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Comprehensive heat management device suitable for hypersonic flight vehicle

A hypersonic and aircraft technology, applied to aircraft parts, transportation and packaging, air handling equipment, etc., can solve problems such as lack of overall planning, and achieve the effect of cost reduction and performance improvement

Active Publication Date: 2016-06-01
XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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  • Abstract
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  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The above-mentioned existing technologies often consider people or equipment, which are relatively independent and have no overall arrangement

Method used

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  • Comprehensive heat management device suitable for hypersonic flight vehicle

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Embodiment Construction

[0020] A comprehensive thermal management device suitable for hypersonic aircraft, including a temperature control valve 1, an evaporator 2, a fan 3, a cabin 4, a compressor 5, a condenser 6, a throttle valve 7, a shut-off valve 8, a second shut-off valve Shutoff valve 9, air hydrocarbon heat exchanger 10, flow regulating valve 11, filter 12, third shutoff valve 13, fourth shutoff valve 14, second fan 15, electronic equipment 16, pump 17, second pump 18. Liquid hydrocarbon heat exchanger 19, heater 20, electronic equipment 21, hydraulic system 22, second power system 23, engine 24, carburetor 25, high temperature catalytic cracking reactor 26, thermal protection system 27, heat pipe heat exchanger 28, hydrocarbon fuel tank 21, the fifth shut-off valve 30, the sixth shut-off valve 31, the third pump 32, the fourth pump 33, the fifth pump 34, the temperature control valve 35; it is characterized in that: the whole system is stored in The hydrocarbon fuel in the hydrocarbon fuel ...

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Abstract

The invention relates to a comprehensive heat management device suitable for a hypersonic flight vehicle. The comprehensive heat management device suitable for the hypersonic flight vehicle comprises a temperature control valve (1), an evaporator (2), a fan (3), a cabin (4), a compressor (5), a condenser (6), a throttling valve (7), a shutoff valve (8), a second shutoff valve (9), an air-hydrocarbon heat exchanger (10), a flow regulation valve (11), a filter (12), a third shutoff valve (13), a fourth shutoff valve (14), a second fan (15), electronic equipment (16), a pump (17) and the like. Hydrocarbon fuel stored in a hydrocarbon fuel tank (21) serves as a link of a whole system, so that all sub-systems are connected. The hydrocarbon fuel serves as the link of the whole system, all the sub-systems are connected, and thus heat management of the hypersonic flight vehicle is achieved. Compared with the prior art, the comprehensive heat management device has the advantages and positive effects of being improved in performance, reduced in cost and the like.

Description

Technical field [0001] The invention relates to an aircraft environment control technology. Background technique [0002] At present, the main technologies applied in the field of aircraft environment control at home and abroad include air circulation cooling technology, evaporative circulation cooling technology and liquid loop cooling technology. [0003] Air circulation cooling technology is widely used in various types of aircraft environmental control systems, but the coefficient of cooling performance is low, the reliability of the system is poor when the ground is stopped, and because the introduction of external ram air, the operating height and speed are limited to a certain extent , These all form a contradiction with the characteristics of severe aerodynamic heating, high flight altitude and high speed of hypersonic vehicles. [0004] Evaporative cycle cooling technology has the following characteristics: high coefficient of performance, good economy; small relat...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D13/08B64D13/00
Inventor 杨文强张翠峰
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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