US4297843A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Combustor of gas turbine with features for vibration reduction and increased cooling
Assignee: Hitachi Ltd
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Filing: 1979-10-12
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Granted: 1981-11-03
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Expires: 1999-10-12
Abstract
Abstract A combustor of a gas turbine having a plurality of liners defining combustion chambers, and transition pieces adapted to rectify the flow of the combustion gas discharged from the liners before the combustion gas is introduced to the turbine. A guide plate is disposed in the gap between each pair of adjacent transition pieces near the gas outlets of the latter so as to guide the flow of air to the radially outer surfaces of adjacent transition pieces, thereby to improve the cooling of these surfaces and, at the same time, to mechanically connect the adjacent transition pieces to suppress the vibration of the transition pieces.
Inventors
- 👤 Isao Sato
- 👤 Fumio Kato
- 👤 Yoshihiro Uchiyama
- 👤 Nobuyuki Iizuka
- 👤 Tsuneyuki Hata
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-06 12:52
CPC Classifications
F; F01; F01D; F01D9/00; F01D9/02; F01D9/023; F23; F23R; F23R3/00; F23R3/02; F23R3/42; F23R3/46; F05; F05D; F05D2240/00; F05D2240/10; F05D2240/12; F05D2240/126
Claims Analysis
Total Claims: 8
Claim 1
Independent Claim
123 words
A combustor of a gas turbine having a plurality of combustor liners, a plurality of transition pieces connected to respective liners and adapted to rectify the flow of combustion gas coming from said liners, and a plurality of outer casings surrounding respective combinations of said liners and said transition pieces, comprising a guide plate having a radial portion disposed in each gap formed between each pair of adjacent transition pieces, said guide plate being adapted to rectify the air flowing through said gap, each guide plate having circumferential members that overlie the transition pieces and are attached to the radial portion of the guide plate, and said circumferential members form a gap between the adjacent circumferential members for exit of the cooling air.
Claim 2
Dependent Claim
123 words
A combustor of a gas turbine having a plurality of combustor liners, a plurality of transition pieces connected to respective liners and adapted to rectify the flow of combustion gas coming from said liners, and a plurality of outer casings surrounding respective combinations of said liners and said transition pieces, comprising a guide plate having a radial portion disposed in each gap formed between each pair of adjacent transition pieces, said guide plate being adapted to rectify the air flowing through said gap, each guide plate having circumferential members that overlie the transition pieces and are attached to the radial portion of the guide plate, and said circumferential members form a gap between the adjacent circumferential members for exit of the cooling air.
Claim 3
Dependent Claim
30 words
A combustor of a gas turbine as claimed in claim 1, wherein each of said guide plates is disposed in the vicinity of the gas outlet of each transition piece.
Claim 4
Dependent Claim
34 words
A combustor of a gas turbine as claimed in claim 1 or 2, wherein each of said guide plates is connected to both of said transition pieces between which said guide plate is located.
Claim 5
Dependent Claim
69 words
A combustor of a gas turbine as claimed in claim 2, wherein radial portions of each of said guide plates are disposed in said gap near the gas outlets of adjacent transition pieces and circumferential portions of each of said guide plates extend circumferentially from the radially outer end of said radial portion to overlie the corners of the radially outer surfaces of gas outlets of adjacent transition pieces.
Claim 6
Dependent Claim
66 words
A combustor of gas turbine as claimed in claim 2, wherein each of said guide plates includes a base plate attached to a turbine casing of said gas turbine, and support members fixed to the side walls of said gas outlets of the adjacent transition pieces, each of said support members having a U-shaped channel section for receiving corresponding side edge portion of said base plate.
Claim 7
Dependent Claim
43 words
A combustor of a gas turbine as claimed in claim 4, wherein the clearance between said circumferential portion of said guide plate and said radially outer surface of said gas outlet of said transition piece is adjustable to provide the optimum cooling effect.
Claim 8
Dependent Claim
53 words
A combustor of a gas turbine as claimed in claim 5, wherein the state of fit of said U-shaped channel sections base plate in said of said support members is so selected as to permit the thermal expansion and shrinkage of said transition pieces but to suppress the vibration of said transition pieces.
References Cited (Backward Citations)
US2743579A
Cited
US3657882A
Cited
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1984-11-02 | 1985-05-04 | 1985-11-03 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1988-11-02 | 1989-05-04 | 1989-11-03 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1992-11-02 | 1993-05-04 | 1993-11-03 | $7700.00 | Window Closed / Lapsed |