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Rotary knocking ramjet engine and hypersonic aircraft

A ramjet and detonation technology, which is applied in the field of aero-engines, can solve the problems of poor combustion organization ability and poor engineering applicability of low-activity hydrocarbon fuels, and improve the combustion organization ability of rotating detonation, strong flame stability, and promote engineering. Applied effect

Active Publication Date: 2019-12-06
NAT UNIV OF DEFENSE TECH
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The invention provides a rotary detonation ramjet and a hypersonic aircraft to solve the technical problems of the existing rotary detonation ramjet, which have poor combustion organization ability and poor engineering applicability of low-activity hydrocarbon fuel

Method used

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  • Rotary knocking ramjet engine and hypersonic aircraft

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Embodiment Construction

[0027] Embodiments of the present invention will be described in detail below in conjunction with the accompanying drawings, but the present invention can be implemented in many different ways defined and covered by the claims.

[0028] refer to figure 1, the preferred embodiment of the present invention provides a rotary detonation ramjet engine, comprising: a casing 10, the casing 10 is in the shape of a hollow cylinder connected at both ends. Also includes a central cone 20, the rear body 21 of the central cone 20 extends into the housing 10 from the air intake end of the housing 10 and is connected to the housing 10, and the gap between the housing 10 and the rear body 21 forms the introduction of air into the housing 10 The drainage channel 30 inside, the cavity between the rear end surface of the rear body 21 and the inner wall of the shell 10 forms the detonation chamber 12 communicated with the drainage channel 30, and the tail nozzle 13 communicated with the detonatio...

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Abstract

The invention discloses a rotary knocking ramjet engine and a hypersonic aircraft. The rotary knocking ramjet engine comprises an outer shell and further comprises a central cone, wherein the outer shell takes the shape of a hollow cylinder, and two ends of the hollow cylinder communicate with each other; the rear body of the central cone extends into the outer shell from the air inlet end of theouter shell and is connected with the outer shell; a flow guide channel used for the introduction of air into the outer shell is formed in a gap between the outer shell and the rear body; a knocking room and an exhaust pipe are formed in a cavity between the rear end surface of the rear body and the inner wall of the outer shell; the knocking room communicates with the flow guide channel; an nozzle of the exhaust spray pipe communicates with the exhaust spray pipe; a plurality of outer nozzles are processed on the outer wall of the outer shell, and two ends of each outer nozzle communicate with a fuel source and the flow guide channel correspondingly; and / or a plurality of inner nozzles are processed on the outer wall of the rear body, and two ends of each inner nozzle communicate with thefuel source and the flow guide channel correspondingly. According to the rotary knocking ramjet engine disclosed by the invention, the rotary knocking combustion organization capability is strong andthe flame combustion stability is high, so that the stable combustion of the rotary knocking of low-activity hydrocarbon fuels such as liquid kerosene and acetylene can be easier achieved.

Description

technical field [0001] The invention relates to the field of aero-engines, in particular to a rotary detonation ramjet engine. In addition, the present invention also relates to a hypersonic aircraft comprising the above-mentioned rotary detonation ramjet engine. Background technique [0002] Hypersonic aircraft is a strategic high-tech that achieves high-speed defense penetration, 2-hour global reach, and low-cost space entry. Its development will change the shape of future warfare. It is a new commanding height of aerospace technology in the 21st century. Its core is hypersonic propulsion technology. Continuous rotary detonation is a form of realization of detonation engine, which usually adopts an annular combustion chamber, only needs one ignition to work continuously, can provide stable thrust, and has broad application prospects. Recently, Liu Shijie, Wang Chao, etc. passed the direct-connection test (【Liu Shijie, Wang Chao, Jiang Luxin, Liu Weidong, Lin Zhiyong, Cont...

Claims

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Application Information

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IPC IPC(8): F02K7/14F02K1/78F02C7/22
CPCF02C7/22F02C7/222F02K1/78F02K7/14
Inventor 刘世杰刘卫东张海龙孙明波彭皓阳王翼蒋露欣任春雷
Owner NAT UNIV OF DEFENSE TECH