FR2401320A1 - Perfectionnements au refroidissement des turbines a gaz - Google Patents

Perfectionnements au refroidissement des turbines a gaz

Info

Publication number
FR2401320A1
FR2401320A1 FR7726637A FR7726637A FR2401320A1 FR 2401320 A1 FR2401320 A1 FR 2401320A1 FR 7726637 A FR7726637 A FR 7726637A FR 7726637 A FR7726637 A FR 7726637A FR 2401320 A1 FR2401320 A1 FR 2401320A1
Authority
FR
France
Prior art keywords
gas turbine
perfections
air
turbine cooling
axis
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.)
Granted
Application number
FR7726637A
Other languages
English (en)
French (fr)
Other versions
FR2401320B1 (US06580902-20030617-M00005.png
Inventor
Michel Robert Ayache
Jean-Claude Lucien Delonge
Daniel Jean Marey
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA SAS
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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR7726637A priority Critical patent/FR2401320A1/fr
Priority to DE19782833220 priority patent/DE2833220A1/de
Priority to US05/929,910 priority patent/US4231704A/en
Priority to GB7831942A priority patent/GB2003230B/en
Publication of FR2401320A1 publication Critical patent/FR2401320A1/fr
Application granted granted Critical
Publication of FR2401320B1 publication Critical patent/FR2401320B1/fr
Granted legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • 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
    • F01D5/02—Blade-carrying members, e.g. rotors
    • F01D5/08—Heating, heat-insulating or cooling means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/26—Rotors specially for elastic fluids
    • F04D29/32—Rotors specially for elastic fluids for axial flow pumps
    • F04D29/321—Rotors specially for elastic fluids for axial flow pumps for axial flow compressors
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
    • F04D—NON-POSITIVE-DISPLACEMENT PUMPS
    • F04D29/00—Details, component parts, or accessories
    • F04D29/58—Cooling; Heating; Diminishing heat transfer
    • F04D29/582—Cooling; Heating; Diminishing heat transfer specially adapted for elastic fluid pumps
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
FR7726637A 1977-08-26 1977-08-26 Perfectionnements au refroidissement des turbines a gaz Granted FR2401320A1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR7726637A FR2401320A1 (fr) 1977-08-26 1977-08-26 Perfectionnements au refroidissement des turbines a gaz
DE19782833220 DE2833220A1 (de) 1977-08-26 1978-07-28 Vorrichtung zur kuehlung von gasturbinen
US05/929,910 US4231704A (en) 1977-08-26 1978-08-01 Cooling fluid bleed for axis of turbine rotor
GB7831942A GB2003230B (en) 1977-08-26 1978-08-02 Axial flow compressor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7726637A FR2401320A1 (fr) 1977-08-26 1977-08-26 Perfectionnements au refroidissement des turbines a gaz

Publications (2)

Publication Number Publication Date
FR2401320A1 true FR2401320A1 (fr) 1979-03-23
FR2401320B1 FR2401320B1 (US06580902-20030617-M00005.png) 1982-04-30

Family

ID=9194968

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7726637A Granted FR2401320A1 (fr) 1977-08-26 1977-08-26 Perfectionnements au refroidissement des turbines a gaz

Country Status (4)

Country Link
US (1) US4231704A (US06580902-20030617-M00005.png)
DE (1) DE2833220A1 (US06580902-20030617-M00005.png)
FR (1) FR2401320A1 (US06580902-20030617-M00005.png)
GB (1) GB2003230B (US06580902-20030617-M00005.png)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2552817A1 (fr) * 1978-11-27 1985-04-05 Snecma Perfectionnements au refroidissement des rotors de turbines
FR2609500A1 (fr) * 1987-01-14 1988-07-15 Snecma Disque de compresseur de turbomachine avec accelerateur centripete pour l'aspiration d'air de refroidissement de la turbine
FR2672943A1 (fr) * 1991-02-20 1992-08-21 Snecma Compresseur de turbomachine equipe d'un dispositif de prelevement d'air.
FR2732405A1 (fr) * 1982-03-23 1996-10-04 Snecma Dispositif pour refroidir le rotor d'une turbine a gaz
EP2412924A3 (en) * 2010-07-28 2015-08-05 United Technologies Corporation A disk spacer for a gas engine turbine and a method for providing a rotor assembly

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3037020C2 (de) * 1980-10-01 1983-11-03 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Gasturbinenstrahltriebwerk in Mehrwellen-Bauweise mit Verdichterhochdruckluftentnahme- und -führungseinrichtungen zur Turbinenkühlung
FR2491549B1 (fr) * 1980-10-08 1985-07-05 Snecma Dispositif de refroidissement d'une turbine a gaz, par prelevement d'air au niveau du compresseur
GB2207465B (en) * 1987-07-18 1992-02-19 Rolls Royce Plc A compressor and air bleed arrangement
US5232339A (en) * 1992-01-28 1993-08-03 General Electric Company Finned structural disk spacer arm
FR2930588B1 (fr) 2008-04-24 2010-06-04 Snecma Rotor de compresseur d'une turbomachine comportant des moyens de prelevement d'air centripete
US20130017092A1 (en) * 2011-07-11 2013-01-17 General Electric Company Rotor assembly for gas turbines
US9145772B2 (en) 2012-01-31 2015-09-29 United Technologies Corporation Compressor disk bleed air scallops
US9091173B2 (en) 2012-05-31 2015-07-28 United Technologies Corporation Turbine coolant supply system
US9657746B2 (en) * 2014-08-29 2017-05-23 Pratt & Whitney Canada Corp. Compressor rotor with anti-vortex fins
US10982595B2 (en) 2016-08-23 2021-04-20 Raytheon Technologies Corporation Heat exchanger for gas turbine engine mounted in intermediate case
KR101896436B1 (ko) * 2017-04-12 2018-09-10 두산중공업 주식회사 보강디스크를 포함하는 압축기 및 이를 포함하는 가스터빈
CN114033744B (zh) * 2022-01-11 2022-03-25 成都中科翼能科技有限公司 一种新型燃气轮机低压压气机转子结构及装配方法

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR966804A (fr) * 1947-03-11 1950-10-19 Rolls Royce Perfectionnements aux moteurs à turbine à gaz
US2618433A (en) * 1948-06-23 1952-11-18 Curtiss Wright Corp Means for bleeding air from compressors
GB712051A (en) * 1951-10-10 1954-07-14 Rolls Royce Improvements in or relating to axial-flow fluid machines
CH366424A (de) * 1958-07-25 1962-12-31 Gen Electric Einrichtung zur Kühlung rotierender Teile einer mehrstufigen Turbine für heisses Medium
US3085400A (en) * 1959-03-23 1963-04-16 Gen Electric Cooling fluid impeller for elastic fluid turbines
US3647313A (en) * 1970-06-01 1972-03-07 Gen Electric Gas turbine engines with compressor rotor cooling
US3742706A (en) * 1971-12-20 1973-07-03 Gen Electric Dual flow cooled turbine arrangement for gas turbine engines
US3897168A (en) * 1974-03-05 1975-07-29 Westinghouse Electric Corp Turbomachine extraction flow guide vanes
US4008977A (en) * 1975-09-19 1977-02-22 United Technologies Corporation Compressor bleed system

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2552817A1 (fr) * 1978-11-27 1985-04-05 Snecma Perfectionnements au refroidissement des rotors de turbines
DE2947521A1 (de) * 1978-11-27 1986-06-26 Snecma Turbinenscheibe mit kanaelen zum durchtritt eines kuehlfluids
DE2947521C2 (US06580902-20030617-M00005.png) * 1978-11-27 1991-03-28 Societe Nationale D'etude Et De Construction De Moteurs D'aviation (S.N.E.C.M.A.), Paris, Fr
FR2732405A1 (fr) * 1982-03-23 1996-10-04 Snecma Dispositif pour refroidir le rotor d'une turbine a gaz
FR2609500A1 (fr) * 1987-01-14 1988-07-15 Snecma Disque de compresseur de turbomachine avec accelerateur centripete pour l'aspiration d'air de refroidissement de la turbine
EP0277853A1 (fr) * 1987-01-14 1988-08-10 Societe Nationale D'etude Et De Construction De Moteurs D'aviation, "S.N.E.C.M.A." Disque de compresseur de turbomachine avec accélérateur centripète pour l'aspiration d'air de refroidissement de la turbine
US4787820A (en) * 1987-01-14 1988-11-29 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "S.N.E.C.M.A." Turbine plant compressor disc with centripetal accelerator for the induction of turbine cooling air
FR2672943A1 (fr) * 1991-02-20 1992-08-21 Snecma Compresseur de turbomachine equipe d'un dispositif de prelevement d'air.
EP2412924A3 (en) * 2010-07-28 2015-08-05 United Technologies Corporation A disk spacer for a gas engine turbine and a method for providing a rotor assembly

Also Published As

Publication number Publication date
GB2003230B (en) 1982-01-20
DE2833220A1 (de) 1979-03-01
US4231704A (en) 1980-11-04
DE2833220C2 (US06580902-20030617-M00005.png) 1988-06-09
FR2401320B1 (US06580902-20030617-M00005.png) 1982-04-30
GB2003230A (en) 1979-03-07

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Legal Events

Date Code Title Description
CL Concession to grant licences
ST Notification of lapse