JPS6287102U - - Google Patents

Info

Publication number
JPS6287102U
JPS6287102U JP17740485U JP17740485U JPS6287102U JP S6287102 U JPS6287102 U JP S6287102U JP 17740485 U JP17740485 U JP 17740485U JP 17740485 U JP17740485 U JP 17740485U JP S6287102 U JPS6287102 U JP S6287102U
Authority
JP
Japan
Prior art keywords
rotor blade
cooling passage
airfoil portion
internal cooling
gas turbine
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
JP17740485U
Other languages
English (en)
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 JP17740485U priority Critical patent/JPS6287102U/ja
Publication of JPS6287102U publication Critical patent/JPS6287102U/ja
Pending legal-status Critical Current

Links

JP17740485U 1985-11-20 1985-11-20 Pending JPS6287102U (enExample)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP17740485U JPS6287102U (enExample) 1985-11-20 1985-11-20

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP17740485U JPS6287102U (enExample) 1985-11-20 1985-11-20

Publications (1)

Publication Number Publication Date
JPS6287102U true JPS6287102U (enExample) 1987-06-03

Family

ID=31118572

Family Applications (1)

Application Number Title Priority Date Filing Date
JP17740485U Pending JPS6287102U (enExample) 1985-11-20 1985-11-20

Country Status (1)

Country Link
JP (1) JPS6287102U (enExample)

Similar Documents

Publication Publication Date Title
US3628885A (en) Fluid-cooled airfoil
JP4575532B2 (ja) ディンプルを設けたインピンジメントバッフルを有する熱い壁
EP0955449B1 (en) Gas turbine blade
US6164914A (en) Cool tip blade
US6126396A (en) AFT flowing serpentine airfoil cooling circuit with side wall impingement cooling chambers
JPS61114005U (enExample)
CA2250169A1 (en) Cooled stationary blade of gas turbine
JPH0370084B2 (enExample)
JPH10274002A (ja) ガスタービンエンジンの動翼の冷却通路の乱流器構造
CA2261107A1 (en) Gas turbine moving blade
US3844678A (en) Cooled high strength turbine bucket
JP4175669B2 (ja) ガスタービン翼の後縁を冷却するための冷却チャンネル構造
US5577884A (en) Structure for a stationary cooled turbine vane
JPS6148610B2 (enExample)
JP3124109B2 (ja) ガスタービンの静翼
JP2953842B2 (ja) タービン静翼
EP1094200A1 (en) Gas turbine cooled moving blade
JPS59200001A (ja) ガスタ−ビン翼
JPS6287102U (enExample)
JP2938506B2 (ja) タービン静翼
JPS62153504A (ja) シユラウドセグメント
JPH04311604A (ja) タービン静翼
JPS6143927Y2 (enExample)
JPS587801B2 (ja) 高温タ−ビン冷却翼
JPS60182302A (ja) ガスタ−ビン冷却翼