Centrifugal compressor with double pressure ratios

A centrifugal compressor and high-pressure technology, applied in the field of compressors, can solve the problems of adding centrifugal compressors, the number of centrifugal compressors cannot be increased at will, and the impact

Inactive Publication Date: 2017-06-13
SHENZHEN FUSTAR POWER TECH CO LTD
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  • Summary
  • Abstract
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  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] At present, whether the centrifugal compressor is single-stage or multi-stage, each impeller has only one annular outlet, and there is only one diffuser corresponding to it, which can only output gas with one pressure ratio. For working machines or special occasions, it can only be satisfied by increasing the number of centrifugal compressors, which not only increases the cost, but also is limited by the environmental space, and the number of centrifugal compressors cannot be increased at will, which will affect it

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Embodiment Construction

[0014] The present invention will be further described below in conjunction with the accompanying drawings and examples, but not as a limitation to the present invention.

[0015] exist figure 1 In the shown structure, the dual pressure ratio centrifugal compressor provided by the present invention includes a rotor and a stator. The rotor is composed of a main shaft 9 and an impeller sleeved on the main shaft 9. The impeller includes a blade 2 and a disc 1, and the chord length of the blade is The 3 / 4 part is designed as a stepped bending structure (in a stepped shape). When the centrifugal compressor is working, the compressed part of the air flow flows out from the bending part. Two annular outlets with different radii are set on the circumference of the impeller. Among them, the radius The large annular outlet is located at the end of the impeller blade, and its air velocity and pressure are relatively high, which is the high-pressure outlet 8. The annular outlet with a sma...

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Abstract

The invention belongs to the field of compressors, and relates to a dual-pressure-ratio centrifugal compressor, which includes a rotor and a stator. The rotor consists of a main shaft and an impeller sleeved on the main shaft. Annular outlets with different radii, among them, the annular outlet with large radius is located at the end of the impeller blade, which is a high-pressure outlet, and the annular outlet with a small radius is located at a certain position from the top to the end of the impeller blade, which is a low-pressure outlet. The diffuser is connected with the low-pressure diffuser, and the high-pressure diffuser and the low-pressure diffuser are respectively connected with the high-pressure air collecting pipe and the low-pressure air collecting pipe. The invention adopts the design concept of setting two air outlets on one impeller, so that the single-stage centrifugal compressor can output two kinds of gases with different pressure ratios to meet the needs of different purposes. The effect of the double ducting of the engine.

Description

technical field [0001] The invention belongs to the field of compressors, and relates to a centrifugal compressor, in particular to a dual-pressure-ratio centrifugal compressor capable of simultaneously outputting two gases with different pressure ratios. Background technique [0002] Centrifugal compressors, also known as radial compressors, generally refer to turbo compressors whose airflow mainly flows along the radial direction. Centrifugal compressors with an exhaust pressure less than 0.2 MPa are generally called centrifugal blowers. Centrifugal compressors are widely used in aviation, metallurgy, chemical and other fields. [0003] Centrifugal compressors usually consist of rotors, stators and bearings. The impeller and other parts are set on the main shaft to form the rotor, which is supported on the bearing and driven by power to rotate at high speed. The stator includes components such as casing, partition, seal, air inlet chamber and volute chamber. Elements su...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F04D29/28F04D29/30F04D29/44
CPCF04D29/284F04D29/30F04D29/441
Inventor 向兵
Owner SHENZHEN FUSTAR POWER TECH CO LTD
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