US4184720A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Air-supported bearing for turbine engines
Assignee: Rolls Royce Solutions GmbH
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Filing: 1977-10-26
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Granted: 1980-01-22
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Expires: 1997-10-26
Abstract
Abstract A bearing for the ceramic rotor of a turbine engine or turbomachine, which consists of an air-supported bearing providing for a lubricating air film between the inner and outer bearing rings at least at the higher operating speeds of the engine. This facilitates operation of the turbine engine or machine under high temperature and rotational speed operating conditions.
Inventors
- 👤 Anton Zacherl
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-02 13:55
CPC Classifications
F; F16; F16C; F16C32/00; F16C32/06; F16C32/0603; F16C32/0614; F16C32/0622; F01; F01D; F01D25/00; F01D25/18; F01D25/22; F16C17/00; F16C17/12; F16C17/18; F16C23/00; F16C23/02; F16C23/04; F16C23/043; F16C23/045; F16C32/0662; F16C32/067; F16C33/00; F16C33/02; F16C33/04; F16C33/06; F16C33/10; F16C33/1005; F16C39/00; F16C39/04; F16C2231/00; F16C2300/00; F16C2300/40; F16C2300/54; F16C2360/00
Claims Analysis
Total Claims: 3
Claim 1
Independent Claim
232 words
In a thermal turbine engine having a ceramic rotor, having a cylindrical shaft, adapted to rotate at high rotational speeds, a bearing comprising an air-supported bearing, said air-supported bearing including an outer bearing ring and an inner bearing ring, and a lubricating air film being maintained intermediate said bearing rings, the improvement comprising: said inner bearing ring including a convex spherical outer surface and said outer bearing ring including a concave inner spherical surface substantially complementary to and positioned adjacent said convex outer spherical surface with a spherical fluid gap existing between the convex and concave surfaces, said inner bearing ring also including a cylindrical inner surface substantially complementary to and positioned adjacent to the outer cylindrical surface of said cylindrical shaft with a cylindrical gap existing therebetween, and the materials of said inner bearing ring and the shaft of said ceramic rotor being selected so that the cylindrical gap between said shaft and said inner bearing ring remains substantially constant over the entire temperature range and rotational speed range of said turbine engine, and the diameters of said shaft and said inner bearing ring being dimensioned relative to each other so that a friction contact exists between said inner bearing ring and said shaft at lower rotational speeds of said engine whereas a dynamic lubricating air film is produced intermediate said shaft and said inner bearing ring at higher rotational speeds.
Claim 2
Dependent Claim
232 words
In a thermal turbine engine having a ceramic rotor, having a cylindrical shaft, adapted to rotate at high rotational speeds, a bearing comprising an air-supported bearing, said air-supported bearing including an outer bearing ring and an inner bearing ring, and a lubricating air film being maintained intermediate said bearing rings, the improvement comprising: said inner bearing ring including a convex spherical outer surface and said outer bearing ring including a concave inner spherical surface substantially complementary to and positioned adjacent said convex outer spherical surface with a spherical fluid gap existing between the convex and concave surfaces, said inner bearing ring also including a cylindrical inner surface substantially complementary to and positioned adjacent to the outer cylindrical surface of said cylindrical shaft with a cylindrical gap existing therebetween, and the materials of said inner bearing ring and the shaft of said ceramic rotor being selected so that the cylindrical gap between said shaft and said inner bearing ring remains substantially constant over the entire temperature range and rotational speed range of said turbine engine, and the diameters of said shaft and said inner bearing ring being dimensioned relative to each other so that a friction contact exists between said inner bearing ring and said shaft at lower rotational speeds of said engine whereas a dynamic lubricating air film is produced intermediate said shaft and said inner bearing ring at higher rotational speeds.
Claim 3
Dependent Claim
118 words
The bearing as claimed in claim 1, said bearing operating under a radial load of about 20 kp and a rated rotational speed of 50,000 rpm at a temperature of about 500° C., said bearing further comprising the parameters of: ______________________________________
Normal diameter of the shaft
50 mm
Width of the inner bearing ring
50 mm
Average roughness of shaft and
inner bearing ring R.sub.a =0.2-0.3
Coefficients of thermal expan- sion of the shaft
##STR4##
Coefficients of thermal expan- sion of the inner bearing
##STR5##
Coefficients of thermal expan- sion of the outer bearing
##STR6##
Difference in diameter between
shaft and inner bearing ring and
between inner bearing ring and
outer bearing ring Δd = 0.04-0.06 mm
______________________________________
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1983-01-21 | 1983-07-23 | 1984-01-22 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1987-01-21 | 1987-07-23 | 1988-01-22 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1991-01-21 | 1991-07-23 | 1992-01-22 | $7700.00 | Window Closed / Lapsed |