JPS6212801Y2 - - Google Patents

Info

Publication number
JPS6212801Y2
JPS6212801Y2 JP1982193440U JP19344082U JPS6212801Y2 JP S6212801 Y2 JPS6212801 Y2 JP S6212801Y2 JP 1982193440 U JP1982193440 U JP 1982193440U JP 19344082 U JP19344082 U JP 19344082U JP S6212801 Y2 JPS6212801 Y2 JP S6212801Y2
Authority
JP
Japan
Prior art keywords
cap
cavity
blade
gas turbine
side walls
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.)
Expired
Application number
JP1982193440U
Other languages
English (en)
Japanese (ja)
Other versions
JPS5997205U (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 JP19344082U priority Critical patent/JPS5997205U/ja
Publication of JPS5997205U publication Critical patent/JPS5997205U/ja
Application granted granted Critical
Publication of JPS6212801Y2 publication Critical patent/JPS6212801Y2/ja
Granted legal-status Critical Current

Links

JP19344082U 1982-12-21 1982-12-21 ガスタ−ビンの翼 Granted JPS5997205U (ja)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP19344082U JPS5997205U (ja) 1982-12-21 1982-12-21 ガスタ−ビンの翼

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP19344082U JPS5997205U (ja) 1982-12-21 1982-12-21 ガスタ−ビンの翼

Publications (2)

Publication Number Publication Date
JPS5997205U JPS5997205U (ja) 1984-07-02
JPS6212801Y2 true JPS6212801Y2 (enrdf_load_stackoverflow) 1987-04-03

Family

ID=30416047

Family Applications (1)

Application Number Title Priority Date Filing Date
JP19344082U Granted JPS5997205U (ja) 1982-12-21 1982-12-21 ガスタ−ビンの翼

Country Status (1)

Country Link
JP (1) JPS5997205U (enrdf_load_stackoverflow)

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2476207A1 (fr) * 1980-02-19 1981-08-21 Snecma Perfectionnement aux aubes de turbines refroidies

Also Published As

Publication number Publication date
JPS5997205U (ja) 1984-07-02

Similar Documents

Publication Publication Date Title
EP1132574B1 (en) Gas turbine cooled stationary blade
US3846041A (en) Impingement cooled turbine blades and method of making same
US6416282B1 (en) Rotor for a gas turbine
US4168938A (en) Blade or vane for a gas turbine engine
US4010531A (en) Tip cap apparatus and method of installation
US4224011A (en) Cooled rotor blade for a gas turbine engine
JP2862536B2 (ja) ガスタービンの翼
US6254346B1 (en) Gas turbine cooling moving blade
JP4713423B2 (ja) 斜め先端孔タービンブレード
US3982851A (en) Tip cap apparatus
US7056083B2 (en) Impingement cooling of gas turbine blades or vanes
US5813836A (en) Turbine blade
US5348446A (en) Bimetallic turbine airfoil
US5564902A (en) Gas turbine rotor blade tip cooling device
US7270515B2 (en) Turbine airfoil trailing edge cooling system with segmented impingement ribs
US20020197160A1 (en) Airfoil tip squealer cooling construction
US3973874A (en) Impingement baffle collars
EP2157280B1 (en) Gas turbine rotor blade
US20020187043A1 (en) Airfoil trailing edge cooling construction
EP2037081A1 (en) Platform cooling structure of gas turbine rotor blade
JPH08503530A (ja) 冷却可能なエアフォイル及び該エアフォイル鋳造用中子
US20040094287A1 (en) Elliptical core support and plug for a turbine bucket
US5779447A (en) Turbine rotor
US6739381B2 (en) Method of producing a turbine blade
JPH0211801A (ja) ガスタービン冷却動翼