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Method for cooling and discharging high-temperature tail gas of aircraft APU in ultralow-temperature environment in laboratory

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

Active Publication Date: 2022-01-07
CHINA AIRPLANT STRENGTH RES INST
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  • 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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  • Method for cooling and discharging high-temperature tail gas of aircraft APU in ultralow-temperature environment in laboratory
  • Method for cooling and discharging high-temperature tail gas of aircraft APU in ultralow-temperature environment in laboratory
  • Method for cooling and discharging high-temperature tail gas of aircraft APU in ultralow-temperature environment in 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 high-temperature tail gas of an aircraft APU in an ultralow-temperature environment in a laboratory. The method comprises the steps: 1, performing fan type selection; 2, giving a safe set temperature for high-temperature tail gas emission of the APU of the airplane; 3, determining the heating temperature of the electric tracing band; 4, estimating the mass flow rate of water for spraying and cooling; 5, primarily cooling and discharging the high-temperature tail gas of the aircraft APU; 6, tail gas emission temperature detection and adjustment; and 7, continuously cooling and discharging the high-temperature tail gas of the aircraft APU. The laboratory exhaust port temperature sensor, the laboratory environment temperature sensor and the laboratory environment pressure sensor are used for detecting whether the indoor environment is balanced or not under the APU driving condition, then the fan type meeting the requirement is selected, it is guaranteed that the temperature and pressure in a laboratory are stable, the safety of aircrafts and testers is guaranteed, the heating temperature of the electric tracing band is determined, the water supply pipe is effectively prevented from being frozen and blocked, and the stability is still achieved in an ultralow-temperature environment in a 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 Applications(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
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