US4773821A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Control mechanism for variably settable vanes of a flow straightener in a turbine plant
Assignee: Safran Aircraft Engines SAS
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Filing: 1987-12-15
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Granted: 1988-09-27
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Expires: 2007-12-15
Abstract
Abstract The connection between the actuating link of each variably settable vane of a compressor flow straightener in a turbine plant and the control ring for the vanes comprises a cylindrical roller rotatably mounted in a bore in the ring parallel to the axis of the compressor, the roller having a radial bore registering with a radial opening in the ring and housing the shaft of the link as a rotary and sliding fit. This arrangement prevents any torsional strain on the link during operation, and is found to be substantially simpler and more reliable than the known arrangements.
Inventors
- 👤 Francis L. Gonthier
- 👤 Bernard Mariner
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-04 02:18
CPC Classifications
F; F01; F01D; F01D17/00; F01D17/10; F01D17/12; F01D17/14; F01D17/16; F01D17/162; F04; F04D; F04D29/00; F04D29/40; F04D29/52; F04D29/54; F04D29/56; F04D29/563; Y; Y02; Y02T; Y02T50/00; Y02T50/60
Claims Analysis
Total Claims: 6
Claim 1
Independent Claim
197 words
Control mechanism for variably settable vanes of a compressor flow straightener of a turbine plant comprising a circular ring mounted for rotation about the longitudinal axis of said compressor, a plurality of links, each said link having first and second ends, and a radially oriented shaft at said second end thereof, first connection means rigidly connecting said first end of each said link to a corresponding one of said vanes, and second connection means pivotally connecting said shaft at said second end of each said link to said ring whereby rotation of said ring about said longitudinal axis of said compressor pivots said links to vary the angle of said vanes, said second connection means of each said link comprising means defining an axially extending bore in said ring having an axis parallel to said longitudinal axis, a cylindrical roller rotatably mounted in said axially extending bore, a port opening radially into said axially extending bore from the periphery of said ring, and means defining a radial bore in said roller, said radial bore being exposed by said port and receiving said shaft of said link whereby said shaft is rotatable and slidable in said radial bore.
Claim 2
Dependent Claim
197 words
Control mechanism for variably settable vanes of a compressor flow straightener of a turbine plant comprising a circular ring mounted for rotation about the longitudinal axis of said compressor, a plurality of links, each said link having first and second ends, and a radially oriented shaft at said second end thereof, first connection means rigidly connecting said first end of each said link to a corresponding one of said vanes, and second connection means pivotally connecting said shaft at said second end of each said link to said ring whereby rotation of said ring about said longitudinal axis of said compressor pivots said links to vary the angle of said vanes, said second connection means of each said link comprising means defining an axially extending bore in said ring having an axis parallel to said longitudinal axis, a cylindrical roller rotatably mounted in said axially extending bore, a port opening radially into said axially extending bore from the periphery of said ring, and means defining a radial bore in said roller, said radial bore being exposed by said port and receiving said shaft of said link whereby said shaft is rotatable and slidable in said radial bore.
Claim 3
Dependent Claim
135 words
Control mechanism according to claim 1, wherein said control ring is formed by a pair of annular members and means detachably securing said annular members to each other, each of said annular members having means defining a plurality of circumferentially spaced axially extending bores coaxially aligned with said bores of the other member, and said annular members defining a radially open gap between said aligned bores, and wherein said cylindrical roller of said second connection means of each said link comprises a pair of smaller diameter end portions separated by a larger diameter central portion, said end portions forming journals which are rotatably received in a pair of said aligned bores of said annular members, and said central portion being located in said radially open gap therebetween and containing said radial bore of said roller.
Claim 4
Dependent Claim
32 words
Control mechanism according to claim 2, wherein one of said annular members of said control ring has a portion with an L-shaped section partly covering said second end of each said link.
Claim 5
Dependent Claim
44 words
Control mechanism according to claim 1, wherein at least one resilient washer is disposed around said shaft at said second end of each said link, said washer acting between said link and said cylindrical roller to center said ring with respect to said links.
Claim 6
Dependent Claim
17 words
Control mechanism according to claim 1, wherein said cylindrical roller is made of a moulded composite material.
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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) | 1991-09-27 | 1992-03-28 | 1992-09-27 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1995-09-27 | 1996-03-28 | 1996-09-27 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1999-09-27 | 2000-03-28 | 2000-09-27 | $7700.00 | Window Closed / Lapsed |