JPS5434088B2 - - Google Patents

Info

Publication number
JPS5434088B2
JPS5434088B2 JP8721673A JP8721673A JPS5434088B2 JP S5434088 B2 JPS5434088 B2 JP S5434088B2 JP 8721673 A JP8721673 A JP 8721673A JP 8721673 A JP8721673 A JP 8721673A JP S5434088 B2 JPS5434088 B2 JP S5434088B2
Authority
JP
Japan
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
JP8721673A
Other versions
JPS4985410A (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
Publication of JPS4985410A publication Critical patent/JPS4985410A/ja
Publication of JPS5434088B2 publication Critical patent/JPS5434088B2/ja
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00—Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12—Blades
    • F01D5/14—Form or construction
    • F01D5/18—Hollow blades, i.e. blades with cooling or heating channels or cavities; Heating, heat-insulating or cooling means on blades
    • F01D5/187—Convection cooling
    • F01D5/188—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall
    • F01D5/189—Convection cooling with an insert in the blade cavity to guide the cooling fluid, e.g. forming a separation wall the insert having a tubular cross-section, e.g. airfoil shape
JP8721673A 1972-08-02 1973-08-02 Expired JPS5434088B2 (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3605872A GB1400285A (en) 1972-08-02 1972-08-02 Hollow cooled vane or blade for a gas turbine engine

Publications (2)

Publication Number Publication Date
JPS4985410A JPS4985410A (ja) 1974-08-16
JPS5434088B2 true JPS5434088B2 (ja) 1979-10-24

Family

ID=10384477

Family Applications (1)

Application Number Title Priority Date Filing Date
JP8721673A Expired JPS5434088B2 (ja) 1972-08-02 1973-08-02

Country Status (5)

Country Link
US (1) US3930748A (ja)
JP (1) JPS5434088B2 (ja)
FR (1) FR2195256A5 (ja)
GB (1) GB1400285A (ja)
IT (1) IT992775B (ja)

Families Citing this family (42)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4162136A (en) * 1974-04-05 1979-07-24 Rolls-Royce Limited Cooled blade for a gas turbine engine
CH584347A5 (ja) * 1974-11-08 1977-01-31 Bbc Sulzer Turbomaschinen
US4153386A (en) * 1974-12-11 1979-05-08 United Technologies Corporation Air cooled turbine vanes
US4063851A (en) * 1975-12-22 1977-12-20 United Technologies Corporation Coolable turbine airfoil
GB1565361A (en) * 1976-01-29 1980-04-16 Rolls Royce Blade or vane for a gas turbine engien
US4118146A (en) * 1976-08-11 1978-10-03 United Technologies Corporation Coolable wall
JPS5390509A (en) * 1977-01-20 1978-08-09 Koukuu Uchiyuu Gijiyutsu Kenki Structure of air cooled turbine blade
US4286924A (en) * 1978-01-14 1981-09-01 Rolls-Royce Limited Rotor blade or stator vane for a gas turbine engine
US4257737A (en) * 1978-07-10 1981-03-24 United Technologies Corporation Cooled rotor blade
US4312624A (en) * 1980-11-10 1982-01-26 United Technologies Corporation Air cooled hollow vane construction
GB2163218B (en) * 1981-07-07 1986-07-16 Rolls Royce Cooled vane or blade for a gas turbine engine
GB2119028B (en) * 1982-04-27 1985-02-27 Rolls Royce Aerofoil for a gas turbine engine
US4601638A (en) * 1984-12-21 1986-07-22 United Technologies Corporation Airfoil trailing edge cooling arrangement
US4770608A (en) * 1985-12-23 1988-09-13 United Technologies Corporation Film cooled vanes and turbines
GB2189553B (en) * 1986-04-25 1990-05-23 Rolls Royce Cooled vane
JPH0663442B2 (ja) * 1989-09-04 1994-08-22 株式会社日立製作所 タービン翼
FR2798422B1 (fr) * 1990-01-24 2002-07-26 United Technologies Corp Pales refroidies pour moteur a turbine a gaz
GB2253443A (en) * 1991-03-05 1992-09-09 Rolls Royce Plc Gas turbine nozzle guide vane arrangement
US5328331A (en) * 1993-06-28 1994-07-12 General Electric Company Turbine airfoil with double shell outer wall
US5484258A (en) * 1994-03-01 1996-01-16 General Electric Company Turbine airfoil with convectively cooled double shell outer wall
US5516260A (en) * 1994-10-07 1996-05-14 General Electric Company Bonded turbine airfuel with floating wall cooling insert
US6283708B1 (en) 1999-12-03 2001-09-04 United Technologies Corporation Coolable vane or blade for a turbomachine
US6270317B1 (en) * 1999-12-18 2001-08-07 General Electric Company Turbine nozzle with sloped film cooling
US6742991B2 (en) * 2002-07-11 2004-06-01 Mitsubishi Heavy Industries, Ltd. Turbine blade and gas turbine
US7090461B2 (en) * 2003-10-30 2006-08-15 Siemens Westinghouse Power Corporation Gas turbine vane with integral cooling flow control system
EP2028344A1 (en) * 2007-08-21 2009-02-25 Siemens Aktiengesellschaft Transition duct
US8740567B2 (en) 2010-07-26 2014-06-03 United Technologies Corporation Reverse cavity blade for a gas turbine engine
US9353631B2 (en) * 2011-08-22 2016-05-31 United Technologies Corporation Gas turbine engine airfoil baffle
EP2628901A1 (en) * 2012-02-15 2013-08-21 Siemens Aktiengesellschaft Turbine blade with impingement cooling
CN104541024B (zh) * 2012-08-20 2018-09-28 安萨尔多能源英国知识产权有限公司 用于旋转机器的内部冷却式翼型件
WO2015012918A2 (en) * 2013-06-04 2015-01-29 United Technologies Corporation Gas turbine engine airfoil trailing edge suction side cooling
US9359902B2 (en) 2013-06-28 2016-06-07 Siemens Energy, Inc. Turbine airfoil with ambient cooling system
EP3049625A4 (en) * 2013-09-18 2017-07-19 United Technologies Corporation Manufacturing method for a baffle-containing blade
US10030524B2 (en) 2013-12-20 2018-07-24 Rolls-Royce Corporation Machined film holes
WO2017039572A1 (en) * 2015-08-28 2017-03-09 Siemens Aktiengesellschaft Turbine airfoil having flow displacement feature with partially sealed radial passages
US10655477B2 (en) * 2016-07-26 2020-05-19 General Electric Company Turbine components and method for forming turbine components
US10260363B2 (en) 2016-12-08 2019-04-16 General Electric Company Additive manufactured seal for insert compartmentalization
US10669861B2 (en) * 2017-02-15 2020-06-02 Raytheon Technologies Corporation Airfoil cooling structure
US10837293B2 (en) 2018-07-19 2020-11-17 General Electric Company Airfoil with tunable cooling configuration
US11078844B2 (en) * 2018-11-21 2021-08-03 Raytheon Technologies Corporation Thermal gradient reducing device for gas turbine engine component
US11242760B2 (en) * 2020-01-22 2022-02-08 General Electric Company Turbine rotor blade with integral impingement sleeve by additive manufacture
US11203981B1 (en) 2020-08-06 2021-12-21 Raytheon Technologies Corporation Baffle systems for airfoils

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2787441A (en) * 1952-03-05 1957-04-02 Thompson Prod Inc Hollow turbine bucket
US2873944A (en) * 1952-09-10 1959-02-17 Gen Motors Corp Turbine blade cooling
DE1070446B (de) * 1956-11-01 1959-12-03 The De Havilland Engine Company Limited, Leavesden, Hertfordshire (Großbritannien) Hohle Turbinenoder Kompressorschaufel
US2923525A (en) * 1958-04-04 1960-02-02 Orenda Engines Ltd Hollow gas turbine blade
US3240468A (en) * 1964-12-28 1966-03-15 Curtiss Wright Corp Transpiration cooled blades for turbines, compressors, and the like
US3433015A (en) * 1965-06-23 1969-03-18 Nasa Gas turbine combustion apparatus
US3388888A (en) * 1966-09-14 1968-06-18 Gen Electric Cooled turbine nozzle for high temperature turbine
US3574481A (en) * 1968-05-09 1971-04-13 James A Pyne Jr Variable area cooled airfoil construction for gas turbines
US3700348A (en) * 1968-08-13 1972-10-24 Gen Electric Turbomachinery blade structure
FR2023239A1 (ja) * 1968-11-14 1970-08-07 Mtu Muenchen Gmbh
US3628885A (en) * 1969-10-01 1971-12-21 Gen Electric Fluid-cooled airfoil
BE755567A (fr) * 1969-12-01 1971-02-15 Gen Electric Structure d'aube fixe, pour moteur a turbines a gaz et arrangement de reglage de temperature associe
US3635587A (en) * 1970-06-02 1972-01-18 Gen Motors Corp Blade cooling liner
US3644060A (en) * 1970-06-05 1972-02-22 John K Bryan Cooled airfoil
GB1355558A (en) * 1971-07-02 1974-06-05 Rolls Royce Cooled vane or blade for a gas turbine engine
GB1361256A (en) * 1971-08-25 1974-07-24 Rolls Royce Gas turbine engine blades
US3806276A (en) * 1972-08-30 1974-04-23 Gen Motors Corp Cooled turbine blade

Also Published As

Publication number Publication date
DE2338841B2 (de) 1975-07-10
DE2338841A1 (de) 1974-04-11
GB1400285A (en) 1975-07-16
US3930748A (en) 1976-01-06
FR2195256A5 (ja) 1974-03-01
JPS4985410A (ja) 1974-08-16
IT992775B (it) 1975-09-30

Similar Documents

Publication Publication Date Title
FR2195256A5 (ja)
JPS49133761A (ja)
CS177101B2 (ja)
JPS4892245A (ja)
JPS4912965A (ja)
FR2206133B1 (ja)
JPS5210466Y2 (ja)
JPS48100633A (ja)
JPS4934586U (ja)
JPS4938552A (ja)
FR2174767B1 (ja)
JPS5214632Y2 (ja)
JPS515478Y2 (ja)
JPS492117U (ja)
JPS4969143A (ja)
JPS4991286U (ja)
CS159686B1 (ja)
CS162474B1 (ja)
CS175598B1 (ja)
CH559931B5 (ja)
CH578053A5 (ja)
SE351857B (ja)
CH569816A5 (ja)
CH564357A5 (ja)
CH569990A5 (ja)