FR2564896B1 - VANE OF GAS TURBINE ENGINE. - Google Patents

VANE OF GAS TURBINE ENGINE.

Info

Publication number
FR2564896B1
FR2564896B1 FR858507928A FR8507928A FR2564896B1 FR 2564896 B1 FR2564896 B1 FR 2564896B1 FR 858507928 A FR858507928 A FR 858507928A FR 8507928 A FR8507928 A FR 8507928A FR 2564896 B1 FR2564896 B1 FR 2564896B1
Authority
FR
France
Prior art keywords
vane
gas turbine
turbine engine
engine
gas
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
FR858507928A
Other languages
French (fr)
Other versions
FR2564896A1 (en
Inventor
Don Butts
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 FR2564896A1 publication Critical patent/FR2564896A1/en
Application granted granted Critical
Publication of FR2564896B1 publication Critical patent/FR2564896B1/en
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
    • 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
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/221—Improvement of heat transfer
    • F05D2260/2212—Improvement of heat transfer by creating turbulence
    • 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
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/221—Improvement of heat transfer
    • F05D2260/2214—Improvement of heat transfer by increasing the heat transfer surface
    • F05D2260/22141—Improvement of heat transfer by increasing the heat transfer surface using fins or ribs

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR858507928A 1984-05-24 1985-05-24 VANE OF GAS TURBINE ENGINE. Expired FR2564896B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US61354384A 1984-05-24 1984-05-24

Publications (2)

Publication Number Publication Date
FR2564896A1 FR2564896A1 (en) 1985-11-29
FR2564896B1 true FR2564896B1 (en) 1989-04-21

Family

ID=24457714

Family Applications (1)

Application Number Title Priority Date Filing Date
FR858507928A Expired FR2564896B1 (en) 1984-05-24 1985-05-24 VANE OF GAS TURBINE ENGINE.

Country Status (7)

Country Link
JP (1) JPS611805A (en)
CA (1) CA1211052A (en)
DE (1) DE3518314A1 (en)
FR (1) FR2564896B1 (en)
GB (1) GB2159585B (en)
IT (1) IT1183653B (en)
SE (1) SE468358B (en)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2672003B1 (en) * 1991-01-30 1993-04-09 Snecma PROCESS FOR PRODUCING COMPLEX CERAMIC CORES FOR FOUNDRY.
FR2672338B1 (en) * 1991-02-06 1993-04-16 Snecma TURBINE BLADE PROVIDED WITH A COOLING SYSTEM.
JP3006174B2 (en) * 1991-07-04 2000-02-07 株式会社日立製作所 Member having a cooling passage inside
US5288207A (en) * 1992-11-24 1994-02-22 United Technologies Corporation Internally cooled turbine airfoil
US5368441A (en) * 1992-11-24 1994-11-29 United Technologies Corporation Turbine airfoil including diffusing trailing edge pedestals
US5431537A (en) * 1994-04-19 1995-07-11 United Technologies Corporation Cooled gas turbine blade
US5759012A (en) * 1996-12-13 1998-06-02 Caterpillar Inc. Turbine disc ingress prevention method and apparatus
DE59709195D1 (en) * 1997-07-14 2003-02-27 Alstom Switzerland Ltd Cooling system for the leading edge area of a hollow gas turbine blade
DE19846332A1 (en) 1998-10-08 2000-04-13 Asea Brown Boveri Cooling channel of a thermally highly stressed component
IT1319140B1 (en) * 2000-11-28 2003-09-23 Nuovo Pignone Spa REFRIGERATION SYSTEM FOR STATIC GAS TURBINE NOZZLES
DE10248548A1 (en) * 2002-10-18 2004-04-29 Alstom (Switzerland) Ltd. Coolable component
US6884036B2 (en) * 2003-04-15 2005-04-26 General Electric Company Complementary cooled turbine nozzle
US6997675B2 (en) * 2004-02-09 2006-02-14 United Technologies Corporation Turbulated hole configurations for turbine blades
US7114916B2 (en) * 2004-02-09 2006-10-03 United Technologies Corporation Tailored turbulation for turbine blades
US7207775B2 (en) * 2004-06-03 2007-04-24 General Electric Company Turbine bucket with optimized cooling circuit
DE102005012803A1 (en) * 2005-03-19 2006-09-21 Alstom Technology Ltd. Rotor blade for gas turbine stage, has whirling effect producing structures, which are formed as elevated sections on inner wall surfaces of coolant duct and enclose narrow gap, where duct is defined by side walls of blade sheet
FR2900850B1 (en) * 2006-05-10 2009-02-06 Snecma Sa PROCESS FOR MANUFACTURING CERAMIC FOUNDRY CORES FOR TURBOMACHINE BLADES
US20070297916A1 (en) * 2006-06-22 2007-12-27 United Technologies Corporation Leading edge cooling using wrapped staggered-chevron trip strips
GB0813839D0 (en) * 2008-07-30 2008-09-03 Rolls Royce Plc An aerofoil and method for making an aerofoil
RU2691867C1 (en) * 2018-07-05 2019-06-18 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Method for cooling turbine blade of low-pressure turbine (lpt) of gas turbine engine and rotor blade of lpt, cooled by this method
RU2691868C1 (en) * 2018-07-05 2019-06-18 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") High-pressure turbine rotor of a gas turbine engine (versions)
RU2684298C1 (en) * 2018-07-05 2019-04-05 Публичное акционерное общество "ОДК-Уфимское моторостроительное производственное объединение" (ПАО "ОДК-УМПО") Method of cooling the rotor of a high pressure turbine (hpt) of gas turbine engine (gte), hpt rotor and hpt rotor blade cooled by this method, knot of the device of twisting of air of hpt rotor

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1374159A (en) * 1962-12-05 1964-10-02 Gen Motors Corp Turbine blade
FR1405746A (en) * 1963-08-30 1965-07-09 Gen Electric Hollow blade for turbine or compressor
US3628885A (en) * 1969-10-01 1971-12-21 Gen Electric Fluid-cooled airfoil
GB1410014A (en) * 1971-12-14 1975-10-15 Rolls Royce Gas turbine engine blade
US4416585A (en) * 1980-01-17 1983-11-22 Pratt & Whitney Aircraft Of Canada Limited Blade cooling for gas turbine engine
US4775296A (en) * 1981-12-28 1988-10-04 United Technologies Corporation Coolable airfoil for a rotary machine
US4515526A (en) * 1981-12-28 1985-05-07 United Technologies Corporation Coolable airfoil for a rotary machine

Also Published As

Publication number Publication date
IT8520834A0 (en) 1985-05-22
JPS611805A (en) 1986-01-07
GB2159585A (en) 1985-12-04
SE8502495L (en) 1985-11-25
GB8511647D0 (en) 1985-06-12
IT1183653B (en) 1987-10-22
SE8502495D0 (en) 1985-05-21
DE3518314A1 (en) 1985-11-28
CA1211052A (en) 1986-09-09
FR2564896A1 (en) 1985-11-29
GB2159585B (en) 1989-02-08
SE468358B (en) 1992-12-21

Similar Documents

Publication Publication Date Title
FR2564896B1 (en) VANE OF GAS TURBINE ENGINE.
FR2617907B1 (en) GAS TURBINE ENGINE
GB2195712B (en) A turbofan gas turbine engine
GB2199375B (en) A turbofan gas turbine engine.
GB2206686B (en) Gas turbine engine augmentor
IT8423443A0 (en) COMBUSTION COMPLEX FOR GAS TURBINE ENGINE.
FR2592092B1 (en) COOLED VANE TURBINE ESPECIALLY FOR A GAS TURBINE ENGINE
DE3663847D1 (en) Combustor for gas turbine engine
FR2590933B1 (en) REFRIGERATED BLADE FOR A GAS TURBINE ENGINE
DE3669750D1 (en) GAS TURBINE COMBUSTION CHAMBER.
GB2221979B (en) A combustion chamber for a gas turbine engine
DE3665627D1 (en) Combustion liner for a gas turbine engine
GB8616153D0 (en) Turbofan gas turbine engine
FR2586453B1 (en) CARBURETOR FOR A GAS TURBINE ENGINE
FR2575221B1 (en) COOLABLE STATOR FOR A GAS TURBINE ENGINE
GB2072268B (en) Fuel efficiency of a gas turbine engine
DE68901320D1 (en) GAS TURBINE COMBUSTION CHAMBER.
FR2557212B1 (en) STATOR STRUCTURE FOR A GAS TURBINE ENGINE
NO151434C (en) Combustion chamber lining for a gas turbine engine
JPS57142422A (en) Combustor for gas turbine engine
GB2199900B (en) A turbopropeller or turbofan gas turbine engine
GB8527286D0 (en) Gas turbine engines
BR8202545A (en) FUEL CONTROL FOR GAS TURBINE ENGINES
FR2601068B1 (en) POWER TURBINE FOR A GAS TURBINE ENGINE.
IT9020544A0 (en) gas turbine engine