺仪的稳定性和进动性与普通陀螺仪的稳定性和进动性有差异,当分体式转子模块(4)跟随连杆(6)在垂直阶段(15)一起旋转时,陀螺仪的稳定性和进动性起作用,这和普通陀螺仪结果是相反的,进动力矩使摆锤(10)的旋转面与分体式转子模块(4)的旋转面分开,产生了交叉,使连杆(6)在垂直阶段(15)旋转时需要较大的力克服陀螺仪的稳定性,从而产生一个较大的向上的反作用力。


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    Titel :

    Modular rotor engine


    Weitere Titelangaben:

    模块转子引擎


    Beteiligte:
    ZHANG JING (Autor:in)

    Erscheinungsdatum :

    09.05.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS



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