Compressor diffuser

Claim 2

A centrifugal compressor comprising, in combination, a rotor operable to discharge gas at high velocity from the periphery of the rotor with radial and tangential components of velocity and a stator enclosing the rotor, the stator including a diffuser disposed around the periphery of the rotor to receive and diffuse the gas discharged from the rotor; the diffuser defining an annular aray of diffusing passages extending radially outwardly and circumferentially from the rotor, at least the downstream portion of each passage being divergent in area in the direction of flow; the passages merging at the entrances to the passages and being discrete at the outlets from the passages; the diffuser including front and rear walls extending generally radially from the periphery of the rotor defining the front and rear boundaries of the diffusing passages and including an annular array of vanes each extending radially and circumferentially from a leading edge and from one said wall to the other, the vanes defining the radially outer and inner boundaries of the diffusing passages; each passage having a throat bounded by the walls, by the leading edge of the vane defining the inner boundary of the passage, and by the inner surface of the vane defining the outer boundary of the passage; in which the improvement comprises an annular flow splitter disposed centrally between the front and rear walls, extending circumferentially across each passage and extending radially through the passage throats, the inner and outer perimeters of the flow splitter being substantially at the inner and outer boundaries of the throats, respectively, the flow splitter dividing the entrance to each diffusing passage into a front passage bounded by the front wall and the splitter and a rear passage bounded by the rear wall and the splitter, so as to reduce flow separation in the diffuser.

Claim 3

A centrifugal compressor comprising, in combination, a rotor operable to discharge gas at high velocity from the periphery of the rotor with radial and tangential components of velocity and a stator enclosing the rotor, the stator including a diffuser disposed around the periphery of the rotor to receive and diffuse the gas discharged from the rotor; the diffuser defining an annular array of diffusing passages extending radially outwardly and circumferentially from the rotor, at least the downstream portion of each passage being divergent in area in the direction of flow; the passages merging at the entrances to the passages and being discrete at the outlets from the passages; the diffuser including front and rear walls extending generally radially from the periphery of the rotor defining the front and rear boundaries of the diffusing passages and including an annular array of vanes each extending radially and circumferentially from a leading edge and from one said wall to the other, the vanes defining the radially outer and inner boundaries of the diffusing passages; each passage having a throat bounded by the walls, by the leading edge of the vane defining the inner boundary of the passage, and by the inner surface of the vane defining the outer boundary of the passage; in which the improvement comprises an annular flow splitter having an uncambered airfoil cross-section with its central plane disposed centrally between the front and rear walls, extending circumferentially across each passage and extending radially through the passage throats, the inner and outer perimeters of the flow splitter being substantially at the inner and outer boundaries of the throats, respectively, the flow splitter dividing the entrance to each diffusing passage into a front passage bounded by the front wall and the splitter and a rear passage bounded by the rear wall and the splitter, so as to reduce flow separation in the diffuser.

Claim 4

A centrifugal compressor comprising, in combination, a rotor operable to discharge gas at high velocity from the periphery of the rotor with radial and tangential components of velocity and a stator enclosing the rotor, the stator including a diffuser disposed around the periphery of the rotor to receive and diffuse the gas discharged from the rotor; the diffuser defining an annular array of diffusing passages extending radially outwardly and circumferentially from the rotor, at least the downstream portion of each passage being divergent in area in the direction of flow; the passages merging at the entrances to the passages and being discrete at the outlets from the passages; the diffuser including front and rear walls extending generally radially from the periphery of the rotor defining the front and rear boundaries of the diffusing passages and including an annular array of vanes each extending radially and circumferentially from a leading edge and from one said wall to the other, the vanes defining the radially outer and inner boundaries of the diffusing passages; each passage having a throat bounded by the walls, by the leading edge of the vane defining the inner boundary of the passage, and by the inner surface of the vane defining the outer boundary of the passage; in which the improvement comprises an annular flow splitter having an uncambered airfoil cross-section with its central plane disposed centrally between the front and rear walls, extending circumferentially across each passage and extending radially through the passage throats, the inner and outer perimeters of the flow splitter being substantially at the inner and outer boundaries of the throats, respectively, the flow splitter dividing the entrance to each diffusing passage into a front passage bounded by the front wall and the splitter and a rear passage bounded by the rear wall and the splitter, so as to reduce flow separation in the diffuser.