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Hydrogenation type multi-stage burning and explosion propelling device

A propulsion device and detonation technology, applied to space vehicle propulsion system devices, propulsion components, ship propulsion, etc., to improve efficiency and ensure gas flow direction

Active Publication Date: 2022-04-15
四川凯德源科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] The purpose of the present invention is to provide a hydrogenated multi-stage combustion and explosion propulsion device, which solves the problem that the prior art cannot quickly achieve better boosting performance in the case of short-distance vertical propulsion of the propeller

Method used

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  • Hydrogenation type multi-stage burning and explosion propelling device
  • Hydrogenation type multi-stage burning and explosion propelling device

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Embodiment Construction

[0030] Please also refer to the attached figure 1 - Instructions attached figure 2 , this embodiment provides a hydrogenated multi-stage combustion explosion propulsion device, the multi-stage hydrogen explosion propulsion device is mainly used to solve the problem that the existing technology cannot aim at the propeller in the case of a short-distance vertical propulsion to achieve a relatively fast boost In order to solve the problem of superior performance, the multi-stage hydrogen explosion propulsion device is already in the stage of practical use.

[0031] A hydrogenation type multi-stage combustion explosion propulsion device, including a device body 1, the device body 1 includes an energy storage component, a hydrogen production component, and a combustion component that are detachably connected from top to bottom in sequence, and the energy storage component and the combustion component are pressurized The tube group is connected.

[0032] It should be noted that t...

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Abstract

The invention relates to the technical field of jet propulsion, in particular to a hydrogenation type multistage fire blast propulsion device which comprises a device body, the device body comprises an energy storage assembly, a hydrogen production assembly and a combustion assembly which are detachably connected in sequence from top to bottom, and the energy storage assembly communicates with the combustion assembly through a pressurizing pipe set. And the energy storage assembly, the hydrogen production assembly, the combustion assembly and the pressurizing pipe set are arranged, so that the propelling operation of the propeller can be efficiently guaranteed, and the short-distance boosting performance optimization efficiency is improved.

Description

technical field [0001] The invention relates to the technical field of jet propulsion, in particular to a hydrogenation type multi-stage combustion explosion propulsion device. Background technique [0002] A propeller is a device that converts any form of energy into mechanical energy. The propulsion is generated by rotating blades in marine ships, and in aircraft, rockets and other equipment, through fuel combustion, etc. Among them, the more common propellers are aviation propellers, aerospace propellers, ship propellers, propeller propellers, jet propellers, etc. Propellers, water jet propellers and special propellers, among which there are many types of special propellers, such as variable pitch propeller propellers, blade geometry variation propellers, ducted propellers, straight wing propellers, jet propellers, ion propellers, Magnetic fluid thrusters, superconducting magnetic fluid thrusters, etc. [0003] Because of its simple structure, the thruster occupies a sm...

Claims

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Application Information

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IPC IPC(8): B64C15/02B64G1/26B64G1/40B63H11/14
CPCY02T70/50
Inventor 王常青王瑛李川刘建苹王钟浩张翔
Owner 四川凯德源科技有限公司
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