JPS5959671U - gas turbine combustor - Google Patents
gas turbine combustorInfo
- Publication number
- JPS5959671U JPS5959671U JP15397382U JP15397382U JPS5959671U JP S5959671 U JPS5959671 U JP S5959671U JP 15397382 U JP15397382 U JP 15397382U JP 15397382 U JP15397382 U JP 15397382U JP S5959671 U JPS5959671 U JP S5959671U
- Authority
- JP
- Japan
- Prior art keywords
- gas turbine
- turbine combustor
- transition piece
- gas
- flow
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Landscapes
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。(57) [Abstract] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
第1図は従来のガスタービン燃焼器と燃焼ガスの流れの
状況を示した図、第2図は第1図めA−A線に沿う断面
でのフィルム冷却空気の流れを示した図、第3図は本考
案に係るガスタービン燃焼器の一実施例と燃焼ガスの流
れの状況を示した図、第4図は第3図のB−B線に沿う
断面でのフィルム冷却空気の流れを示した図である。
1・・・・・・燃焼器、3・・・・・・尾筒、4・・・
・・・高温ガス流、5.5a、5b・・・・・・フィル
ム冷却空気流、6・・・・・・背側壁面、7・・・・・
・腹側壁面、10・・・・・・スケーラ。Figure 1 is a diagram showing a conventional gas turbine combustor and the flow of combustion gas, Figure 2 is a diagram showing the flow of film cooling air in a cross section along line A-A in Figure 1, Figure 3 is a diagram showing an embodiment of the gas turbine combustor according to the present invention and the flow of combustion gas, and Figure 4 is a diagram showing the flow of film cooling air in a cross section taken along line B-B in Figure 3. FIG. 1... Combustor, 3... Transition piece, 4...
...High temperature gas flow, 5.5a, 5b... Film cooling air flow, 6... Back wall surface, 7...
- Ventral wall surface, 10...Scalar.
Claims (1)
筒を通してタービン部へ供給するガスタービン燃焼器に
おいて、ガスタービン燃焼器の出、口部に、燃焼ガスの
壁面近傍の流れに前記尾筒の背側へ向かう旋回を与える
ようにしたスワーラを設けたことを特徴とするガスター
ビン燃焼器。In a gas turbine combustor that has a tapered transition piece that is bent at the outlet and supplies combustion gas to the turbine section through the transition piece, a gas turbine combustor is provided with a flow of combustion gas near the wall surface at the exit and mouth of the gas turbine combustor. A gas turbine combustor characterized in that a swirler is provided to give a swirl toward the back side of the transition piece.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP15397382U JPS5959671U (en) | 1982-10-13 | 1982-10-13 | gas turbine combustor |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP15397382U JPS5959671U (en) | 1982-10-13 | 1982-10-13 | gas turbine combustor |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS5959671U true JPS5959671U (en) | 1984-04-18 |
JPS6311492Y2 JPS6311492Y2 (en) | 1988-04-04 |
Family
ID=30340490
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP15397382U Granted JPS5959671U (en) | 1982-10-13 | 1982-10-13 | gas turbine combustor |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS5959671U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2018181063A1 (en) * | 2017-03-27 | 2018-10-04 | 株式会社Ihi | Combustion device and gas turbine |
-
1982
- 1982-10-13 JP JP15397382U patent/JPS5959671U/en active Granted
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2018181063A1 (en) * | 2017-03-27 | 2018-10-04 | 株式会社Ihi | Combustion device and gas turbine |
JP2018162724A (en) * | 2017-03-27 | 2018-10-18 | 株式会社Ihi | Combustor and gas turbine |
Also Published As
Publication number | Publication date |
---|---|
JPS6311492Y2 (en) | 1988-04-04 |
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