Environmental test cabin

An environmental test and test cabin technology, applied in the field of aero-engine test devices, can solve problems such as easy oil leakage, high construction cost, and complex structure, and achieve the effects of reduced design size, simple driving operation, and simple overall structure

Active Publication Date: 2021-04-30
AECC HUNAN AVIATION POWERPLANT RES INST
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  • Abstract
  • Description
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  • Application Information

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Problems solved by technology

[0008] The invention provides an environmental test chamber to solve the technical problems of the...

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  • Environmental test cabin
  • Environmental test cabin
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Embodiment Construction

[0031] The embodiments of the present invention will be described in detail below with reference to the accompanying drawings, but the present invention can be implemented in various ways defined and covered below.

[0032] refer to figure 1 with figure 2 , the preferred embodiment of the present invention provides an environmental test chamber, comprising: a hollow cylindrical test chamber body 10, the test chamber body 10 is arranged on the installation foundation along the horizontal direction, and the wall surface of the test chamber body 10 is provided with a Exit 101, for the machine to be tested and the test equipment to be tested to enter and exit the test cabin body 10. The entrance and exit 101 is provided with a sliding hatch for sealing the entrance and exit 101, the sliding hatch is connected to the test cabin 10, and is arranged to slide horizontally along the axial direction of the test cabin 10 to open or close the test cabin 10 .

[0033]In the environment...

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Abstract

The invention discloses an environmental test cabin comprising a hollow cylindrical test cabin body; the test cabin body is arranged on a mounting foundation in the horizontal direction, and the wall surface of the test cabin body is provided with an inlet and outlet for a to-be-tested machine for test and test equipment to enter and exit from the test cabin body. A sliding cabin door for sealing the inlet and outlet is arranged at the inlet and outlet, is connected to the test cabin body and is horizontally arranged in a sliding manner along the axial direction of the test cabin body so as to open or close the test cabin body. According to the sliding type cabin door, the design size of the sliding type cabin door can be effectively reduced, and then the construction cost of an environment test cabin is greatly reduced; the environmental test cabin is simple in overall structure and low in manufacturing cost, the driving force only needs to overcome the friction force generated when the sliding cabin door slides, and the driving force is small, so that the driving mechanism which is simple in structure, low in manufacturing cost and simple in driving operation can be selected to drive the sliding cabin door, and the defects of complex structure, large size, high cost, oil leakage and the like caused by hydraulic drive are overcome.

Description

technical field [0001] The invention relates to the technical field of aero-engine test devices, in particular to an environmental test chamber. Background technique [0002] Before the design of the aero-engine is finalized, it is necessary to complete high and low temperature start tests, and plateau start tests, etc. During the test, it is necessary to simulate the temperature and pressure of the engine inlet and the exhaust pressure. The 5km plateau starting test needs to simulate the atmospheric environment of 54.0kPa(A) / -17.5℃. In order to complete the above test, the engine under test is generally placed in the environmental test chamber, the inlet and outlet of the environmental test chamber are connected to the external air source, the air of a certain temperature and pressure enters from the inlet of the environmental test chamber, the engine inhales and burns, and the high-temperature gas discharged It is discharged through the outlet of the environmental test ch...

Claims

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Application Information

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IPC IPC(8): G01M15/02
CPCG01M15/02
Inventor 吴志勇吴施志陈国智熊荆江袁先圣杜庆林罗智浩
Owner AECC HUNAN AVIATION POWERPLANT RES INST
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