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US4194869A
Expired / Lapsed
US
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Stator vane cluster
Assignee: RTX Corp
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Filing: 1978-06-29
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Granted: 1980-03-25
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Expires: 1998-06-29
Abstract
Abstract A structure for clustered stator vanes of the type utilized in axial flow gas turbine engines is disclosed. Concepts and techniques for retaining the vanes in position within the engine are developed. The concepts are well suited to structures in which the vanes are metallurgically joined. In one embodiment the stator vanes are grouped in pairs of a first, or principal vane and a second, or secondary vane each. East secondary vane is joined to a complementary principal vane along planes which preclude radial or axial movement of the secondary vane with respect to the principal vane, in the event that the bond between the joined vanes fails.
Inventors
- 👤 Nicholas Corcokios
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 17:16
CPC Classifications
F; F01; F01D; F01D9/00; F01D9/02; F01D9/04; F01D9/041; F01D9/042
Claims Analysis
Total Claims: 5
Claim 1
Independent Claim
101 words
In a vane cluster formed of a first vane having an inner platform and an outer platform, and a second vane having an inner platform and an outer platform, the improvement comprising: first and second vanes joined at the inner platforms along a plane A and at the outer platforms along a plane B wherein the planes A and B intersect along a line of intersection which passes between the inner and outer platforms and are oriented so as to form inwardly facing, joining surfaces on one of said vanes and outwardly facing, joining surfaces on the other of said vanes.
Claim 2
Dependent Claim
101 words
In a vane cluster formed of a first vane having an inner platform and an outer platform, and a second vane having an inner platform and an outer platform, the improvement comprising: first and second vanes joined at the inner platforms along a plane A and at the outer platforms along a plane B wherein the planes A and B intersect along a line of intersection which passes between the inner and outer platforms and are oriented so as to form inwardly facing, joining surfaces on one of said vanes and outwardly facing, joining surfaces on the other of said vanes.
Claim 3
Dependent Claim
59 words
The invention according to claim 1 wherein the planes A and B are further oriented such that each of the platforms of the vanes have a trapezoidal geometry including a longer parallel side and a shorter parallel side and wherein the longer parallel side of one of said platforms aligns with the shorter parallel side of the adjacent platform.
Claim 4
Dependent Claim
150 words
A stator vane cluster of an axial flow gas turbine engine, wherein the cluster has an upstream end and a downstream end and comprises: a first vane having an inner platform and an outer platform, each platform having a trapezoidal shape including a longer parallel side and a shorter parallel side; and a second vane having an inner platform and an outer platform, each platform having a trapezoidal shape including a longer parallel side and a shorter parallel side wherein the longer parallel side of the inner platform of the first vane aligns with the shorter parallel side of the inner platform of the second vane at the upstream end of the vane cluster and wherein the shorter parallel side of the outer platform of the first vane aligns with the longer parallel side of the outer platform of the second vane at the upstream end of the vane cluster.
Claim 5
Dependent Claim
150 words
A stator vane cluster of an axial flow gas turbine engine, wherein the cluster has an upstream end and a downstream end and comprises: a first vane having an inner platform and an outer platform, each platform having a trapezoidal shape including a longer parallel side and a shorter parallel side; and a second vane having an inner platform and an outer platform, each platform having a trapezoidal shape including a longer parallel side and a shorter parallel side wherein the longer parallel side of the inner platform of the first vane aligns with the shorter parallel side of the inner platform of the second vane at the upstream end of the vane cluster and wherein the shorter parallel side of the outer platform of the first vane aligns with the longer parallel side of the outer platform of the second vane at the upstream end of the vane cluster.
References Cited (Backward Citations)
GB128190A
Cited
US3363416A
Cited
US3302926A
Cited
US3824034A
Cited
US3751182A
Cited
US3923420A
Cited
US4015910A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1983-03-25 | 1983-09-24 | 1984-03-25 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1987-03-25 | 1987-09-24 | 1988-03-25 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1991-03-25 | 1991-09-24 | 1992-03-25 | $7700.00 | Window Closed / Lapsed |