JPS587062U - gas turbine combustor - Google Patents
gas turbine combustorInfo
- Publication number
- JPS587062U JPS587062U JP10012581U JP10012581U JPS587062U JP S587062 U JPS587062 U JP S587062U JP 10012581 U JP10012581 U JP 10012581U JP 10012581 U JP10012581 U JP 10012581U JP S587062 U JPS587062 U JP S587062U
- Authority
- JP
- Japan
- Prior art keywords
- cylinder
- gas turbine
- turbine combustor
- diffuser
- inner cylinder
- 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
Landscapes
- Flow Control (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) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.
Description
第１図は従来のバイパス空気供給構造を示すガスタービ
ン燃焼器の断面図、第２図は本考案のバイパス空気構造
を示す断面図、および第３図は第２図の要部の拡大断面
図である。
３・・・・・・内筒、慢・・・・・・接続図、５・・・
・・・尾筒、６・・・・・・ディフューザ、９・・・・
・・尾筒サポート、１１・・・・・・スプリングシール
、１２・・・・・・穴、１３・・・・・・バイパス空気
供給管、１５・・・・・・調節弁。Fig. 1 is a sectional view of a gas turbine combustor showing a conventional bypass air supply structure, Fig. 2 is a sectional view showing a bypass air structure of the present invention, and Fig. 3 is an enlarged sectional view of the main parts of Fig. 2. It is. 3... Inner cylinder, long... Connection diagram, 5...
... Tail tube, 6... Diffuser, 9...
... Transition pipe support, 11 ... Spring seal, 12 ... Hole, 13 ... Bypass air supply pipe, 15 ... Control valve.
Claims (1)
続筒、尾筒およびディフューザを含むガスタービン燃焼
器において、前記筒を接続筒の奥まで伸ばしこれら内筒
と接続筒とで前記スプリングシールを介して２重円筒構
造を形成させ、前記接続筒はバイパス空気供給管を介し
てディフューザに接続し、前記２重円筒部に対応する内
筒部分には空気導通穴を設け、前記バイパス空気管の途
中に空気流量調節用の弁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 includes an inner cylinder, a connecting cylinder connected to the inner cylinder via a spring seal, a transition cylinder, and a diffuser, the cylinder is extended to the depths of the connecting cylinder and the spring seal is formed between the inner cylinder and the connecting cylinder. The connecting cylinder is connected to the diffuser through the bypass air supply pipe, and an air passage hole is provided in the inner cylinder portion corresponding to the double cylinder part, and the bypass air pipe is connected to the diffuser. It is characterized by having a valve for adjusting the air flow rate in the middle.
Gas turbine combustor.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP10012581U JPS587062U (en) | 1981-07-07 | 1981-07-07 | gas turbine combustor |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP10012581U JPS587062U (en) | 1981-07-07 | 1981-07-07 | gas turbine combustor |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS587062U true JPS587062U (en) | 1983-01-18 |
Family
ID=29894831
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP10012581U Pending JPS587062U (en) | 1981-07-07 | 1981-07-07 | gas turbine combustor |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS587062U (en) |
-
1981
- 1981-07-07 JP JP10012581U patent/JPS587062U/en active Pending
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