JPS63143704U - - Google Patents

Info

Publication number
JPS63143704U
JPS63143704U JP3601887U JP3601887U JPS63143704U JP S63143704 U JPS63143704 U JP S63143704U JP 3601887 U JP3601887 U JP 3601887U JP 3601887 U JP3601887 U JP 3601887U JP S63143704 U JPS63143704 U JP S63143704U
Authority
JP
Japan
Prior art keywords
rotor blade
shroud
air
tip
air passage
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
Application number
JP3601887U
Other languages
Japanese (ja)
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed filed Critical
Priority to JP3601887U priority Critical patent/JPS63143704U/ja
Publication of JPS63143704U publication Critical patent/JPS63143704U/ja
Pending legal-status Critical Current

Links

Description

【図面の簡単な説明】[Brief explanation of drawings]

第1図は本考案の実施例を示すシユラウド付動
翼お平面図、第2図は第1図の正面図、第3図は
第1図の―線に沿う断面図、第4図は第1図
の―線に沿う断面図、第5図及び第6図は本
考案の実施例を示す斜視図である。 1,2,3……空気吐出口、4……空気通路、
5……シユラウド、6……シユラウドリブ、7…
…動翼。
Fig. 1 is a plan view of a rotor blade with a shroud showing an embodiment of the present invention, Fig. 2 is a front view of Fig. 1, Fig. 3 is a cross-sectional view taken along the - line of Fig. 1, and FIGS. 5 and 6 are perspective views showing embodiments of the present invention. 1, 2, 3...Air discharge port, 4...Air passage,
5...Shuroud, 6...Shuroud rib, 7...
...moving blades.

Claims (1)

【実用新案登録請求の範囲】[Scope of utility model registration request] 動翼の先端部にシユラウドを有するシユラウド
付動翼において、前記動翼の内部に空気通路を設
け、この空気通路に連通する空冷孔から冷却空気
を吐出して前記動翼の先端部及び前記シユラウド
の付根部を冷却するように構成したことを特徴と
するシユラウド付動翼。
In a rotor blade with a shroud having a shroud at the tip of the rotor blade, an air passage is provided inside the rotor blade, and cooling air is discharged from an air cooling hole communicating with the air passage to cover the tip of the rotor blade and the shroud. A rotor blade with a shroud, characterized in that the rotor blade is configured to cool the root portion of the rotor blade.
JP3601887U 1987-03-13 1987-03-13 Pending JPS63143704U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP3601887U JPS63143704U (en) 1987-03-13 1987-03-13

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP3601887U JPS63143704U (en) 1987-03-13 1987-03-13

Publications (1)

Publication Number Publication Date
JPS63143704U true JPS63143704U (en) 1988-09-21

Family

ID=30846041

Family Applications (1)

Application Number Title Priority Date Filing Date
JP3601887U Pending JPS63143704U (en) 1987-03-13 1987-03-13

Country Status (1)

Country Link
JP (1) JPS63143704U (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006316750A (en) * 2005-05-16 2006-11-24 Hitachi Ltd Gas turbine moving blade, gas turbine using the same, and its power generation plant
JP2011001919A (en) * 2009-06-21 2011-01-06 Toshiba Corp Turbine moving blade
JP2017198202A (en) * 2016-04-14 2017-11-02 ゼネラル・エレクトリック・カンパニイ System for cooling seal rails of tip shroud of turbine blade
JP2017210959A (en) * 2016-05-24 2017-11-30 ゼネラル・エレクトリック・カンパニイ Cooling passage for gas turbine rotor blade
US11225872B2 (en) 2019-11-05 2022-01-18 General Electric Company Turbine blade with tip shroud cooling passage

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2006316750A (en) * 2005-05-16 2006-11-24 Hitachi Ltd Gas turbine moving blade, gas turbine using the same, and its power generation plant
JP4628865B2 (en) * 2005-05-16 2011-02-09 株式会社日立製作所 Gas turbine blade, gas turbine using the same, and power plant
JP2011001919A (en) * 2009-06-21 2011-01-06 Toshiba Corp Turbine moving blade
JP2017198202A (en) * 2016-04-14 2017-11-02 ゼネラル・エレクトリック・カンパニイ System for cooling seal rails of tip shroud of turbine blade
JP2017210959A (en) * 2016-05-24 2017-11-30 ゼネラル・エレクトリック・カンパニイ Cooling passage for gas turbine rotor blade
US11225872B2 (en) 2019-11-05 2022-01-18 General Electric Company Turbine blade with tip shroud cooling passage

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