The invention discloses a multidirectional thrust engine. The multidirectional thrust engine comprises an engine body (1), a forward thrust part (2), a stilling part (3) and a reverse thrust part (4), wherein the engine body (1), the forward thrust part (2) and the stilling part (3) are the existing patent contents. After the reverse thrust part (4) is added and the forward thrust part (2) is turned off, the reverse thrust part (4) is started, an electromagnetic valve (4-3) and a water pump (4-1) are turned on, water (2-7) enters a water pipe (4-2) and reaches a spraying pipe (4-4), and the water (2-7) sprayed out of an injection pipe (3-4) is sprayed out from the spraying pipe (4-4), so that the water (2-7) collides with one another, and the speed of the water (2-7) sprayed out of the spraying pipe (4-4) is reduced; when the backward thrust is greater than the forward thrust, an aircraft starts to decelerate. Certainly, when the multidirectional thrust engine is applied to products such as ships, trains and automobiles, the multidirectional thrust engine can also travel backwards.

    本发明公开了一种包括机体(1)、正向推力部分(2)、消力部分(3)和反向推力部分(4)的多向推力式发动机;机体(1)、正向推力部分(2)和消力部分(3)为已有专利内容。当增加了反向推力部分(4)之后,关闭正向推力部分(2)后,起动反向推力部分(4),打开电磁阀(4‑3)和水泵(4‑1),水(2‑7)进入水管(4‑2)到喷管(4‑4),从喷管(4‑4)喷出射向管(3‑4)喷出的水(2‑7),从而使水(2‑7)相碰,从而使喷管(4‑4)喷出的水(2‑7)速度减小;而向后推的力大于向前推力,飞机开始减速。当然,本发明如果在船舶、列车和汽车等产品上应用时,也可以向后方行驶。


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    Title :

    Multidirectional thrust engine


    Additional title:

    多向推力式发动机


    Contributors:

    Publication date :

    2021-12-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    F03G Feder-, Gewichts-, Trägheits- oder ähnliche Kraftmaschinen , SPRING, WEIGHT, INERTIA, OR LIKE MOTORS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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