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An electric environment control system for a multi-electric aircraft

A technology for multi-electric aircraft and control systems, which is used in aircraft parts, air handling equipment, transportation and packaging, etc., and can solve problems such as low energy efficiency, poor reliability, and complex aircraft and engine structures.

Active Publication Date: 2022-05-13
JINCHENG NANJING ELECTROMECHANICAL HYDRAULIC PRESSURE ENG RES CENT AVIATION IND OF CHINA
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AI Technical Summary

Problems solved by technology

Traditional aircraft use multiple secondary energy systems such as hydraulic pressure, air pressure, and machinery to ensure flight. The coexistence of multiple energy sources has led to problems such as complex structures of aircraft and engines, low energy efficiency, and poor reliability.

Method used

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  • An electric environment control system for a multi-electric aircraft

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Embodiment Construction

[0031] The technical solution of the present invention is as figure 1 shown.

[0032] An electric environment control system for a multi-electric aircraft, including an electric pressurized air source subsystem, an evaporative cycle refrigeration subsystem, and a liquid cycle cooling subsystem;

[0033] Among them, the electric pressurized air source subsystem includes a ram air intake device 1, an electric compressor 3, a motor 4, a heating / anti-breathing valve 5, a reverse flow cut-off valve 6, an ozone converter 7, a radiator 8, a temperature control valve 9 and electric fan13. The main function of the electric booster air source subsystem is to suck in external ambient air and pressurize it. Among them, the ram air intake device 1 absorbs the external ambient air from the outside, and prevents external foreign matter from entering the air intake of the aircraft with the external ambient air; The external ambient air is pressurized to obtain a high-pressure air source, a...

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Abstract

The invention belongs to the field of environment control for multi-electric aircraft, and relates to an electric environment control system for multi-electric aircraft, which includes an electric pressurized air source subsystem, an evaporation cycle refrigeration subsystem and a liquid cycle cooling subsystem. This solution uses electric compressors to provide air sources for aircraft, and combines evaporative cycle refrigeration technology and liquid cycle cooling technology to meet the needs of aircraft cabin pressurization, air supply, heating, and equipment cooling. It has the advantages of no engine bleed air, large cooling capacity, and cooling The characteristics of high heat flux density and excellent operating efficiency can ensure the safety and comfort of the personnel on board and the reliable operation of electronic equipment.

Description

technical field [0001] The invention belongs to the field of environment control for multi-electric aircraft, and in particular relates to an electric environment control system for multi-electric aircraft. Background technique [0002] The multi-electric aircraft uses electricity as the main secondary energy source of the aircraft, which has the advantages of high energy utilization rate, low pollutant emission, good system maintainability, and low operating cost. Traditional aircraft use multiple secondary energy systems such as hydraulic pressure, air pressure, and machinery to ensure flight. The coexistence of multiple energy sources has led to problems such as complex structures of aircraft and engines, low energy efficiency, and poor reliability. The multi-electric aircraft introduces the advanced technology of non-bleed air and electric drive, adopts non-bleed air engine, non-bleed air APU, starter / generator, electric environment control and other systems to replace t...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64D13/06
CPCB64D13/06B64D2013/0644
Inventor 孟繁鑫崔文君程定斌贺鹏程高赞军陆育良
Owner JINCHENG NANJING ELECTROMECHANICAL HYDRAULIC PRESSURE ENG RES CENT AVIATION IND OF CHINA
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