Centrifugal compressor gas-supplementing structure and compressor
Provided are a centrifugal compressor gas-supplementing structure and a compressor using the foregoing gas-supplementing structure. The centrifugal compressor gas-supplementing structure includes a annular gas-supplementing passage ( 6 ) for introducing supplemented gas into a gas passage ( 5 ) of a compressor, and an airflow-guiding assembly is provided in the annular gas-supplementing passage ( 6 ). The gas-guiding assembly is used for adjusting a direction of the supplemented gas flowing into the gas passage ( 5 ), so that an angle between a direction of the supplemented gas flowing into the gas passage ( 5 ) and a direction of an airflow in the gas passage ( 5 ) falls within a preset range, and a turbulence loss generated when the two passages of gas merge is avoided to the greatest extent, thereby improving cycle efficiency.
1. A centrifugal compressor gas-supplementing structure, comprising an annular gas-supplementing passage ( 6 ) for introducing supplemented gas into a gas passage ( 5 ) of a compressor, wherein an airflow-guiding assembly is provided in the annular gas-supplementing passage ( 6 ), and the airflow-guiding assembly is used for adjusting a direction of the supplemented gas flowing into the gas passage ( 5 ), so that an angle between a direction of the supplemented gas flowing into the gas passage ( 5 ) and a direction of an airflow in the gas passage ( 5 ) falls within a preset range, the airflow-guiding assembly comprises at least one group of guide vanes ( 7 ) provided in a circumferential direction of the annular gas-supplementing passage ( 6 ), wherein the preset range is −5° to 5°; wherein a thickness of each guide vane of the at least one group of guide vanes ( 7 ) is the same as a thickness of each return vane ( 41 ).
2. The centrifugal compressor gas-supplementing structure as claimed in claim 1 , wherein each guide vane of the at least one group of guide vanes ( 7 ) is of a flat plate shape, an inclined direction thereof is the same as an inclined direction of each return vane ( 41 ) of the compressor; or, each guide vane of the at least one group of guide vanes ( 7 ) is of a spiral shape, a spiral direction thereof is the same as an inclined direction of each return vane ( 41 ) of the compressor.
3. The centrifugal compressor gas-supplementing structure as claimed in claim 2 , wherein viewed from an axial direction of an impeller, each guide vane of the at least one group of the guide vanes ( 7 ) is provided radially outside of each return vane ( 41 ); and each guide vane of the at least one group of guide vanes ( 7 ) is provided on a spiral line extending outward in a spiral direction of each return vane ( 41 ), or the each guide vane of the at least one group of the guide vanes ( 7 ) is spaced from each corresponding return vane ( 41 ).
4. The centrifugal compressor gas-supplementing structure as claimed in claim 1 , wherein two opposite side surfaces of each guide vane of the at least one group of guide vanes ( 7 ) are connected with an inner wall of the annular gas-supplementing passage ( 6 ) respectively.
5. The centrifugal compressor gas-supplementing structure as claimed in claim 1 , wherein the number of guide vanes in the at least one group of guide vanes ( 7 ) is the same as the number of return vanes ( 41 ).
6. The centrifugal compressor gas-supplementing structure as claimed in claim 1 , wherein a supplemented gas outlet ( 62 ) of the gas passage ( 5 ) is provided at an inlet bend of a returning device ( 4 ) and/or an inlet of a next-stage impeller, each of the at least one group of guide vanes ( 7 ) is provided closer to the supplemented gas outlet ( 62 ) relative to a supplemented gas inlet ( 61 ).
7. The centrifugal compressor gas-supplementing structure as claimed in claim 2 , wherein two opposite side surfaces of each guide vane of the at least one group of guide vanes ( 7 ) are connected to an inner wall of the annular gas-supplementing passage ( 6 ) respectively.
8. The centrifugal compressor gas-supplementing structure as claimed in claim 3 , wherein two opposite side surfaces of each guide vane of the at least one group of guide vanes ( 7 ) are connected to an inner wall of the annular gas-supplementing passage ( 6 ) respectively.
9. The centrifugal compressor gas-supplementing structure as claimed in claim 2 , wherein the number of guide vanes in the at least one group of guide vanes ( 7 ) is the same as the number of return vanes ( 41 ).
10. The centrifugal compressor gas-supplementing structure as claimed in claim 3 , wherein the number of guide vanes in the at least one group of guide vanes ( 7 ) is the same as the number of return vanes ( 41 ).
11. A centrifugal compressor gas-supplementing structure, comprising an annular gas-supplementing passage ( 6 ) for introducing supplemented gas into a gas passage ( 5 ) of a compressor, wherein an airflow-guiding assembly is provided in the annular gas-supplementing passage ( 6 ), and the airflow-guiding assembly is used for adjusting a direction of the supplemented gas flowing into the gas passage ( 5 ), so that an angle between a direction of the supplemented gas flowing into the gas passage ( 5 ) and a direction of an airflow in the gas passage ( 5 ) falls within a preset range, the airflow-guiding assembly comprises at least one group of guide vanes ( 7 ) provided in a circumferential direction of the annular gas-supplementing passage ( 6 ), wherein a thickness of each guide vane of the at least one group of guide vanes ( 7 ) is the same as a thickness of each return vane ( 41 ).
12. A centrifugal compressor gas-supplementing structure, comprising an annular gas-supplementing passage ( 6 ) for introducing supplemented gas into a gas passage ( 5 ) of a compressor, wherein an airflow-guiding assembly is provided in the annular gas-supplementing passage ( 6 ), and the airflow-guiding assembly is used for adjusting a direction of the supplemented gas flowing into the gas passage ( 5 ), so that an angle between a direction of the supplemented gas flowing into the gas passage ( 5 ) and a direction of an airflow in the gas passage ( 5 ) falls within a preset range, the airflow-guiding assembly comprises at least one group of guide vanes ( 7 ) provided in a circumferential direction of the annular gas-supplementing passage ( 6 ), wherein the preset range is −5° to 5°; wherein the number of guide vanes in the at least one group of guide vanes ( 7 ) is the same as the number of return vanes ( 41 ).