US4504189A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Stator vane for a gas turbine engine
Assignee: Rolls Royce PLC
•
Filing: 1983-10-26
•
Granted: 1985-03-12
•
Expires: 2003-10-26
Abstract
Abstract A vane for a gas turbine engine has an aerofoil of unconventional shape. The stacking of sections which defines the aerofoil is arranged to produce an aerofoil whose concave flank is convex in spanwise sections and whose convex flank is concave in spanwise sections. In order to reduce the problems produced by the resulting shape of trailing edge the sections are stacked so that all their trailing edges lie in a plane substantially parallel with the plane of the throat formed between the trailing edge and the next adjacent vane in an array.
Inventors
- 👤 Barry W. Lings
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-10-31 00:16
CPC Classifications
F; F01; F01D; F01D9/00; F01D9/02; F01D9/04; F01D9/041; F01D5/00; F01D5/12; F01D5/14; F01D5/141; Y; Y02; Y02T; Y02T50/00; Y02T50/60; Y10; Y10S; Y10S415/00; Y10S415/914
Claims Analysis
Total Claims: 4
Claim 1
Independent Claim
222 words
A stator vane assembly for a gas turbine engine comprising: a plurality of vanes arranged in an annular array, each of said vanes including an aerofoil having a convex flank, a concave flank and a continuous spanwise extending trailing edge, a throat between each of adjacent vanes, each said throat being defined by said continuous spanwise extending trailing edge of a particular one of said vanes and said convex flank of the adjacent vane in said annular array, said aerofoil of each of said vanes having an aerodynamic profile defined by a stack of planar elemental aerofoil sections, each of said planar elemental aerofoil sections of each one of said vanes having a trailing edge forming part of said spanwise trailing edge of said aerofoil of the particular one of each one of said vanes, said planar elemental aerofoil sections for each of said vanes being stacked to provide said concave flank of said aerofoil of each of said vanes with a concave shape in the spanwise direction and to provide said convex flank of said aerofoil of each of said vanes with a concave shape in the spanwise direction, said trailing edges of the stack of said planar elemental aerofoil sections of each of said vanes being disposed in a single plane extending substantially parallel with said throat between adjacent vanes.
Claim 2
Dependent Claim
222 words
A stator vane assembly for a gas turbine engine comprising: a plurality of vanes arranged in an annular array, each of said vanes including an aerofoil having a convex flank, a concave flank and a continuous spanwise extending trailing edge, a throat between each of adjacent vanes, each said throat being defined by said continuous spanwise extending trailing edge of a particular one of said vanes and said convex flank of the adjacent vane in said annular array, said aerofoil of each of said vanes having an aerodynamic profile defined by a stack of planar elemental aerofoil sections, each of said planar elemental aerofoil sections of each one of said vanes having a trailing edge forming part of said spanwise trailing edge of said aerofoil of the particular one of each one of said vanes, said planar elemental aerofoil sections for each of said vanes being stacked to provide said concave flank of said aerofoil of each of said vanes with a concave shape in the spanwise direction and to provide said convex flank of said aerofoil of each of said vanes with a concave shape in the spanwise direction, said trailing edges of the stack of said planar elemental aerofoil sections of each of said vanes being disposed in a single plane extending substantially parallel with said throat between adjacent vanes.
Claim 3
Dependent Claim
37 words
A stator vane assembly as claimed in claim 1 and in which said stack of said aerofoil of each of said vanes is hollow and provided with means for cooling it by the passage of cooling fluid.
Claim 4
Dependent Claim
27 words
A stator vane assembly as claimed in claim 1 and in which said planar elemental sections of each of said vanes are all of the same shape.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1988-03-11 | 1988-09-10 | 1989-03-12 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1992-03-11 | 1992-09-10 | 1993-03-12 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1996-03-11 | 1996-09-10 | 1997-03-12 | $7700.00 | Window Closed / Lapsed |