JPS613903U - gas turbine nozzle - Google Patents
gas turbine nozzleInfo
- Publication number
- JPS613903U JPS613903U JP8806284U JP8806284U JPS613903U JP S613903 U JPS613903 U JP S613903U JP 8806284 U JP8806284 U JP 8806284U JP 8806284 U JP8806284 U JP 8806284U JP S613903 U JPS613903 U JP S613903U
- Authority
- JP
- Japan
- Prior art keywords
- gas turbine
- turbine nozzle
- nozzle
- flanges
- nozzle blade
- 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
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図は従来用いられている単翼ノズルの構造図、第2
図は従来用いられている多枚翼ノズルの構造図、第3図
は従来用いられているノズル翼の内部構造図、第4図は
本考案の一実施例の単翼ノズルの構造図、第5図は同じ
く多枚翼ノズルの構造図、第6、第7図は第5図の外周
側からの矢視図である。
1・・・ノズル翼、2・・・内周側フランジ、2a・・
・内周側前縁部ジランジ、2b・・・内周側後縁部フラ
ンジ、3・・・外周側フランジ、3a・・・外周側前縁
部フランジ、3b・・・外周側後縁部フランジ、4・・
・燃焼空気、5・・・冷却空気、”6・・・冷却孔、7
・・・内輪、8・・・シール、9・・・シール用溝。Figure 1 is a structural diagram of a conventionally used single-blade nozzle, Figure 2
Figure 3 is a structural diagram of a conventionally used multi-blade nozzle, Figure 3 is an internal structural diagram of a conventionally used nozzle blade, and Figure 4 is a structural diagram of a single-blade nozzle according to an embodiment of the present invention. Similarly, FIG. 5 is a structural diagram of the multi-blade nozzle, and FIGS. 6 and 7 are views taken from the outer peripheral side of FIG. 1... Nozzle blade, 2... Inner peripheral side flange, 2a...
・Inner circumference side front edge flange, 2b...Inner circumference side rear edge flange, 3...Outer circumference side flange, 3a...Outer circumference side front edge flange, 3b...Outer circumference side rear edge flange , 4...
・Combustion air, 5... Cooling air, "6... Cooling hole, 7
... Inner ring, 8... Seal, 9... Seal groove.
Claims (1)
ーシングにノズル翼を固定する構造においソ、内外周両
方のフランジ、又は、どちらか一方のフランジがノズル
翼のコード方向に沿って、完全に分割されるか、又は、
1部が切断されることを特徴とするガスター,ビンノズ
ル。In a structure in which the nozzle blade is fixed to the casing using flanges provided on the outer and inner circumferential sides of the nozzle blade, both the inner and outer flanges, or either one of the flanges are completely aligned along the cord direction of the nozzle blade. be divided or
A gaster or bottle nozzle characterized in that one part is cut off.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP8806284U JPS613903U (en) | 1984-06-15 | 1984-06-15 | gas turbine nozzle |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP8806284U JPS613903U (en) | 1984-06-15 | 1984-06-15 | gas turbine nozzle |
Publications (1)
Publication Number | Publication Date |
---|---|
JPS613903U true JPS613903U (en) | 1986-01-11 |
Family
ID=30640848
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP8806284U Pending JPS613903U (en) | 1984-06-15 | 1984-06-15 | gas turbine nozzle |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS613903U (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2012510582A (en) * | 2008-12-05 | 2012-05-10 | シーメンス アクティエンゲゼルシャフト | Guide vane array structure for axial turbomachinery |
-
1984
- 1984-06-15 JP JP8806284U patent/JPS613903U/en active Pending
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2012510582A (en) * | 2008-12-05 | 2012-05-10 | シーメンス アクティエンゲゼルシャフト | Guide vane array structure for axial turbomachinery |
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