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FR2223549B1 - - Google Patents

Info

Publication number
FR2223549B1
FR2223549B1 FR7410763A FR7410763A FR2223549B1 FR 2223549 B1 FR2223549 B1 FR 2223549B1 FR 7410763 A FR7410763 A FR 7410763A FR 7410763 A FR7410763 A FR 7410763A FR 2223549 B1 FR2223549 B1 FR 2223549B1
Authority
FR
France
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
FR7410763A
Other languages
French (fr)
Other versions
FR2223549A1 (en
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
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 by General Electric Co filed Critical General Electric Co
Publication of FR2223549A1 publication Critical patent/FR2223549A1/fr
Application granted granted Critical
Publication of FR2223549B1 publication Critical patent/FR2223549B1/fr
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
    • F01D5/185—Liquid cooling
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2240/00—Components
    • F05D2240/80—Platforms for stationary or moving blades
    • F05D2240/81—Cooled platforms

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR7410763A 1973-03-28 1974-03-28 Expired FR2223549B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US00345538A US3849025A (en) 1973-03-28 1973-03-28 Serpentine cooling channel construction for open-circuit liquid cooled turbine buckets

Publications (2)

Publication Number Publication Date
FR2223549A1 FR2223549A1 (en) 1974-10-25
FR2223549B1 true FR2223549B1 (en) 1979-10-12

Family

ID=23355426

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7410763A Expired FR2223549B1 (en) 1973-03-28 1974-03-28

Country Status (8)

Country Link
US (1) US3849025A (en)
JP (1) JPS5025914A (en)
CA (1) CA994245A (en)
DE (1) DE2414397A1 (en)
FR (1) FR2223549B1 (en)
GB (1) GB1470322A (en)
IT (1) IT1005870B (en)
NL (1) NL7404171A (en)

Families Citing this family (45)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5244994U (en) * 1975-09-26 1977-03-30
US4017210A (en) * 1976-02-19 1977-04-12 General Electric Company Liquid-cooled turbine bucket with integral distribution and metering system
US4156582A (en) * 1976-12-13 1979-05-29 General Electric Company Liquid cooled gas turbine buckets
US4118145A (en) * 1977-03-02 1978-10-03 Westinghouse Electric Corp. Water-cooled turbine blade
JPS5477820A (en) * 1977-12-02 1979-06-21 Hitachi Ltd Method of cooling gas turbine blade
US4275990A (en) * 1977-12-17 1981-06-30 Rolls-Royce Limited Disc channel for cooling rotor blade roots
US4260336A (en) * 1978-12-21 1981-04-07 United Technologies Corporation Coolant flow control apparatus for rotating heat exchangers with supercritical fluids
US4565490A (en) * 1981-06-17 1986-01-21 Rice Ivan G Integrated gas/steam nozzle
US4543781A (en) * 1981-06-17 1985-10-01 Rice Ivan G Annular combustor for gas turbine
GB2163219B (en) * 1981-10-31 1986-08-13 Rolls Royce Cooled turbine blade
ES2122423T3 (en) * 1994-11-14 1998-12-16 Nippon Catalytic Chem Ind PROCEDURE FOR THE PRODUCTION OF ACRYLIC ACID.
US5611662A (en) * 1995-08-01 1997-03-18 General Electric Co. Impingement cooling for turbine stator vane trailing edge
DE19705442A1 (en) * 1997-02-13 1998-08-20 Bmw Rolls Royce Gmbh Turbine impeller disk with cooling air channels
DE19713268B4 (en) * 1997-03-29 2006-01-19 Alstom Chilled gas turbine blade
US5967752A (en) * 1997-12-31 1999-10-19 General Electric Company Slant-tier turbine airfoil
US5971708A (en) * 1997-12-31 1999-10-26 General Electric Company Branch cooled turbine airfoil
DE69928073T2 (en) 1999-02-19 2006-07-20 Nippon Shokubai Co., Ltd. Process for the preparation of acrylic acid and process for the preparation of the catalyst
JP3943284B2 (en) 1999-05-27 2007-07-11 株式会社日本触媒 Acrylic acid production method
JP5134745B2 (en) 2001-09-19 2013-01-30 株式会社日本触媒 Acrylic acid production method
US6923362B2 (en) * 2002-09-30 2005-08-02 The Curators Of University Of Missouri Integral channels in metal components and fabrication thereof
JP4813758B2 (en) 2003-02-27 2011-11-09 株式会社日本触媒 Composite oxide catalyst and method for producing acrylic acid using the same
KR100497175B1 (en) 2003-03-26 2005-06-23 주식회사 엘지화학 Method for preparing catalysts for partial oxidation of propylene and iso-butylene
US6955525B2 (en) * 2003-08-08 2005-10-18 Siemens Westinghouse Power Corporation Cooling system for an outer wall of a turbine blade
US7217088B2 (en) * 2005-02-02 2007-05-15 Siemens Power Generation, Inc. Cooling fluid preheating system for an airfoil in a turbine engine
US7744347B2 (en) 2005-11-08 2010-06-29 United Technologies Corporation Peripheral microcircuit serpentine cooling for turbine airfoils
US8177506B2 (en) * 2006-01-25 2012-05-15 United Technologies Corporation Microcircuit cooling with an aspect ratio of unity
US7549843B2 (en) * 2006-08-24 2009-06-23 Siemens Energy, Inc. Turbine airfoil cooling system with axial flowing serpentine cooling chambers
US7722324B2 (en) * 2006-09-05 2010-05-25 United Technologies Corporation Multi-peripheral serpentine microcircuits for high aspect ratio blades
US8047788B1 (en) * 2007-10-19 2011-11-01 Florida Turbine Technologies, Inc. Turbine airfoil with near-wall serpentine cooling
US8118553B2 (en) * 2009-03-20 2012-02-21 Siemens Energy, Inc. Turbine airfoil cooling system with dual serpentine cooling chambers
US20110110772A1 (en) * 2009-11-11 2011-05-12 Arrell Douglas J Turbine Engine Components with Near Surface Cooling Channels and Methods of Making the Same
US8894352B2 (en) * 2010-09-07 2014-11-25 Siemens Energy, Inc. Ring segment with forked cooling passages
US9109454B2 (en) 2012-03-01 2015-08-18 General Electric Company Turbine bucket with pressure side cooling
US9562439B2 (en) * 2013-12-27 2017-02-07 General Electric Company Turbine nozzle and method for cooling a turbine nozzle of a gas turbine engine
US10301946B2 (en) 2016-10-26 2019-05-28 General Electric Company Partially wrapped trailing edge cooling circuits with pressure side impingements
US10450950B2 (en) 2016-10-26 2019-10-22 General Electric Company Turbomachine blade with trailing edge cooling circuit
US10273810B2 (en) 2016-10-26 2019-04-30 General Electric Company Partially wrapped trailing edge cooling circuit with pressure side serpentine cavities
US10233761B2 (en) 2016-10-26 2019-03-19 General Electric Company Turbine airfoil trailing edge coolant passage created by cover
US10352176B2 (en) * 2016-10-26 2019-07-16 General Electric Company Cooling circuits for a multi-wall blade
US10450875B2 (en) 2016-10-26 2019-10-22 General Electric Company Varying geometries for cooling circuits of turbine blades
US10598028B2 (en) 2016-10-26 2020-03-24 General Electric Company Edge coupon including cooling circuit for airfoil
US10309227B2 (en) 2016-10-26 2019-06-04 General Electric Company Multi-turn cooling circuits for turbine blades
US10465521B2 (en) 2016-10-26 2019-11-05 General Electric Company Turbine airfoil coolant passage created in cover
US11566527B2 (en) 2018-12-18 2023-01-31 General Electric Company Turbine engine airfoil and method of cooling
US11814965B2 (en) 2021-11-10 2023-11-14 General Electric Company Turbomachine blade trailing edge cooling circuit with turn passage having set of obstructions

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2888241A (en) * 1954-06-09 1959-05-26 Stalker Corp Fabricated cooled turbine blades
US2888243A (en) * 1956-10-22 1959-05-26 Pollock Robert Stephen Cooled turbine blade
US3220697A (en) * 1963-08-30 1965-11-30 Gen Electric Hollow turbine or compressor vane
US3370829A (en) * 1965-12-20 1968-02-27 Avco Corp Gas turbine blade construction
US3736071A (en) * 1970-11-27 1973-05-29 Gen Electric Bucket tip/collection slot combination for open-circuit liquid-cooled gas turbines
US3658439A (en) * 1970-11-27 1972-04-25 Gen Electric Metering of liquid coolant in open-circuit liquid-cooled gas turbines

Also Published As

Publication number Publication date
GB1470322A (en) 1977-04-14
NL7404171A (en) 1974-10-01
DE2414397A1 (en) 1974-10-17
US3849025A (en) 1974-11-19
CA994245A (en) 1976-08-03
IT1005870B (en) 1976-09-30
FR2223549A1 (en) 1974-10-25
JPS5025914A (en) 1975-03-18

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Legal Events

Date Code Title Description
ST Notification of lapse