JPS61192166U - - Google Patents
Info
- Publication number
- JPS61192166U JPS61192166U JP7341385U JP7341385U JPS61192166U JP S61192166 U JPS61192166 U JP S61192166U JP 7341385 U JP7341385 U JP 7341385U JP 7341385 U JP7341385 U JP 7341385U JP S61192166 U JPS61192166 U JP S61192166U
- Authority
- JP
- Japan
- Prior art keywords
- transition piece
- combustor
- turbine
- connects
- working gas
- 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.)
- Pending
Links
- 230000007704 transition Effects 0.000 claims description 5
- 239000012530 fluid Substances 0.000 claims 2
- 238000010586 diagram Methods 0.000 description 2
- 239000000567 combustion gas Substances 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
Description
第１図は本考案の多缶燃焼器の場合の一実施例
の構成図である。第２図は従来の多缶燃焼器の断
面図、第３図は従来の多缶燃焼器尾筒周囲の流速
分布図、第４図は従来例の部分断面図、第５図は
考案の多缶燃焼器の場合の他の実施例、第６図は
本考案の単缶燃焼器の場合の一実施例の断面図で
ある。
２……圧縮機、３……タービン、４……燃焼ガ
ス、５……空気、１１……外筒、１２……内筒、
１３……尾筒、１４……ケーシング、１５……車
室、１６……デイフユーザ、２０……貫通流路。
FIG. 1 is a block diagram of an embodiment of the multi-can combustor of the present invention. Fig. 2 is a sectional view of a conventional multi-can combustor, Fig. 3 is a flow velocity distribution diagram around the transition piece of a conventional multi-can combustor, Fig. 4 is a partial sectional view of the conventional example, and Fig. 5 is a devised multi-can combustor. Another embodiment for a can combustor: FIG. 6 is a sectional view of an embodiment for a single can combustor of the present invention. 2... Compressor, 3... Turbine, 4... Combustion gas, 5... Air, 11... Outer cylinder, 12... Inner cylinder,
13... Transition piece, 14... Casing, 15... Vehicle interior, 16... Diffusion user, 20... Through flow path.
Claims (1)
器の内筒と、作動ガス流体を仕事に変換するター
ビンを連結する尾筒において、尾筒出口近傍に尾
筒腹側の背側とを連結する貫通流路を一本以上設
けたことを特徴とするガスタービン燃焼器。 In the transition piece that connects the inner cylinder of the combustor that generates the working gas fluid of the gas turbine and the turbine that converts the working gas fluid into work, a through flow connects the ventral side of the transition piece near the exit of the transition piece. A gas turbine combustor characterized by having one or more passages.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7341385U JPS61192166U (en) | 1985-05-20 | 1985-05-20 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP7341385U JPS61192166U (en) | 1985-05-20 | 1985-05-20 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS61192166U true JPS61192166U (en) | 1986-11-29 |
Family
ID=30612754
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP7341385U Pending JPS61192166U (en) | 1985-05-20 | 1985-05-20 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS61192166U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2008169837A (en) * | 2007-01-09 | 2008-07-24 | General Electric Co <Ge> | Airfoil, sleeve and method for assembling combustor assembly |
-
1985
- 1985-05-20 JP JP7341385U patent/JPS61192166U/ja active Pending
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2008169837A (en) * | 2007-01-09 | 2008-07-24 | General Electric Co <Ge> | Airfoil, sleeve and method for assembling combustor assembly |
| US8387396B2 (en) | 2007-01-09 | 2013-03-05 | General Electric Company | Airfoil, sleeve, and method for assembling a combustor assembly |
| KR101437171B1 (en) * | 2007-01-09 | 2014-09-03 | 제너럴 일렉트릭 캄파니 | Airfoil, sleeve, and method for assembling a combustor assembly |