US4768924A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Ceramic stator vane assembly
Assignee: Pratt and Whitney Canada Corp
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Filing: 1986-07-22
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Granted: 1988-09-06
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Expires: 2006-07-22
Abstract
Abstract A ceramic stator vane assembly for a gas turbine engine comprises a plurality of ceramic stator vane segments arranged in an annular array with each vane segment having integral concentric tip and root platform members. The tip and root platform members define continuous inner and outer surfaces for receiving inner and outer ceramic rings. Radial and axial housing members are provided for mounting the stator vane assembly within the engine, and thermal insulation means are provided between the ceramic vane assembly and the housing members.
Inventors
- 👤 Gilles Carrier
- 👤 Michael D. Stoten
- 👤 Patrick Szwedska
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-06 01:43
CPC Classifications
F; F01; F01D; F01D5/00; F01D5/12; F01D5/28; F01D5/284; F01D9/00; F01D9/02; F01D9/04; F01D9/042; F05; F05D; F05D2240/00; F05D2240/10; F05D2300/00; F05D2300/20; F05D2300/21; F05D2300/22; F05D2300/226; F05D2300/2261
Claims Analysis
Total Claims: 8
Claim 1
Independent Claim
158 words
A ceramic vane assembly for a gas turbine engine, the vane assembly comprising a plurality of ceramic stator vane segments arranged in an annular array simulating a monolithic stator vane ring with each vane segment having integral concentric tip and root platform members, said tip and root platform members defining continuous inner and outer shroud surfaces, and outer ceramic ring surrounding the vane assembly on the outer shroud surface in a cold interference fit and subject to tensile stresses during all thermal conditions, an inner ceramic ring provided in a cold interference fit within the inner shroud surface and subject to compression stress during all thermal conditions, the vane assembly being compressively prestressed by the inner and outer ceramic rings, radial and axial housing means provided for mounting said prestressed stator vane assembly within said engine, and thermal insulation means provided between the mounting means and said prestressed ceramic vane assembly and the inner and outer ceramic rings.
Claim 2
Dependent Claim
158 words
A ceramic vane assembly for a gas turbine engine, the vane assembly comprising a plurality of ceramic stator vane segments arranged in an annular array simulating a monolithic stator vane ring with each vane segment having integral concentric tip and root platform members, said tip and root platform members defining continuous inner and outer shroud surfaces, and outer ceramic ring surrounding the vane assembly on the outer shroud surface in a cold interference fit and subject to tensile stresses during all thermal conditions, an inner ceramic ring provided in a cold interference fit within the inner shroud surface and subject to compression stress during all thermal conditions, the vane assembly being compressively prestressed by the inner and outer ceramic rings, radial and axial housing means provided for mounting said prestressed stator vane assembly within said engine, and thermal insulation means provided between the mounting means and said prestressed ceramic vane assembly and the inner and outer ceramic rings.
Claim 3
Dependent Claim
16 words
A ceramic vane assembly as defined in claim 1, wherein the ceramic material is silicon carbide.
Claim 4
Dependent Claim
25 words
A vane assembly as defined in claim 2, wherein the stator vane segments are silicon carbide while the outer and inner rings are silicon carbide.
Claim 5
Dependent Claim
16 words
A ceramic vane assembly as defined in claim 1, wherein the ceramic material is silicon nitride.
Claim 6
Dependent Claim
25 words
A vane assembly as defined in claim 4, wherein the stator vane segments are silicon nitride while the outer and inner rings are silicon nitride.
Claim 7
Dependent Claim
38 words
A ceramic vane assembly as defined in claim 1, wherein the outer ring which is under tensile stress during thermal expansion is substantially larger in cross-section than the inner ring which is under compression stress during thermal expansion.
Claim 8
Dependent Claim
26 words
A stator vane assembly as defined in claim 1, wherein the insulation material is in the form of ceramic fibers held within a thin metallic envelope.
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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) | 1991-09-06 | 1992-03-07 | 1992-09-06 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1995-09-06 | 1996-03-07 | 1996-09-06 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1999-09-06 | 2000-03-07 | 2000-09-06 | $7700.00 | Window Closed / Lapsed |