Patent US4543041A successfully refreshed from Google Patents.
US4543041A
Expired / Lapsed
US
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Impellor for centrifugal compressor
Assignee: Cummins Turbo Technologies Ltd
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Filing: 1985-01-10
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Granted: 1985-09-24
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Expires: 2005-01-10
Abstract
Abstract An impeller for a centrifugal impeller comprising a disc portion, a coaxial hub portion having a longitudinal through-bore by which the impeller is mounted on a rotatable shaft, and a plurality of blades in any one of several forms. The tip of each blade is curved in a direction opposite to the rotation of the impeller more than the rest of the blade. The radius of the tip curve decreases uniformly toward the radially outer end of the blade. This tip treatment produces improved isentropic efficiency.
Inventors
- 👤 Pierre B. French
- 👤 Paul J. Langdon
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-08 19:15
CPC Classifications
F; F04; F04D; F04D29/00; F04D29/26; F04D29/28; F04D29/284; F04D29/30; F05; F05D; F05D2240/00; F05D2240/20; F05D2240/30; F05D2240/304
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
161 words
An impeller for a centrifugal compressor, said impeller comprising: an annular disc portion having a front face and a rear face; an integral coaxial hub portion rotatable about a central axis; and a plurality of blades mounted on the front face of the disc portion and on the hub portion, each blade having a leading and trailing surface; each of said blades having an inlet portion for substantially axial entry of fluid and a tip portion for substantially radial movement of fluid as viewed in a plane containing the central axis of said impeller, the leading surface of the tip portion curving in a direction away from the direction of tip portion movement as viewed in a plane perpendicular to the central axis of said impeller, the radius of curvature of said leading surface uniformly decreasing to a minimum radius of curvature at the outer end of said blade that is less than any curvature radially inward from said tip portion.
Claim 2
Dependent Claim
161 words
An impeller for a centrifugal compressor, said impeller comprising: an annular disc portion having a front face and a rear face; an integral coaxial hub portion rotatable about a central axis; and a plurality of blades mounted on the front face of the disc portion and on the hub portion, each blade having a leading and trailing surface; each of said blades having an inlet portion for substantially axial entry of fluid and a tip portion for substantially radial movement of fluid as viewed in a plane containing the central axis of said impeller, the leading surface of the tip portion curving in a direction away from the direction of tip portion movement as viewed in a plane perpendicular to the central axis of said impeller, the radius of curvature of said leading surface uniformly decreasing to a minimum radius of curvature at the outer end of said blade that is less than any curvature radially inward from said tip portion.
Claim 3
Dependent Claim
31 words
An impeller as in claim 1 in which substantially the entire leading face of the blade radially inward from said tip portion curves opposite the direction of rotation of the impeller.
Claim 4
Dependent Claim
50 words
An impeller as in claim 1 in which the portion of the blades between said tip portion and the inlet portion extend radially and are straight except for the tip portion and both leading and trailing faces of said tip portion curve opposite the direction of rotation of the impeller.
Claim 5
Dependent Claim
24 words
An impeller as in claim 1 in which both leading and trailing surfaces of the blades radially inward from said tip portion are curved.
Claim 6
Dependent Claim
151 words
An impeller as in claim 1 further comprising a plurality of splitter blades mounted on the front face of the disc portion and on the hub portion and extending to the periphery of the disc portion, said splitter blades being placed between the blades so that the splitter blades and blades alternate, said splitter blades each having a tip portion for substantially radial movement of fluid as viewed in a plane containing the central axis of said compressor, said splitter blades having a leading surface which, in the tip portion, curves in a direction away from the direction of tip section movement as viewed in a plane perpendicular to the central axis of said hub portion, the radius of curvature of said leading surface uniformly decreasing to a minimum radius of curvature at the outer end of said blade that is less than any curvature radially inward from said tip section.
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USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1988-09-23 | 1989-03-25 | 1989-09-24 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1992-09-23 | 1993-03-25 | 1993-09-24 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1996-09-23 | 1997-03-25 | 1997-09-24 | $7700.00 | Window Closed / Lapsed |