US4311432A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Radial seal
Assignee: RTX Corp
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Filing: 1979-11-20
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Granted: 1982-01-19
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Expires: 1999-11-20
Abstract
Abstract A thin ring fabricated from a relatively low thermal expansion material located between the engine case and the outer air seal segments and adjacent vane segments serves to seal the gap between the adjacent vane segments and outer air seal segments by virtue of deforming the ring caused by the expansion of the case.
Inventors
- 👤 Robert J. Kildea
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-06 17:16
CPC Classifications
F; F01; F01D; F01D11/00; F01D11/08; F01D11/005
Claims Analysis
Total Claims: 3
Claim 1
Independent Claim
179 words
A turbine type power plant having a generally cylindrical outer casing surrounding at least one set of vanes and its adjacent rotor, a segmented generally cylindrically shaped outer air seal between the casing and the tips of the blades on said rotor, platform adjacent the outer edges of said set of vanes and being in substantially axial alignment with but spaced from said outer air seal defining a gap forming a leakage path of engine cooling air into the gas path, a tie connection extending radially inward from said casing securing said platform and said outer air seal and being disposed adjacent said gap, seal means for said gap disposed between the end of said tie connection and overlying a portion of said platform and said outer air seal and extending across said gap, said seal means being a continuous ring-like element and having a relative low thermal expansion in relation to said case whereby heating of said case deforms said seal means to position it into contact with said platform and outer air seal and seal said gap.
Claim 2
Dependent Claim
179 words
A turbine type power plant having a generally cylindrical outer casing surrounding at least one set of vanes and its adjacent rotor, a segmented generally cylindrically shaped outer air seal between the casing and the tips of the blades on said rotor, platform adjacent the outer edges of said set of vanes and being in substantially axial alignment with but spaced from said outer air seal defining a gap forming a leakage path of engine cooling air into the gas path, a tie connection extending radially inward from said casing securing said platform and said outer air seal and being disposed adjacent said gap, seal means for said gap disposed between the end of said tie connection and overlying a portion of said platform and said outer air seal and extending across said gap, said seal means being a continuous ring-like element and having a relative low thermal expansion in relation to said case whereby heating of said case deforms said seal means to position it into contact with said platform and outer air seal and seal said gap.
Claim 3
Dependent Claim
41 words
Apparatus as in claim 1 wherein the edge of said platform and the adjacent edge of said outer air seal adjacent said gap is beveled radially outward whereby said ring-like element tends to deform into said space formed by said bevels.
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) | 1985-01-18 | 1985-07-20 | 1986-01-19 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1989-01-18 | 1989-07-20 | 1990-01-19 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1993-01-18 | 1993-07-20 | 1994-01-19 | $7700.00 | Window Closed / Lapsed |