Patent US4537634A successfully refreshed from Google Patents.
Patent US5120192A successfully refreshed from Google Patents.
US5120192A
Expired / Lapsed
US
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Cooled turbine blade and combined cycle power plant having gas turbine with this cooled turbine blade
Assignee: Toshiba Corp
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Filing: 1990-03-12
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Granted: 1992-06-09
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Expires: 2010-03-12
Abstract
Abstract A blade includes a blade body having a cavity, an insert inserted in the cavity, a plurality of impingement holes formed in a circumferential wall of the insert, and a recovery path for recovering a cooling medium sprayed from the impingement holes. The cooling medium can be recovered without being discharged into a main gas. A gas turbine having this blade is used for a combined cycle power plant. In this plant, steam is supplied as a cooling medium to the blade, and the steam recovered from the blade is supplied to a steam turbine.
Inventors
- 👤 Fumio Ohtomo
- 👤 Tatsuo Araki
- 👤 Asako Matsuura
- 👤 Yoshiaki Tsukumo
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-03 15:53
CPC Classifications
F; F01; F01D; F01D5/00; F01D5/12; F01D5/14; F01D5/18; F01D5/187; F01D5/188; F01D5/189; F02; F02C; F02C7/00; F02C7/12; F02C7/16; F05; F05D; F05D2240/00; F05D2240/80; F05D2240/81; F05D2260/00; F05D2260/20; F05D2260/201; F05D2260/232; F05D2260/2322
Claims Analysis
Total Claims: 10
Claim 1
Independent Claim
171 words
A cooled turbine blade through which a cooling medium passes, comprising: a blade body having cavities extending in a direction of spay, said cavities including at least a fore cavity formed in a front portion of said blade body and an aft cavity formed in a rear portion of said blade body; a fore hollow insert and an aft hollow insert mounted in said fore and aft cavities, respectively, an outer surface of a circumferential wall of said inserts and an inner wall surface of said blade body defining a gap therebetween, said circumferential wall of said inserts being provided with a plurality of impingement holes, and the cooling medium being sprayed from said impingement holes to said inner wall surface of said blade body; and recovery paths formed in one-end portions of said fore and aft cavities, respectively, the cooling medium sprayed from said impingement holes cooling a wall of said blade body and flowing in said recovery paths and being recovered from said blade body through said recovery paths.
Claim 2
Dependent Claim
171 words
A cooled turbine blade through which a cooling medium passes, comprising: a blade body having cavities extending in a direction of spay, said cavities including at least a fore cavity formed in a front portion of said blade body and an aft cavity formed in a rear portion of said blade body; a fore hollow insert and an aft hollow insert mounted in said fore and aft cavities, respectively, an outer surface of a circumferential wall of said inserts and an inner wall surface of said blade body defining a gap therebetween, said circumferential wall of said inserts being provided with a plurality of impingement holes, and the cooling medium being sprayed from said impingement holes to said inner wall surface of said blade body; and recovery paths formed in one-end portions of said fore and aft cavities, respectively, the cooling medium sprayed from said impingement holes cooling a wall of said blade body and flowing in said recovery paths and being recovered from said blade body through said recovery paths.
Claim 3
Dependent Claim
35 words
A blade according to claim 1, which further comprises a communication path through which the cooling medium sprayed from said fore insert and recovered through said fore recovery path is supplied to said aft insert.
Claim 4
Dependent Claim
43 words
A blade according to claim 2, wherein an auxiliary supply port is formed to communicate with said communication path, and a flow of the cooling medium supplied to said aft insert is added with a new cooling medium through said auxiliary supply port.
Claim 5
Dependent Claim
56 words
A blade according to claim 1, wherein a trailing edge cooling path is formed in a trailing edge portion of said blade body, and the cooling medium is supplied to said trailing edge cooling path, cools said trailing edge portion, and is discharged from said tailing edge portion of said blade body in a main gas.
Claim 6
Dependent Claim
120 words
A blade according to claim 1, wherein film cooling holes which communicate with said cavity and open to said outer wall surface of said blade body are formed in said wall of said blade body and part of the cooling medium sprayed from said insert flows as a film-like flow along said outer wall surface of said blade body; and baffles are arranged between said outer circumferential surface of said wall of said insert and said inner wall surface of said blade body in the direction of chord, and a flow of the cooling medium in the direction of span is regulated by said baffles, thereby controlling a flow rate of the cooling medium sprayed from said film cooling holes.
Claim 7
Dependent Claim
18 words
A blade according to claim 1, wherein shrouds are respectively formed at both tips of said blade body.
Claim 8
Dependent Claim
24 words
A blade according to claim 6, wherein cooling paths are respectively formed in said shrouds and receive the cooling medium, thereby cooling said shrouds.
Claim 9
Dependent Claim
24 words
The blade according to claim 6, wherein the cooling medium recovered in said recovery path is supplied to said cooling path of said shrouds.
Claim 10
Dependent Claim
34 words
The blade according to claim 6, wherein an auxiliary supply port communicating with said cooling path of said shrouds, and new cooling medium is added to the cooling path through the auxiliary supply port.
References Cited (Backward Citations)
CA853499A
Cited
US2779565A
Cited
US2873944A
Cited
FR1404931A
Cited
DE2065334A1
Cited
US3891348A
Cited
FR2174497A7
Cited
FR2457965A1
Cited
CA1050895A
Cited
US4180373A
Cited
JPS5514241A
Cited
JPS55107005A
Cited
GB2054749A
Cited
GB2093923A
Cited
JPS5985305A
Cited
JPS6340244A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1995-06-09 | 1995-12-09 | 1996-06-09 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1999-06-09 | 1999-12-09 | 2000-06-09 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 2003-06-09 | 2003-12-09 | 2004-06-09 | $7700.00 | Window Closed / Lapsed |