JPS6295103U - - Google Patents
Info
- Publication number
- JPS6295103U JPS6295103U JP18607885U JP18607885U JPS6295103U JP S6295103 U JPS6295103 U JP S6295103U JP 18607885 U JP18607885 U JP 18607885U JP 18607885 U JP18607885 U JP 18607885U JP S6295103 U JPS6295103 U JP S6295103U
- Authority
- JP
- Japan
- Prior art keywords
- partition wall
- blade
- gas turbine
- hollow part
- stator vane
- 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
- 238000005192 partition Methods 0.000 claims description 5
- 238000001816 cooling Methods 0.000 claims description 2
- 238000010586 diagram Methods 0.000 description 1
- 239000011148 porous material Substances 0.000 description 1
Description
第１図は本考案の一実施例の静翼の断面図、第
２図は本考案の静翼隔壁部の拡大図、第３図は静
翼の全体構造の概略図、第４図は従来構造の静翼
の翼部断面図である。
１…翼部、２…エンドウオール、３…インサー
トコア、４…細孔、５…フイルム冷却孔、６…後
縁吹出孔、７…隔壁、８…連通孔、９…翼壁、１
０…断熱層。
Fig. 1 is a sectional view of a stator vane according to an embodiment of the present invention, Fig. 2 is an enlarged view of the stator vane partition of the present invention, Fig. 3 is a schematic diagram of the overall structure of the stator vane, and Fig. 4 is a conventional one. FIG. 2 is a sectional view of a vane portion of a stator vane of the structure. DESCRIPTION OF SYMBOLS 1... Wing part, 2... End wall, 3... Insert core, 4... Pore, 5... Film cooling hole, 6... Trailing edge blow-off hole, 7... Partition wall, 8... Communication hole, 9... Wing wall, 1
0...Insulating layer.
Claims (1)
け、前記中空部に冷却空気を導入して翼部を冷却
する静翼において、 前記隔壁に断熱層を設け、前記隔壁が過度に冷
却されることを防止したことを特徴とするガスタ
ービン用静翼。[Claims for Utility Model Registration] A stator vane that includes a hollow part and a partition wall inside a gas turbine stator blade, and cools the blade part by introducing cooling air into the hollow part, wherein a heat insulating layer is provided in the partition wall; A stationary blade for a gas turbine, characterized in that the partition wall is prevented from being excessively cooled.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP18607885U JPS6295103U (en) | 1985-12-04 | 1985-12-04 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP18607885U JPS6295103U (en) | 1985-12-04 | 1985-12-04 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| JPS6295103U true JPS6295103U (en) | 1987-06-17 |
Family
ID=31135306
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP18607885U Pending JPS6295103U (en) | 1985-12-04 | 1985-12-04 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS6295103U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2019509459A (en) * | 2016-03-25 | 2019-04-04 | ゼネラル・エレクトリック・カンパニイ | Integrated combustor nozzle for split annular combustion system |
-
1985
- 1985-12-04 JP JP18607885U patent/JPS6295103U/ja active Pending
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2019509459A (en) * | 2016-03-25 | 2019-04-04 | ゼネラル・エレクトリック・カンパニイ | Integrated combustor nozzle for split annular combustion system |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JPS6295103U (en) | ||
| JPS6434404U (en) | ||
| JPS6314803U (en) | ||
| JPS616606U (en) | Gas turbine combustor blade cooling mechanism | |
| JPS63143704U (en) | ||
| JPS6375502U (en) | ||
| JPS6112903U (en) | gas turbine air cooling blade | |
| JPS61186702U (en) | ||
| JPS62101008U (en) | ||
| JPS62168756U (en) | ||
| JPS6184379U (en) | ||
| JPS5857501U (en) | turbine blade | |
| JPS62167802U (en) | ||
| JPS59168501U (en) | Gas turbine stator blade segment | |
| JPS6298701U (en) | ||
| JPS61116101U (en) | ||
| JPS61459U (en) | Ventilation structure of valve water turbine generator | |
| JPS62162446U (en) | ||
| JPS6210288U (en) | ||
| JPH0294440U (en) | ||
| JPS6163402U (en) | ||
| JPS59139502U (en) | Shroud ring for gas turbine | |
| JPH0240346U (en) | ||
| JPS62182940U (en) | ||
| JPS59131903U (en) | axial flow turbine |