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US3736071A Expired / Lapsed US ⏱️ 0.0 years remaining

Bucket tip/collection slot combination for open-circuit liquid-cooled gas turbines

Assignee: General Electric Co
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Filing: 1970-11-27
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Granted: 1973-05-29
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Expires: 1990-11-27
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Abstract

Abstract Bucket tip designs are shown for manifolding fluid discharge from open-ended coolant passages in a liquid-cooled gas turbine. The manifolded fluid (e.g., steam and excess water in a watercooled system) is discharged from the trailing edge of the bucket and liquid content thereof is thrown into a collection slot located in register therewith in the wall of the casing.

Inventors

  • 👤 P H Kydd

Bibliographic Details

Application Number —
Jurisdiction US
Data Source google_patents
Last Synchronized 2026-10-25 21:26
CPC Classifications
F; F01; F01D; F01D5/00; F01D5/12; F01D5/14; F01D5/18; F01D5/185; F01D5/02; F01D5/08; F05; F05B; F05B2240/00; F05B2240/80; F05B2240/801; F05D; F05D2240/00; F05D2240/80; F05D2240/81

Claims Analysis

Total Claims: 10
Claim 1
Independent Claim 358 words
In a gas turbine wherein a turbine disk is mounted on a shaft rotatably supported in a casing, said turbine disk extending substantially perpendicular to the axis of said shaft and having turbine buckets and platform means affixed to the outer rim thereof, said buckets receiving a driving force from a hot motive fluid confined within said casing and moving in a direction generally parallel to said axis of said shaft and the driving force being transmitted to said shaft via said turbine disk, means located radially inward of said platform adjacent said turbine disk for introducing liquid coolant within said turbine in a radially outward direction into open-circuit distribution paths by which said coolant traverses surface area of said rim and said platform means, passes into cooling channels in said buckets and exits from said channels in a radially outward direction, the improvement comprising: a manifolding, discharge and collection system for the coolant fluid exiting from the coolant channels in the turbine buckets, said system consisting of 1. first and second interconnected manifolds located beneath the bucket surface near the tip of each bucket in flow communication with the discharge ends of the coolant channels, said first and second manifolds being located on the pressure and suction sides of said bucket, respectively, 2. a single opening through the blade structure interconnecting said first manifold and the region of hot motive fluid flow within the casing near the trailing edge of said bucket, each of said manifolds being separated from the tip of said bucket by a wall formed in the bucket structure on the radially outward side of said manifold and extending generally chordwise of said bucket whereby coolant discharged radially from said coolant channels is redirected as required to reach said opening, and 3. liquid collection means located in the casing wall closely adjacent said trailing edge in register with said opening whereby open-circuit flow conditions are maintained with coolant fluid being discharged radially from said coolant channels into said manifolds, redirected and discharged from said first manifold through said opening into the hot motive fluid flow with excess liquid being thrown into said collection means.
Claim 2
Dependent Claim 358 words
In a gas turbine wherein a turbine disk is mounted on a shaft rotatably supported in a casing, said turbine disk extending substantially perpendicular to the axis of said shaft and having turbine buckets and platform means affixed to the outer rim thereof, said buckets receiving a driving force from a hot motive fluid confined within said casing and moving in a direction generally parallel to said axis of said shaft and the driving force being transmitted to said shaft via said turbine disk, means located radially inward of said platform adjacent said turbine disk for introducing liquid coolant within said turbine in a radially outward direction into open-circuit distribution paths by which said coolant traverses surface area of said rim and said platform means, passes into cooling channels in said buckets and exits from said channels in a radially outward direction, the improvement comprising: a manifolding, discharge and collection system for the coolant fluid exiting from the coolant channels in the turbine buckets, said system consisting of 1. first and second interconnected manifolds located beneath the bucket surface near the tip of each bucket in flow communication with the discharge ends of the coolant channels, said first and second manifolds being located on the pressure and suction sides of said bucket, respectively, 2. a single opening through the blade structure interconnecting said first manifold and the region of hot motive fluid flow within the casing near the trailing edge of said bucket, each of said manifolds being separated from the tip of said bucket by a wall formed in the bucket structure on the radially outward side of said manifold and extending generally chordwise of said bucket whereby coolant discharged radially from said coolant channels is redirected as required to reach said opening, and 3. liquid collection means located in the casing wall closely adjacent said trailing edge in register with said opening whereby open-circuit flow conditions are maintained with coolant fluid being discharged radially from said coolant channels into said manifolds, redirected and discharged from said first manifold through said opening into the hot motive fluid flow with excess liquid being thrown into said collection means.
Claim 3
Dependent Claim 81 words
a single opening through the blade structure interconnecting said first manifold and the region of hot motive fluid flow within the casing near the trailing edge of said bucket, each of said manifolds being separated from the tip of said bucket by a wall formed in the bucket structure on the radially outward side of said manifold and extending generally chordwise of said bucket whereby coolant discharged radially from said coolant channels is redirected as required to reach said opening, and
Claim 4
Dependent Claim 81 words
a single opening through the blade structure interconnecting said first manifold and the region of hot motive fluid flow within the casing near the trailing edge of said bucket, each of said manifolds being separated from the tip of said bucket by a wall formed in the bucket structure on the radially outward side of said manifold and extending generally chordwise of said bucket whereby coolant discharged radially from said coolant channels is redirected as required to reach said opening, and
Claim 5
Dependent Claim 45 words
The improvement of claim 1 wherein each of the manifolds consists of a slot formed in the bucket core and extending from leading edge to trailing edge, the two slots being interconnected near the opening by a passage extending through the separating bucket core material.
Claim 6
Dependent Claim 16 words
The improvement of claim 1 wherein the opening is in the trailing edge of the bucket.
Claim 7
Dependent Claim 62 words
liquid collection means located in the casing wall closely adjacent said trailing edge in register with said opening whereby open-circuit flow conditions are maintained with coolant fluid being discharged radially from said coolant channels into said manifolds, redirected and discharged from said first manifold through said opening into the hot motive fluid flow with excess liquid being thrown into said collection means.
Claim 8
Dependent Claim 62 words
liquid collection means located in the casing wall closely adjacent said trailing edge in register with said opening whereby open-circuit flow conditions are maintained with coolant fluid being discharged radially from said coolant channels into said manifolds, redirected and discharged from said first manifold through said opening into the hot motive fluid flow with excess liquid being thrown into said collection means.
Claim 9
Dependent Claim 19 words
The improvement of claim 1 wherein the opening is through the top of the bucket near the trailing edge.
Claim 10
Dependent Claim 39 words
The improvement in claim 1 wherein the root of each bucket is in the form of a plurality of spaced tines fitting between and bonded to the walls of annular grooves in the outer rim of the turbine disk.

References Cited (Backward Citations)

DE346599C Cited
DE383506C Cited
CA588243A Cited
DE386276C Cited
FR726545A Cited
GB586838A Cited
US2848192A Cited
US3533712A Cited
US3532438A Cited
US3446481A Cited

USPTO Annuity & Maintenance Windows

Annuity Stage Window Opens Payment Deadline Surcharge Period Until Estimated Fee Status
3.5 Years (Year 4) 1976-05-28 1976-11-27 1977-05-29 $2000.00 Window Closed / Lapsed
7.5 Years (Year 8) 1980-05-28 1980-11-27 1981-05-29 $3760.00 Window Closed / Lapsed
11.5 Years (Year 12) 1984-05-28 1984-11-27 1985-05-29 $7700.00 Window Closed / Lapsed

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