首页> 外国专利> The principle and accelerating device of a comprehensive air purifying device utilizing discharge pressure gas of a device that utilizes engines of a spacecraft a ship an automobile an aircraft a power plant forward friction resistor

The principle and accelerating device of a comprehensive air purifying device utilizing discharge pressure gas of a device that utilizes engines of a spacecraft a ship an automobile an aircraft a power plant forward friction resistor

机译:利用航天器发动机,船舶,汽车,飞机,动力装置前向摩擦阻力器的装置的排出压力气体的综合空气净化装置的原理及加速装置

摘要

Based on a device that utilizes the engine and turbine of a spacecraft, a ship, an automobile, an aircraft, a power plant, and the like, pressure and exhaust gas utilized as thrust and energy is suctioned 100% so that the suctioned pressure helps an explosion process in the compression, explosion, and exhaust of various engine cylinders and that air pollution is reduced 100% (Fig. 50). An intake device is connected to a turbine used as thrust, increases the thrust by injecting pressure into the resistance area of blades, and removes an after-raising back blast by the blades of the turbine and the propellers of a helicopter or the like. Thrust pressure is increased by suctioning the back-blast pressure of the propellers and discharging the suctioned pressured in the direction of the rear of the propellers (Figs. 51, 51-1, and 51-2). Energy efficiency is increased and noise is removed by suctioning the remaining pressure from the suctioned thrust. The principle of a small suction, discharge, and compression tank that can be used in a narrow space when a compression tank is mounted is utilized. The additional principle of additional acceleration due to action and reaction is utilized. The principle of movement of a spacecraft (flying saucer) capable of preventing noise and pollution and moving by mounting the engine inside a moving device is utilized (Fig. 70-1).
机译:基于利用航天器,轮船,汽车,飞机,发电厂等的发动机和涡轮的装置,作为推力和能量利用的压力和废气被100%吸入,从而有助于在各种发动机气缸的压缩,爆炸和排气过程中发生爆炸,空气污染减少了100%(图50)。进气装置与用作推力的涡轮机相连,通过向叶片的阻力区域注入压力来增加推力,并消除涡轮机叶片和直升飞机等的螺旋桨产生的后鼓风。通过吸取螺旋桨的反吹压力并释放沿螺旋桨后部方向吸入的压力,可以提高推力压力(图51、51-1和51-2)。通过从吸入的推力中吸收剩余压力,可以提高能源效率并消除噪音。利用了在安装压缩罐时可在狭窄空间中使用的小型吸入,排放和压缩罐的原理。利用了由于作用和反作用而产生的附加加速度的附加原理。利用了能够防止噪音和污染并通过将发动机安装在移动装置内进行移动的航天器(飞碟)的移动原理(图70-1)。

著录项

  • 公开/公告号KR20200005833A

    专利类型

  • 公开/公告日2020-01-17

    原文格式PDF

  • 申请/专利权人 KIM JUU HWAN;

    申请/专利号KR20180079308

  • 发明设计人 KIM JUU HWAN;

    申请日2018-07-09

  • 分类号F02C9/18;F02B75/12;F02K9/60;

  • 国家 KR

  • 入库时间 2022-08-21 11:08:03

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