Electromagnetic fluid vortex power device

A power device and fluid vortex technology, applied in the field of electromagnetic fluid vortex power devices, can solve problems such as difficulty in starting work, heavy engine weight, and difficulty in ignition, etc.

Pending Publication Date: 2021-12-10
陈晓彬
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] Most of the energy used in the current aviation and aerospace engines is chemical fuels, which will generate high temperature and high pressure during operation, which has very high requirements on the performance of the engine blades, resulting in protracted engine development cycles; the combustion efficiency of chemical fuels has also become a

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  • Electromagnetic fluid vortex power device
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Embodiment Construction

[0026] The present invention will be further described below in conjunction with drawings and embodiments. The following examples are used to illustrate the present invention, but are not intended to limit the protection scope of the present invention.

[0027] See figure 1 and figure 2 As shown, the electromagnetic fluid vortex power device of the present invention is composed of three structures: a main air inlet, an auxiliary air inlet and a vortex hole. The auxiliary air inlet 4 is located on both sides of the main air inlet, and is separated from the guide wall 6, and is embedded with each other to form a tubular shape; the main air inlet 1 and the auxiliary air inlet 4 are connected by the vortex hole 5; The side wall of the main air inlet 1 is equipped with an electromagnetic starter 2 and an electromagnetic thruster 3; the electromagnetic starter 2, the electromagnetic thruster 3 and the vortex hole 5 can all generate intersecting electric fields and magnetic fields...

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Abstract

The invention discloses an electromagnetic fluid vortex power device which comprises a main air inlet channel, auxiliary air inlet channels and vortex holes. The auxiliary air inlet channels are distributed on the two sides of the main air inlet channel and separated by a flow guide wall, the side walls of the main air inlet channel and the auxiliary air inlet channels are communicated through the vortex holes to form a communicated space, and an electromagnetic starter and an electromagnetic propeller are installed on the side wall of the main air inlet channel. When a power device is started to work, the structures of the electromagnetic starter and the vortex holes can enable working media to generate conductivity and generate intersected electromagnetic and magnetic fields, so that the working media flow under the action of Lorentz force; and working media in the auxiliary air inlet channels flow into the main air inlet channel through the vortex holes, vortexes are formed, and then the electromagnetic propeller is started, so that stable and continuous work is achieved. The power device takes electric power as working energy, is light in weight, high in working efficiency and large in thrust, can normally work in a region with lower oxygen content, and is wide in application range.

Description

technical field [0001] The invention relates to a power device, in particular to an electromagnetic fluid vortex power device for aviation, aerospace and ship power systems. Background technique [0002] Most of the energy used in the current aviation and aerospace engines is chemical fuel, which will generate high temperature and high pressure during operation, which has very high requirements on the performance of the engine blades, resulting in protracted engine development cycles; the combustion efficiency of chemical fuels has also become a problem, and a large number of The blades and other equipment can only work normally when they are installed in the engine, which causes the weight of the engine to be heavy, which affects the overall performance of the aircraft; and in a specific area, the oxygen content is low, which makes it difficult to ignite and start work. [0003] In order to overcome the above-mentioned defects, the electromagnetic fluid vortex power device ...

Claims

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Application Information

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IPC IPC(8): F03H1/00
CPCF03H1/0081Y02E10/72
Inventor 陈晓彬
Owner 陈晓彬
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