Patent US3990810A successfully refreshed from Google Patents.
US3990810A
Expired / Lapsed
US
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Vane assembly for close coupling the compressor turbine and a single stage power turbine of a two-shaped gas turbine
Assignee: Westinghouse Electric Corp
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Filing: 1975-12-23
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Granted: 1976-11-09
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Expires: 1995-12-23
Abstract
Abstract A vane assembly is shown for a relatively short annular transition zone directing the discharge of the working fluid from the compressor turbine to a single stage power turbine in a gas turbine engine. The annular transition zone comprises a plurality of individual arcuate segments having a pair of stationary vanes integrally molded to inner and outer shroud members. A variable vane is disposed immediately downstream of each stationary vane for guiding the working fluid into the power turbine at an optimum angle. The variable vanes are manually adjustable from outside the turbine casing through a linkage and support mechanism that maintains a constant clearance between the variable vane and the shroud members and also accommodates variations in dimensional relationships due to temperature variations. Also, provision is made for centering the axis of the variable vanes to a precise position with respect to the stationary vane to accommodate the buildup of assembly tolerances.
Inventors
- 👤 David J. Amos
- 👤 Taku Ichiryu
- 👤 Tomohiko Sato
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-05 16:30
CPC Classifications
F; F01; F01D; F01D17/00; F01D17/10; F01D17/12; F01D17/14; F01D17/16; F01D17/162
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
243 words
In a gas turbine engine having a closely coupled fluid flow path between the compressor turbine and the power turbine, said path defined by an annular duct comprising: opposed radially inner and radially outer arcuate shroud members extending axially between the discharge area of said compressor turbine and the inlet area of said power turbine; at least one stationary vane extending radially across and interconnecting said shroud members generally adjacent said compressor turbine discharge area, a pivotable vane extending radially between said shroud members generally adjacent the power turbine inlet area and providing opposed projections extending generally radially from the opposed ends of said vane for receipt in inner and outer bearing structure supported in said respective shroud members, means for adjusting the angular orientation of such pivotable vane exteriorly of the casing of said engine and; means for maintaining a unidirectional biasing force on said vane to positively seat the vane in a predetermined relationship with respect to said outer shroud member to maintain a pre-set minimal clearance gap between said variable vane and said outer shroud member and, means forming the part of said inner shroud member supporting said inner bearing structure and mounted to the adjacent portion of said inner shroud member for radial movement with respect thereto in accordance with the expansion and contraction of said pivotable vane to maintain a pre-set minimal clearance gap between said variable vane and said bearing supporting part of said inner shroud member.
Claim 2
Dependent Claim
243 words
In a gas turbine engine having a closely coupled fluid flow path between the compressor turbine and the power turbine, said path defined by an annular duct comprising: opposed radially inner and radially outer arcuate shroud members extending axially between the discharge area of said compressor turbine and the inlet area of said power turbine; at least one stationary vane extending radially across and interconnecting said shroud members generally adjacent said compressor turbine discharge area, a pivotable vane extending radially between said shroud members generally adjacent the power turbine inlet area and providing opposed projections extending generally radially from the opposed ends of said vane for receipt in inner and outer bearing structure supported in said respective shroud members, means for adjusting the angular orientation of such pivotable vane exteriorly of the casing of said engine and; means for maintaining a unidirectional biasing force on said vane to positively seat the vane in a predetermined relationship with respect to said outer shroud member to maintain a pre-set minimal clearance gap between said variable vane and said outer shroud member and, means forming the part of said inner shroud member supporting said inner bearing structure and mounted to the adjacent portion of said inner shroud member for radial movement with respect thereto in accordance with the expansion and contraction of said pivotable vane to maintain a pre-set minimal clearance gap between said variable vane and said bearing supporting part of said inner shroud member.
Claim 3
Dependent Claim
89 words
Structure according to claim 1 wherein the downstream end of said stationary vane and the upstream end of said rotatable vane define complementary nested surfaces and means providing a generally sealing engagement therebetween along their common radial extent and, means for adjusting the position of said bearing supporting part of said inner shroud member with respect to said bearing structure in said outer shroud member to, upon assembly, adjust the axis of said rotatable vane to maintain said sealing engagement with said stationary vane to accommodate assembly tolerance build-up.
Claim 4
Dependent Claim
67 words
Structure according to claim 2 wherein said pivotable vane adjusting means includes at least a two-piece member extending from engagement with the upper radial projection of said variable vane to exteriorly of said casing, with the juncture between the exteriorly extending portion and the vane engaging portion providing a knuckle for accommodating relative displacement of the casing with respect to the vane caused by expansion or contraction.
Claim 5
Dependent Claim
112 words
Structure according to claim 2 wherein said means for maintaining a unidirectional biasing force comprises: rod means engaging said upper radial projection of said variable vane and extending exteriorly of said casing, spring means biasing said rod means in a radially outwardly direction, means engaging and seating a bearing surface surrounding said projection, said means disposed within said outer shroud member and, retaining means for securing said engaging and seating means in a predetermined position, whereby, the upward force on said vane by said spring maintains said bearing surface in said engaging means in the most radially outward permitted position to minimize the clearance between said vane and said outer shroud member.
Claim 6
Dependent Claim
224 words
A vane and shroud assembly for an annular transition portion between the compressor turbine and power turbine of a gas turbine engine comprising a plurality of individual arcuate segments defined by radially opposed inner and outer shroud members integrally molded with at least one stationary vane extending therebetween, a pivotable vane disposed therebetween downstream of said stationary vane and generally forming a continuous surface therewith to provide an airfoil shaped contour, said pivotable vane having a projection extending generally radial from each end thereof, bearing seating means housed within the outer shroud for engaging the radially outer projection, a platform member movably attached to and forming a part of the inner shroud and housing a bearing means for engaging the radially inner projection, biasing means connected to said outer projection to maintain an outward force on said pivotable vane to maintain a constant seating relationship of said projection in said outer bearing seating means and a constant clearance of said variable vane relative to said outer shroud, means interconnecting said inner projection and said inner bearing means for causing radial movement of said platform in correspondence to expansion or contraction of said pivotable vane and, means connected to said inner shroud for aligning said inner bearing seat with respect to said outer bearing seat for establishing generally precisely the axis of said pivotable vane.
Claim 7
Dependent Claim
224 words
A vane and shroud assembly for an annular transition portion between the compressor turbine and power turbine of a gas turbine engine comprising a plurality of individual arcuate segments defined by radially opposed inner and outer shroud members integrally molded with at least one stationary vane extending therebetween, a pivotable vane disposed therebetween downstream of said stationary vane and generally forming a continuous surface therewith to provide an airfoil shaped contour, said pivotable vane having a projection extending generally radial from each end thereof, bearing seating means housed within the outer shroud for engaging the radially outer projection, a platform member movably attached to and forming a part of the inner shroud and housing a bearing means for engaging the radially inner projection, biasing means connected to said outer projection to maintain an outward force on said pivotable vane to maintain a constant seating relationship of said projection in said outer bearing seating means and a constant clearance of said variable vane relative to said outer shroud, means interconnecting said inner projection and said inner bearing means for causing radial movement of said platform in correspondence to expansion or contraction of said pivotable vane and, means connected to said inner shroud for aligning said inner bearing seat with respect to said outer bearing seat for establishing generally precisely the axis of said pivotable vane.
Claim 8
Dependent Claim
36 words
Structure according to claim 5 wherein the downstream end of said stationary vane and the upstream end of said rotatable vane define complementary nested surfaces providing a generally sealing engagement therebetween along their common radial extent.
Claim 9
Dependent Claim
72 words
Structure according to claim 6 including adjusting means for manually setting the angular orientation of said vane exteriorly of the casing of said engine comprising a two piece member extending from engagement with the upper radial projection to a position exteriorly of said casing, with the juncture between the two separate portions providing a knuckle to accommodate relative displacement of the casing with respect to the vane caused by expansion or contraction.
Claim 10
Dependent Claim
113 words
Structure according to claim 6 wherein said means for maintaining a unidirectional biasing force comprises: rod means engaging said upper radial projection of said variable vane and extending exteriorly of said casing, spring means biasing said rod means in a radially outwardly direction, means engaging and seating a bearing surface surrounding said projection, said means disposed within said outer shroud member and, retaining means for securing said engaging and seating means in a predetermined position, whereby the radially outward force on said vane by said spring maintains said bearing surface in said engaging means in the most radially outward permitted position to minimize the clearance between said vane and said outer shroud member.
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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) | 1979-11-09 | 1980-05-10 | 1980-11-09 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1983-11-09 | 1984-05-10 | 1984-11-09 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1987-11-09 | 1988-05-10 | 1988-11-09 | $7700.00 | Window Closed / Lapsed |