초록 ▼

The centrifugal compressor of the present invention is equipped with a plurality of vane groups (A, B) comprised of a plurality of vanes (16A, 16B) disposed in the peripheral direction of an impeller (12) so as to be concentric about the center of an axis of rotation (15) of the impeller, and the in

The centrifugal compressor of the present invention is equipped with a plurality of vane groups (A, B) comprised of a plurality of vanes (16A, 16B) disposed in the peripheral direction of an impeller (12) so as to be concentric about the center of an axis of rotation (15) of the impeller, and the individual vanes (16A) belonging to vane group (A) nearest to the impeller are able to rotate. Since diffuser efficiency decreases if the intake flow volume of the impeller changes and the flow of gas is unable to easily continue from the vanes (16A) to vanes (16B), the vanes (16A) are rotated to change the inclination of the direction of a wing center line on their front edges so as to coincide with the direction of the flow of gas discharged from the impeller. As a result, diffuser efficiency is maintained at a high level even if the intake flow volume of the impeller is changed.

대표청구항 ▼

The centrifugal compressor of the present invention is equipped with a plurality of vane groups (A, B) comprised of a plurality of vanes (16A, 16B) disposed in the peripheral direction of an impeller (12) so as to be concentric about the center of an axis of rotation (15) of the impeller, and the in

The centrifugal compressor of the present invention is equipped with a plurality of vane groups (A, B) comprised of a plurality of vanes (16A, 16B) disposed in the peripheral direction of an impeller (12) so as to be concentric about the center of an axis of rotation (15) of the impeller, and the individual vanes (16A) belonging to vane group (A) nearest to the impeller are able to rotate. Since diffuser efficiency decreases if the intake flow volume of the impeller changes and the flow of gas is unable to easily continue from the vanes (16A) to vanes (16B), the vanes (16A) are rotated to change the inclination of the direction of a wing center line on their front edges so as to coincide with the direction of the flow of gas discharged from the impeller. As a result, diffuser efficiency is maintained at a high level even if the intake flow volume of the impeller is changed. ressor according to claim 3 wherein, said rotatable vanes stand on flanges independent from the walls that form a portion of said diffuser separated in the direction of said axis of rotation with said vanes interposed between, and rotate with said flanges. 6. The centrifugal compressor according to claim 4 wherein, said rotatable vanes stand on flanges independent from the walls that form a portion of said diffuser separated in the direction of said axis of rotation with said vanes interposed between, and rotate with said flanges. 7. The centrifugal compressor according to claim 3 wherein, the vane group adjacent on the outside to said rotatable vanes is able to turn in said peripheral direction while maintaining the arrangement of the individual vanes. 8. The centrifugal compressor according to claim 4 wherein, the vane group adjacent on the outside to said rotatable vanes is able to turn in said peripheral direction while maintaining the arrangement of the individual vanes. 9. The centrifugal compressor according to claim 5 wherein, the vane group adjacent on the outside to said rotatable vanes is able to turn in said peripheral direction while maintaining the arrangement of the individual vanes. 10. The centrifugal compressor according to claim 6 wherein, the vane group adjacent on the outside to said rotatable vanes is able to turn in said peripheral direction while maintaining the arrangement of the individual vanes. 11. The centrifugal compressor according to any of claims 3 to 10 wherein, the ratio of the chord length to the interval between adjacent vanes in the peripheral direction of said rotatable vanes is less than 1.0. 12. The centrifugal compressor according to any of claims 3 to 10 wherein the ratio of the chord length to the interval between adjacent vanes in the peripheral direction of those vanes belonging to the vane group adjacent on the outside to said rotatable vanes is from 0.5 to 2.0. 13. The centrifugal compressor according to claim 11 wherein the ratio of the chord length to the interval between adjacent vanes in the peripheral direction of those vanes belonging to the vane group adjacent on the outside to said rotatable vanes is from 0.5 to 2.0. 14. The centrifugal compressor according to any of claims 1 to 10 wherein the ratio of the length from the center of said impeller to the front edge of a vane belonging to the vane group at a position nearest said impeller toward the outer radius of said impeller is from 1.05 to 1.30. 15. The centrifugal compressor according to claim 11 wherein the ratio of the length from the center of said impeller to the front edge of a vane belonging to the vane group at a position nearest said impeller toward the outer radius of said impeller is from 1.05 to 1.30. 16. The centrifugal compressor according to claim 12 wherein the ratio of the length from the center of said impeller to the front edge of a vane belonging to the vane group at a position nearest said impeller toward the outer radius of said impeller is from 1.05 to 1.30. 17. The centrifugal compressor according to claim 13 wherein the ratio of the length from the center of said impeller to the front edge of a vane belonging to the vane group at a position nearest said impeller toward the outer radius of said impeller is from 1.05 to 1.30. 18. A centrifugal compressor comprising: an impeller having a rotation axis; and a diffuser provided around said impeller, said diffuser having a first group of vanes including a plurality of vanes provided at a first angle relative to a radial direction of said impeller and a second group of vanes including a plurality of vanes provided at a second angle relative to the radial direction, said first group of vanes and said second group of vanes being concentric about the rotation axis with said first group of vanes being positioned at a greater distance from the rotation axis than said second group of vanes, said first angle being smaller than said second angle.