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US4861228A Expired / Lapsed US ⏱️ 0.0 years remaining

Variable stator vane assembly

Assignee: Rolls Royce PLC
•
Filing: 1988-08-16
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Granted: 1989-08-29
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Expires: 2008-08-16
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Abstract

Abstract A variable stator vane assembly suitable for a power turbine in which each stator vane is provided at its radially inner and outer extents with disc-shaped platforms which locate on bushes provided on associated support structure. The bushes are cooled by a flow of cooling air which is of higher pressure than that of the hot gases operationally flowing over the vanes so as to prevent the leakage of such hot gases past the bushes.

Inventors

  • 👤 Michael T. Todman

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-05 16:58
CPC Classifications
F; F01; F01D; F01D17/00; F01D17/10; F01D17/12; F01D17/14; F01D17/16; F01D17/162

Claims Analysis

Total Claims: 9
Claim 1
Independent Claim 181 words
A variable stator aerofoil vane assembly comprising an annular array of generally radially extending aerofoil cross-section stator vanes, and support structure supporting the radially inner and outer extents of said vanes so that said vanes are pivotable about their longitudinal axes, each of said vanes being provided at each of its longitudinal extents with platform means to cooperate with said support structure to limit any radial movement of said vane, and bush means interposed between each of platform means and said support structure, means being provided to supply a cooling fluid to said bush means at pressure higher than that of any fluid operationally flowing over said vanes so that said cooling fluid flows between each of said bush means and at least one platform means and said support structure so the said cooling fluid is placed in heat exchange relationship with said bush means and is subsequently exhausted into said fluid operationally flowing over said vanes, each of said bush means adjacent a radially inner or outer platform being grooved to at least partially define passages for said cooling fluid.
Claim 2
Dependent Claim 181 words
A variable stator aerofoil vane assembly comprising an annular array of generally radially extending aerofoil cross-section stator vanes, and support structure supporting the radially inner and outer extents of said vanes so that said vanes are pivotable about their longitudinal axes, each of said vanes being provided at each of its longitudinal extents with platform means to cooperate with said support structure to limit any radial movement of said vane, and bush means interposed between each of platform means and said support structure, means being provided to supply a cooling fluid to said bush means at pressure higher than that of any fluid operationally flowing over said vanes so that said cooling fluid flows between each of said bush means and at least one platform means and said support structure so the said cooling fluid is placed in heat exchange relationship with said bush means and is subsequently exhausted into said fluid operationally flowing over said vanes, each of said bush means adjacent a radially inner or outer platform being grooved to at least partially define passages for said cooling fluid.
Claim 3
Dependent Claim 82 words
A variable stator vane assembly as claimed in claim 1 wherein said cooling fluid is supplied to the region of the radially outer extent of each of said vanes, said cooling fluid so supplied being divided into two flow portions, a first flow portion which is directed to said bush means adjacent said radially outer platform, and a second flow portion which is directed via a longitudinal passage in each of said vanes to said bush means adjacent said radially inner platform.
Claim 4
Dependent Claim 57 words
A variable stator vane assembly as claimed in claim 1 wherein two separate flows of said cooling fluid from separate sources are supplied respectively to the radially inner and outer extents of each of said stator vanes to be placed in said heat exchange relationship with said bush means adjacent said radially inner and outer platforms respectively.
Claim 5
Dependent Claim 47 words
A variable stator vane assembly as claimed in claim 1 wherein each of said vanes is provided with a spigot extending radially from each of its extents, said spigots locating in corresponding bush means provided in said support structure to facilitate said pivotal movement of said vanes.
Claim 6
Dependent Claim 66 words
A stator vane assembly as claimed in claim 4 wherein each of said radially outer spigots is surrounded in spaced apart relationship by a sleeve so that a space is defined between them, said sleeves being positioned in a flow of said cooling fluid and apertured to permit said cooling fluid to flow through said so defined space and thence to said radially outer bush means.
Claim 7
Dependent Claim 26 words
A stator vane assembly as claimed in claim 1 wherein each of said radially outer spigots is provided with a lever to facilitate said vane pivoting.
Claim 8
Dependent Claim 15 words
A stator vane assembly as claimed in claim 1 wherein said cooling fluid is air.
Claim 9
Dependent Claim 21 words
A stator vane assembly as claimed in claim 1 wherein said vanes are positioned in the inlet of a power turbine.

References Cited (Backward Citations)

GB805015A Cited
US3284048A Cited
GB1072538A Cited
US3367628A Cited
GB1200348A Cited
GB1201949A Cited
US3542484A Cited
GB1263857A Cited
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GB2016091A Cited
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US4695777A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1992-08-28 1993-02-27 1993-08-29 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1996-08-28 1997-02-27 1997-08-29 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 2000-08-28 2001-02-27 2001-08-29 $7700.00 Window Closed / Lapsed

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