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Metal powder fuel air-water cross-medium engine and control method thereof

A metal powder and cross-media technology, which is applied in the field of metal powder fuel air-water cross-media engine and its control, can solve the problems of limited flight speed range and unsatisfactory performance requirements, and achieve the effects of high energy, compact structure and high performance

Active Publication Date: 2022-04-15
XIAN AEROSPACE PROPULSION INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] In order to solve the problem that the existing air-water trans-medium engine has a limited flight speed range and the performance does not meet the requirements, the present invention proposes a metal powder fuel air-water trans-media engine , the engine has the ability to jump into water and air with multiple frequencies, fly at Ma0-4.0 speed, and work at high speed under water

Method used

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  • Metal powder fuel air-water cross-medium engine and control method thereof
  • Metal powder fuel air-water cross-medium engine and control method thereof
  • Metal powder fuel air-water cross-medium engine and control method thereof

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Embodiment Construction

[0028] The present invention will be described in detail below in conjunction with the accompanying drawings and specific embodiments. Those skilled in the art should understand that these embodiments are only used to explain the technical principles of the present invention, and are not intended to limit the protection scope of the present invention.

[0029] The invention provides a metal powder fuel air-water trans-medium engine and its control method. The engine uses gas-fluidized high-energy metal powder as a propellant that reacts with water and air. The engine has a simple system and a high density specific impulse. features.

[0030] Such as Figure 1 to Figure 4As shown, the metal powder fuel air-water cross-medium engine of the present invention includes an air inlet 1, an ATR core machine 3, an air inlet channel switching valve 2, a flow mixer 6, a combustion chamber 8, a water secondary jet injector 9, and a nozzle 10. Flame stabilizer 7, ram valve 17, combustion...

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Abstract

The invention provides a metal powder fuel air-water cross-medium engine and a control method thereof. The engine has the capabilities of jumping water and air at multiple frequencies, flying at the speed of Ma0-4.0 and working at a high speed underwater. According to the metal powder fuel air-water cross-medium engine, an air turbine rocket engine mode, a subsonic combustion ramjet engine mode and a water ramjet engine mode are organically combined, the engine can work in water and air media through engine flow channel adjustment, the working modes can be automatically switched according to the external environment, and the engine has the wide speed range and high-performance working capacity.

Description

technical field [0001] The invention belongs to the field of air-water cross-medium engines, in particular to a metal powder fuel air-water cross-medium engine and a control method thereof. Background technique [0002] The ramjet engine is a kind of air jet engine that uses the deceleration and supercharging effect of high-speed air flow to complete the supercharged combustion and thus work. It usually consists of an intake port, a combustion chamber and a nozzle. During flight, the airflow decelerates while passing through the intake port, and the static pressure increases. The pressurized air enters the combustion chamber and mixes with fuel to organize combustion. The high-temperature gas generated expands and accelerates in the nozzle and is discharged to generate thrust. [0003] The fuel specific impulse of the ramjet engine is much higher than that of the existing turbojet engine and compression ignition ramjet engine, which can achieve higher flight speed and altitu...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F02K7/10
Inventor 杜泉王玉峰呼延霄朱向东莫建伟陈磊石腾
Owner XIAN AEROSPACE PROPULSION INST
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