Test system for aircraft climate environment test and configuration method thereof

A climate environment and test system technology, which is applied in the direction of aircraft component testing, climate sustainability, building types, etc., can solve problems such as errors and resource waste experiments, and achieve easy operation, reduce construction costs, and save equipment construction area Effect

Active Publication Date: 2022-02-18
CHINA AIRPLANT STRENGTH RES INST
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, when switching between aircrafts of different sizes, the simulated experimental cabin is likely to cause a certain waste of resources or experimental errors.

Method used

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  • Test system for aircraft climate environment test and configuration method thereof
  • Test system for aircraft climate environment test and configuration method thereof
  • Test system for aircraft climate environment test and configuration method thereof

Examples

Experimental program
Comparison scheme
Effect test

Embodiment 1

[0045] Such as figure 2 Shown, a kind of test system of aircraft climate environment test, comprises: the big environment cabin 1 and the small environment cabin 2 that are arranged side by side front and back, the first annex building 11 that is positioned at the big environment cabin 1 side and is positioned at the big environment cabin 1 another The second annex building 12 on the side, the third annex building 21 on one side of the small environment cabin 2, the power assembly 3 located at the rear of the small environment cabin 2, the power assembly 3 includes a warehouse 31, a boiler room 32, and a compressed air station arranged side by side. 33 and the circulating water pump room 34, the exhaust space of the exhaust pipe 22 is reserved between the boiler room 32 and the compressed air station 33, a circulating water pool 35 is arranged underground on one side of the circulating water pump room 34, and a There is a circulating cooling tower 36 connected to the circulat...

Embodiment 2

[0050] The difference between this embodiment and Embodiment 1 lies in that the thickness of the interlayer 4 is different, and the thickness of the interlayer 4 is 1 m.

Embodiment 3

[0052] The difference between this embodiment and Embodiment 1 lies in that the thickness of the interlayer 4 is different, and the thickness of the interlayer 4 is 2 m.

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Abstract

The invention discloses a test system for an aircraft climate environment test and a configuration method thereof, and belongs to the technical field of aircraft tests. The test system for the aircraft climate environment test comprises a large environment chamber, a small environment chamber, a first auxiliary building located on one side of the large environment chamber, a second auxiliary building located on the other side of the large environment chamber, a third auxiliary building located on one side of the small environment chamber and a power assembly located behind the small environment chamber, wherein the large environment chamber and the small environment chamber are arranged side by side front and back. Interlayers are arranged between the inner walls and the outer walls of the large environment chamber and the small environment chamber, an isolation door is arranged at the joint of the large environment chamber and the small environment chamber, a water collecting tank is arranged under the ground of the large environment chamber and the small environment chamber, and a drainage assembly is arranged in the water collecting tank. According to the test system for the aircraft climate environment test, factors such as functional requirements, building structures, environment simulation systems and power supply of an ultra-large climate environment laboratory are comprehensively considered, iterative optimization is carried out on the laboratory layout, and the overall layout suitable for the ultra-large comprehensive climate environment laboratory is formed.

Description

technical field [0001] The invention relates to the technical field of aircraft testing, in particular to a test system and a configuration method for aircraft climate environment testing. Background technique [0002] Aircraft flight test refers to various test experiments conducted by the aircraft under the real flight environment conditions. The design and test of the aircraft need to go through repeated all-round simulation tests before entering the flight test stage. Therefore, in order to complete the simulation tests under various conditions of the aircraft, a large-scale climate environment laboratory is needed. [0003] The climate and environment laboratory is used for climate and environment adaptability tests of large-scale equipment such as aviation aircraft. Snowfall, fog, wind, icing / freezing rain, wind blowing rain, wind blowing snow and other climate environments. The volume of the climate and environment laboratory, the scale and complexity of the environ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64F5/60E04H1/00
CPCB64F5/60E04H1/00Y02P70/50
Inventor 王彬文成竹吴敬涛任战鹏刘海燕
Owner CHINA AIRPLANT STRENGTH RES INST
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