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Closed impeller and gas compressor

A closed impeller and compressor technology, applied in the field of compressors, can solve the problems of increased axial size of compressors, increased processing and assembly errors, high processing and assembly difficulties, etc., to achieve improved flow field, increased rigidity, and light weight Effect

Pending Publication Date: 2021-03-16
刘慕华
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0007] In addition, the current compressors generally use a bearing group composed of multiple radial bearings and thrust bearings, which often require a long enough shaft for installation. The problem is that the axial dimension of the compressor increases. If this type of compressor When used in equipment such as micro gas turbine generator sets, it will increase the space occupied by the equipment and increase the overall weight, which is not conducive to integrated design; and the processing and assembly errors caused by arranging multiple bearings will increase, processing and assembly high difficulty

Method used

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Examples

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Embodiment 1

[0045] A closed impeller, including a rear cover 201, blades 202, a casing 203 and a front cover 204, such as Figure 1~5As shown, wherein, the rear cover 201 is arranged at the tail end of the sleeve body 203, and the center of the rear cover 201 and the sleeve body 203 is provided with an integrated through hole for sheathing and fixing on the rotating shaft 1; the blade 202 is arranged around the sleeve body 203 and faces Rotating in the same direction, one end of the blade 202 is connected to the outer wall of the sleeve body 203, and the other end is connected to the end face of the rear cover 201; A curved surface with a smooth transition along the outline of the ridge line of the blade 202, the back air surface is provided with grooves that match the ends of the blades 202, and the ends of the blades 202 corresponding to each groove are embedded in the grooves for tight fit connection; the blade 202, the rear cover 201 A flow channel 205 is formed between the front cove...

Embodiment 2

[0062] A compressor includes a rotating shaft 1, on which an impeller 2 and a motor 4 are sheathed; wherein, the structure of the impeller includes a rear cover 201, blades 202, a casing 203 and a front cover 204, such as Figure 1~5 As shown, wherein, the rear cover 201 is arranged at the tail end of the sleeve body 203, and the center of the rear cover 201 and the sleeve body 203 is provided with an integrated through hole for sheathing and fixing on the rotating shaft 1; the blade 202 is arranged around the sleeve body 203 and faces Rotating in the same direction, one end of the blade 202 is connected to the outer wall of the sleeve body 203, and the other end is connected to the end face of the rear cover 201; A curved surface with a smooth transition along the outline of the ridge line of the blade 202, the back air surface is provided with grooves that match the ends of the blades 202, and the ends of the blades 202 corresponding to each groove are embedded in the grooves...

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Abstract

The invention discloses a closed impeller. The closed impeller comprises a rear cover, blades, a sleeve body and a front cover, the front cover covers the blades, the front cover is in a circular truncated cone ring shape, an air inlet surface is a curved surface in smooth transition along the ridge outline of the blades, grooves matched with the ends of the blades are formed in a back air surface, and the ends, corresponding to the grooves, of the blades are embedded into the grooves to be connected in a close fit manner. A flow channel is formed among the blades, the rear cover and the frontcover; and the tail part of the front cover and the rear cover are separated into spaced air outlets by the blades, and air flows out of the air outlets from the front parts of the blades through theflow channel. The invention further discloses a gas compressor comprising the closed impeller structure. The closed impeller is provided with the front cover, so that gas leakage is little, frictionloss is small, flowing resistance is small, and efficiency is high in the working process. The front cover is made of carbon fiber composite materials, and the impeller is light in overall weight andhigh in strength. The splitter blades are arranged, so that blockage of inlet airflow can be reduced, the slip coefficient of an outlet of the impeller can be increased, the impeller efficiency is improved, and the overall efficiency of the gas compressor can be improved.

Description

technical field [0001] The invention relates to a closed impeller and an air compressor, belonging to the technical field of air compressors. Background technique [0002] Industrial gas turbines mainly include three major components: compressor, combustor and turbine. The compressor is a component that uses high-speed rotating blades to do work on the gas (mostly air) to increase the pressure of the gas. It compresses the air into high-temperature and high-pressure air, and then supplies fuel to the combustion chamber for combustion. The high-temperature and high-pressure gas generated expands in the turbine. acting. The impellers used in compressors are divided into open type, semi-open type and closed type. The characteristics of the three types of impellers are as follows: [0003] Open impeller: The friction loss and flow resistance are very large, the impeller efficiency is the lowest, and it is easy to generate vibration, so it is not suitable to work at high speed....

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F04D29/28F04D29/42F04D29/02F04D29/056F04D29/057
CPCF04D29/284F04D29/4206F04D29/023F04D29/056F04D29/057
Inventor 靳普
Owner 刘慕华
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