Main combustion chamber part test piece for simulating radial velocity field of outlet of gas compressor

A main combustion chamber and component testing technology, which is applied in the field of aero-engines, can solve the problems of large differences in parabolic distribution rules and the influence of the temperature field performance at the outlet of the combustion chamber, and achieve the effect of improving similarity

Pending Publication Date: 2022-03-22
AECC SICHUAN GAS TURBINE RES INST
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

In the state of the engine, when the air speed is as high as 120m/s~160m/s after being compressed by the compressor, affected by the shape of the compressor blades and the frictional resistance of the flow channel wall, the airflow of the compressor will generate The distribution law is a parabolic shape velocity field with a high center and a low top and bottom. There is a speed difference of about 5% between the airflow in the middle and the top and bottom. The gas flow rate of the channel affects the performance of the combustion chamber outlet temperature field. Therefore, it is very important to accurately simulate this parabolic velocity field on the combustion chamber c

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  • Main combustion chamber part test piece for simulating radial velocity field of outlet of gas compressor
  • Main combustion chamber part test piece for simulating radial velocity field of outlet of gas compressor
  • Main combustion chamber part test piece for simulating radial velocity field of outlet of gas compressor

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Embodiment Construction

[0025] It should be noted that, in the case of no conflict, the embodiments in the present application and the features in the embodiments can be combined with each other. The present invention will be described in detail below with reference to the accompanying drawings and examples.

[0026] Such as Figure 1 to Figure 10 As shown, the embodiment of the present invention provides a main combustion chamber component test piece for simulating the compressor outlet radial velocity field, including the front casing 1, the outer intake ring 2, the inner intake ring 3, and the compressor outlet velocity field Simulation board 4, outer ring adjusting gasket 5, inner ring adjusting gasket 6, outer ring flow channel 7, inner ring flow channel 8. The cylinder body of the front casing 1 is a stepped ring structure with a small front and a large rear. The small end flange 11 is connected to the equipment pipeline. The air in the front combustion chamber tester pipeline passes through t...

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Abstract

The invention provides a main combustion chamber component test piece for simulating a radial velocity field of an outlet of a gas compressor, and the test piece comprises a main combustion chamber which is provided with a combustion chamber inlet; an outer ring assembly and an inner ring assembly, the inner ring assembly is sleeved in the outer ring assembly, the outer ring assembly and the inner ring assembly are coaxially arranged at an interval, and a simulation channel is formed between the outer ring assembly and the inner ring assembly; and the gas compressor outlet velocity field simulation plate is provided with a plurality of gas inlet simulation holes, the gas compressor outlet velocity field simulation plate is arranged in the simulation channel, and the distance between the gas compressor outlet velocity field simulation plate and the combustion chamber inlet is adjustable. The device has the beneficial effects that the device can be assembled on a combustion chamber part test piece, a gas compressor outlet airflow radial velocity field under the engine condition is simulated at a combustion chamber inlet, and the similarity between the part test condition and the engine condition is improved.

Description

technical field [0001] The invention relates to the field of aero-engines, in particular to a main combustion chamber component test piece for simulating the radial velocity field at the outlet of a compressor. Background technique [0002] The combustion chamber component test is a common way to verify the performance of the combustion chamber. Compared with the engine or core machine test, the combustion chamber component test does not require the assembly of engine components other than the combustion chamber, such as fans, compressors or high and low pressure turbines, and the test cost is low. The development period is short, and the test risk is small. A large number of measuring points can be arranged to record the performance of the combustion chamber. The traditional method of testing the combustion chamber components is to heat and pressurize the air supplied by the gas source into the combustion chamber. The radial velocity field of the air at the inlet of the dif...

Claims

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Application Information

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IPC IPC(8): G01M15/04G01M15/02
CPCG01M15/04G01M15/02
Inventor 汪庆赵雅婷贺进黎武李朋玉张建国周昊航邢力周孙宇苏建
Owner AECC SICHUAN GAS TURBINE RES INST
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