Centrifugal compressor

• US 5,310,309 A
• Filed: 10/15/1992
• Issued: 05/10/1994
• Est. Priority Date: 10/21/1991
• Status: Expired due to Fees

• Current Assignee: Hitachi, Ltd.
• Original Assignee: Hitachi, Ltd.
• Inventors: Nakagawa, Koji, Terasaki, Masatoshi
• Primary Examiner(s): KWON, JOHN
• Application Number:
  US07/961,389
• Time in Patent Office: 572 Days
• Field of Search: 415/208.1, 415/208.2, 415/208.3, 415/211.2, 415/211.1, 415/914
• US Class Current: 415/208.3
• CPC Class Codes: F04D 29/444 Bladed diffusers
• CPC Class Codes: F05D 2250/52 Outlet

Abstract

A centrifugal compressor has a diffuser with stator blades arranged therein for converting the kinetic energy of a fluid discharged from an impeller into a pressure energy. The stator blades have leading edges inclined in the downstream direction while extending away from a side plate toward a core plate. Auxiliary blades having a chord length shorter than that of each of the stator blades have leading edges inclined in the downstream direction while extending away from the side plate toward the core plate and are arranged at positions radially inward of the stator plates in such a manner that one of the surfaces of each of the auxiliary blades faces a stator blade. The compressor is capable of operating without suffering from surging and rotating stall even in a low flow rate region.

Claims

1. A centrifugal compressor comprising a diffuser provided with stator blades operative to convert the kinetic energy of a fluid discharged from an impeller into a pressure energy, wherein said stator blades have leading edges inclined in the downstream direction while extending away from a side plate toward a core plate;

and auxiliary blades each having a chord length shorter than that of each of said stator blades have leading edges inclined in the downstream direction while extending away from said side plate toward said core plate, said auxiliary blades being arranged at positions radially inward of said stator blades in such a manner that one of the surfaces of each said auxiliary blade faces a stator blade.

2. A centrifugal compressor according to claim 1, wherein the stator blades and said auxiliary blades are arranged in such a manner that the blades are sparse in a vicinity of a tongue portion of a scroll-shaped flow passage and dense in a part of said passage remote from said tongue portion.

3. A centrifugal compressor comprising a diffuser provided with stator blades operative to convert the kinetic energy of a fluid discharged from an impeller into a pressure energy, wherein said stator blades are uniformly arranged in said diffuser and have leading edges inclined in the downstream direction while extending away from a side plate toward a core plate;

and auxiliary blades each having a chord length shorter than that of a chord length of each of said stator blades having leading edges inclined in the downstream direction while extending away from said side plate toward said core plate, said auxiliary blades being arranged at positions radially inwardly of said stator blades in such a manner that one of the surfaces of each of said auxiliary blades faces a stator blade.

4. A centrifugal compressor according to claim 3, wherein said stator blades and said auxiliary blades are arranged in such a manner that such blades are sparse in a vicinity of a tongue portion of a scroll-shaped flow passage and dense in a part of said passage remote from said tongue portion.

5. A centrifugal compressor comprising a diffuser provided with stator blades operative to convert he kinetic energy of a fluid discharged from an impeller into a pressure energy, wherein the stator blades are uniformly arranged in said diffuser, said stator blades including a first group of stator blades having leading edges inclined in a downstream direction while extending away from a side plate toward a core plate and a second group of stator blades having leading edges not inclined with respect to the downstream direction of the flow of said fluid, the stator blades of said first and second groups being arranged in a mixed number;

and auxiliary blades each having a chord length shorter than that of a chord length of each of said stator blades have leading edges inclined in the downstream direction while extending away from said side plate toward said core plate are disposed radially inwardly of said stator blades in such a manner that one of the surfaces of each of said auxiliary blades faces a stator blade.

6. A centrifugal compressor according to claim 5, wherein said stator blades and said auxiliary blades are arranged in such a manner that such blades are sparse in a vicinity of a tongue portion of a scroll-shaped flow passage and dense in a part of said passage remote from said tongue portion.

7. A centrifugal compressor comprising a diffuser provided with stator blades operative to convert kinetic energy of a fluid discharged from an impeller into a pressure energy, wherein the stator blades are uniformly arranged in said diffuser, said stator blades having leading edges inclined in a downstream direction while extending away from a side plate toward a core plate;

and auxiliary blades each having a chord length shorter than a chord length of each of said stator blades includes a first group of auxiliary blades having leading edges inclined in the downstream direction while extending away from said side plate toward said core plate and a second group of auxiliary blades having leading edges not inclined with respect to the downstream direction of the flow of said fluid, said first and second auxiliary blades being arranged in a mixed manner at positions radially inwardly of said stator blades in such a manner that one of the surfaces of each of said auxiliary blades faces a stator blade.

8. A centrifugal compressor comprising a diffuser provided with stator blades operative to convert kinetic energy of a fluid discharged from an impeller into a pressure energy, wherein the stator blades are uniformly arranged in said diffuser, said stator blades include a first group of stator blades having leading edges inclined in a downstream direction while extending away from a side plate toward a core plate and a second group of stator blades having leading edges not inclined with respect to the direction of the flow of said fluid, the stator blades of said first and second groups being arranged in a mixed manner;

and auxiliary blades each having a chord length shorter than a chord length of each of said stator blades include a first group of auxiliary blades having leading edges inclined in the downstream direction while extending away from said side plate toward said core plate and a second group of auxiliary blades having leading edges not inclined with respect tot he direction of flow of said fluid, the auxiliary blades of said first and second groups being arranged in a mixed manner at positions radially inwardly of said stator blades in such a manner that one of the surfaces of each of said auxiliary blades faces a stator blade.

9. A centrifugal compressor comprising a diffuser provided with stator blades operative to convert kinetic energy of a fluid discharged from an impeller into a pressure energy, wherein the stator blades are non-uniformly arranged in said diffuser, and have leading edges inclined in a downstream direction while extending away from a side plate toward a core plate;

and auxiliary blades each having a chord length shorter than a chord length of each of said stator blades and having leading edges inclined in the downstream direction while extending away from said side plate toward said core plate arranged at positions radially inwardly of said stator blades in such a manner that one of the surfaces of each of said auxiliary blades faces a stator blade.

10. A centrifugal compressor according to claim 9, wherein said stator blades and said auxiliary blades are arranged in such manner that said blades are sparse in the vicinity of a tongue portion of a scroll-shaped flow passage and dense in the part of said passage remote from said tongue portion.

11. A centrifugal compressor according to claim 10, wherein said vicinity of said tongue portion is an area including said tongue portion and corresponding to not more than one half of the entire circumference.

12. A centrifugal compressor comprising a diffuser provided with stator blades operative to convert kinetic energy of a fluid discharged from an impeller into a pressure energy, wherein the stator blades are non-uniformly arranged in said diffuser, and include a first group of stator blades having leading edges inclined in a downstream direction while extending away from a side plate toward a core plate and a second group of stator blades having leading edges normal to a direction of a flow of said fluid, the stator blades of said first and second groups being arranged in a mixed manner;

and auxiliary blades each having a chord length shorter than a chord length of each of said stator blades and a leading edges inclined in the downstream direction while extending away from said side plate toward said core plate are arranged at positions radially inwardly of said stator blades in such a manner that one of the surfaces of each of said auxiliary blades faces a stator blade.

13. A centrifugal compressor comprising a diffuser provided with stator blades operative to convert kinetic energy of a fluid discharged from an impeller into a pressure energy, wherein the stator blades are non-uniformly arranged in said diffuser, said stator blades including a first group of stator blades having leading edges inclined in a downstream direction while extending away from a side plate toward a core plate and a second group of stator blades having leading edges normal to a direction of flow of said fluid, the stator blades of said first and second groups being arranged in a mixed manner;

and auxiliary blades each having a chord length shorter than a chord length of each of said stator blades include a first group of auxiliary blades having leading edges inclined in the downstream direction while extending away from said side plate toward said core plate and a second group of auxiliary blades having leading edges normal to the direction of flow of said fluid, the auxiliary blades of said first and second groups being arranged at positions radially inwardly of said stator blades in such a manner that one of the surfaces of each of said auxiliary blades faces said stator blade.

14. A centrifugal compressor comprising a diffuser provided with stator blades operative to convert kinetic energy of a fluid discharged from an impeller into a pressure energy, wherein the stator blades are non-uniformly arranged in said diffuser, and include first group of stator blades having leading edges inclined in a downstream direction while extending away from a side plate toward a core plate and a second group of stator blades having leading edges not inclined with respect to the direction of flow of said fluid, said first and second groups of stator blades being arranged in a mixed manner;

and auxiliary blades each having a chord length shorter than a chord length of each of said stator blades include a first group of auxiliary blades having leading edges inclined in the downstream direction while extending away from said side plate toward said core plate and a second group of auxiliary blades having leading edges not inclined to the direction of flow of said fluid, the auxiliary blades of said first and second groups being arranged in a mixed manner at positions radially inwardly of said stator blades in such a manner that one of the surfaces of each of said auxiliary blades faces a stator blade.