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Aircraft apu high-temperature exhaust gas cooling and emission method in ultra-low temperature environment in the laboratory

A kind of exhaust emission and laboratory technology, applied in the direction of aircraft component testing, etc., can solve the problems of aircraft test personnel's safety threat, damage temperature, pressure environment, etc., to achieve the effect of easy promotion and use, ensure heating temperature, and prevent short-circuit burnout

Active Publication Date: 2022-02-25
CHINA AIRPLANT STRENGTH RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

If the high-temperature and high-pressure exhaust gas discharged by the APU is directly discharged into the laboratory, it will not only destroy the temperature and pressure environment in the laboratory, but also accumulate exhaust gas in the laboratory, which will also pose a threat to the safety of the laboratory, aircraft and even test personnel.

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  • Aircraft apu high-temperature exhaust gas cooling and emission method in ultra-low temperature environment in the laboratory
  • Aircraft apu high-temperature exhaust gas cooling and emission method in ultra-low temperature environment in the laboratory
  • Aircraft apu high-temperature exhaust gas cooling and emission method in ultra-low temperature environment in the laboratory

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Embodiment Construction

[0049] Such as Figure 1 to Figure 6 As shown, the aircraft APU high-temperature tail gas cooling and discharging method under the ultra-low temperature environment in the laboratory of the present invention uses the aircraft APU exhaust system in the laboratory to discharge and cool the aircraft APU exhaust. The aircraft APU exhaust system in the laboratory includes for The laboratory 6 containing the aircraft 7 and the aircraft APU exhaust equipment that outputs the aircraft APU exhaust to the outside, the aircraft APU exhaust equipment includes an initial adjustment pipeline 1, a drainage pipeline 2, a butterfly valve 3 and a fan 4 connected in sequence, and the initial adjustment pipeline 1 is provided with a spray cooling device 5, and the spray cooling device 5 includes a plurality of spray cooling mechanisms uniformly arranged along the length direction of the initial adjustment pipeline 1, and the spray cooling mechanism includes a water supply pipe arranged outside the...

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Abstract

The invention discloses a method for cooling and discharging aircraft APU high-temperature exhaust gas in an ultra-low temperature environment in a laboratory, comprising the steps of: 1. selecting the type of fan; Heating temperature; 4. Estimated spray cooling water mass flow; 5. Aircraft APU high-temperature exhaust primary cooling discharge; 6. Exhaust emission temperature detection and adjustment; 7. Aircraft APU high-temperature exhaust continuous cooling discharge. The invention utilizes the exhaust port temperature sensor in the laboratory, the environmental temperature sensor in the laboratory and the environmental pressure sensor in the laboratory to detect whether the indoor environment is balanced when the APU is running, and then selects the type of fan that meets the requirements, ensuring the temperature and pressure in the laboratory The stability ensures the safety of the aircraft and test personnel, determines the heating temperature of the electric heating cable, effectively prevents the water supply pipe from freezing, freezing and blocking, and still has stability in the ultra-low temperature environment in the laboratory.

Description

technical field [0001] The invention belongs to the technical field of APU drainage and exhaust cooling during the opening process of an aircraft APU in a closed laboratory, and specifically relates to a method for cooling and discharging an aircraft APU high-temperature exhaust gas in a laboratory at an ultra-low temperature environment. Background technique [0002] To carry out climate experiments in the full-aircraft climate laboratory, it is necessary to turn on the aircraft APU to provide power for the aircraft. If the high-temperature and high-pressure exhaust gas discharged by the APU is directly discharged into the laboratory, it will not only destroy the temperature and pressure environment in the laboratory, but also accumulate in the laboratory, which will also pose a threat to the safety of the laboratory, the aircraft and even the test personnel. Therefore, when the aircraft APU is turned on in the laboratory, the exhaust gas needs to be discharged outside the ...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B64F5/60
CPCB64F5/60
Inventor 成竹吴敬涛任战鹏李剑杜文辉
Owner CHINA AIRPLANT STRENGTH RES INST