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US4229140A Expired / Lapsed US ⏱️ 0.0 years remaining

Turbine blade

Assignee: Rolls Royce PLC
•
Filing: 1978-12-15
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Granted: 1980-10-21
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Expires: 1998-12-15
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Abstract

Abstract A turbine blade comprising an aerofoil-shaped body having a main portion and a trailing portion, the latter being of undulating shape so as to define at each side of the blade chordally extending troughs. The blade may include cooling air holes extending from the interior of the main portion to a surface of the troughs.

Inventors

  • 👤 Alexander Scott

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-11-05 22:00
CPC Classifications
F; F01; F01D; F01D5/00; F01D5/12; F01D5/22; F01D5/225; F01D5/14; F01D5/141; F01D5/18; F01D5/187; F05; F05D; F05D2240/00; F05D2240/10; F05D2240/12; F05D2240/122; F05D2240/20; F05D2240/30; F05D2240/304; Y; Y02; Y02T; Y02T50/00; Y02T50/60

Claims Analysis

Total Claims: 4
Claim 1
Independent Claim 130 words
A turbine blade comprising an aerofoil-shaped body having spanwise and chordal extent and including a main portion and a trailing portion, the trailing portion having an upstream end integral with the main portion and a free downstream extremity, the trailing portion being a single wall having an undulating shape defining exteriorly of the wall and at each side thereof chordally extending troughs and ribs, wherein any one rib at one side of the wall has a hollow back defined by one of said troughs at the other side of the wall, and wherein the troughs are open to said downstream extremity and terminate at said upstream end, and cooling air holes extending between the interior of the main portion and the troughs at at least one side of the wall.
Claim 2
Dependent Claim 130 words
A turbine blade comprising an aerofoil-shaped body having spanwise and chordal extent and including a main portion and a trailing portion, the trailing portion having an upstream end integral with the main portion and a free downstream extremity, the trailing portion being a single wall having an undulating shape defining exteriorly of the wall and at each side thereof chordally extending troughs and ribs, wherein any one rib at one side of the wall has a hollow back defined by one of said troughs at the other side of the wall, and wherein the troughs are open to said downstream extremity and terminate at said upstream end, and cooling air holes extending between the interior of the main portion and the troughs at at least one side of the wall.
Claim 3
Dependent Claim 27 words
A turbine blade according to claim 1 wherein the holes are positioned to emanate from the main portion in the direction of the length of the troughs.
Claim 4
Dependent Claim 65 words
A turbine blade according to claim 2 wherein at at least one side of the wall there are troughs whose depth is such that there is formed at the upstream end of the trough another wall having a surface which is aerodynamically discontinuous with the surface of the main portion, and said holes are arranged to be open to the trough at said wall surface.

References Cited (Backward Citations)

US2238749A Cited
US2647368A Cited
GB1222565A Cited
US3423069A Cited
US3628885A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1983-10-21 1984-04-21 1984-10-21 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1987-10-21 1988-04-21 1988-10-21 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1991-10-21 1992-04-21 1992-10-21 $7700.00 Window Closed / Lapsed

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