液压推力驱动式发动机

文档序号:1843088 发布日期:2021-11-16 浏览:24次 >En<

阅读说明:本技术 液压推力驱动式发动机 (Hydraulic thrust driven engine ) 是由 李晓亮 于 2021-08-25 设计创作,主要内容包括:本发明公开了一种包括推力部分(1)和去反力部分(2)的液压推力驱动式发动机,进水管(1-2)一端与水泵(1-1)相联,另一端放在水(1-6)中;支架(2-3)和长支架(2-4)焊在水池(1-5)上,水泵(2-1)一台安在水池(1-5)上,另外二台分别安在支架(2-3)和长支架(2-4)上,进水管(2-2)一端与水泵(2-1)相联,另一端放在水(1-6)中。起动水泵(1-1)和所有水泵(2-1),水泵(1-1)喷出来的水(1-6)与水泵(2-1)喷出来的水(1-6)相互汇合后,使得水泵(1-1)向前受到的推力时喷出来的水(1-6)向后对水池(1-5)的推力大,发动机对外合力为向前的一个推力。(The invention discloses a hydraulic thrust drive type engine comprising a thrust part (1) and a reaction removing part (2), wherein one end of a water inlet pipe (1-2) is connected with a water pump (1-1), and the other end of the water inlet pipe is placed in water (1-6); the support (2-3) and the long support (2-4) are welded on the water pool (1-5), one water pump (2-1) is arranged on the water pool (1-5), the other two water pumps are respectively arranged on the support (2-3) and the long support (2-4), one end of the water inlet pipe (2-2) is connected with the water pump (2-1), and the other end is arranged in the water (1-6). The water pump (1-1) and all the water pumps (2-1) are started, water (1-6) sprayed by the water pump (1-1) and water (1-6) sprayed by the water pump (2-1) are mutually converged, so that the water (1-6) sprayed by the water pump (1-1) has large backward thrust on the water pool (1-5) when the water pump (1-1) receives forward thrust, and the external resultant force of the engine is forward thrust.)

液压推力驱动式发动机

一、领域:

本发明涉及做为推动飞机航行的发动机。

二、背景:

已有的飞机发动机,一种是螺旋浆式的;另外有喷气式的。但是它们都是以后面的空气作为反作用力的。由于空气本身可以流动,同时,也具有可压缩性,所以,当作用力的气体向后喷出后,所受到的反作用力比较小,工作效率低,能耗大,飞行航程短,载荷小。

三、

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