FR3025835B1 - Systeme de circulation d'air de refroidissement d'aubes de turbine de turbomachine - Google Patents

Systeme de circulation d'air de refroidissement d'aubes de turbine de turbomachine Download PDF

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Publication number
FR3025835B1
FR3025835B1 FR1458695A FR1458695A FR3025835B1 FR 3025835 B1 FR3025835 B1 FR 3025835B1 FR 1458695 A FR1458695 A FR 1458695A FR 1458695 A FR1458695 A FR 1458695A FR 3025835 B1 FR3025835 B1 FR 3025835B1
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FR
France
Prior art keywords
cooling air
air circulation
circulation system
duct
blade cooling
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.)
Active
Application number
FR1458695A
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English (en)
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FR3025835A1 (fr
Inventor
Francois Gallet
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
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Filing date
Publication date
Application filed by SNECMA SAS filed Critical SNECMA SAS
Priority to FR1458695A priority Critical patent/FR3025835B1/fr
Publication of FR3025835A1 publication Critical patent/FR3025835A1/fr
Application granted granted Critical
Publication of FR3025835B1 publication Critical patent/FR3025835B1/fr
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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
    • F02C7/22—Fuel supply systems
    • F02C7/224—Heating fuel before feeding to the burner
    • 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
    • F01D5/081—Cooling fluid being directed on the side of the rotor disc or at the roots of the blades
    • 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
    • F02C7/185—Cooling means for reducing the temperature of the cooling air or gas
    • 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
    • F05D2240/20—Rotors
    • F05D2240/24—Rotors for turbines
    • 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
    • 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
    • F05D2270/00—Control
    • F05D2270/30—Control parameters, e.g. input parameters
    • F05D2270/306—Mass flow
    • F05D2270/3062—Mass flow of the auxiliary fluid for heating or cooling purposes
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

L'objet principal de l'invention est un système (1) de circulation d'air de refroidissement (A1-A4) d'aubes (24a) de turbine (24) d'une turbomachine (10), caractérisé en ce qu'il comporte un conduit amont (2) de circulation d'air de refroidissement (A1) pour le prélèvement d'air de refroidissement (A1) depuis un compresseur (22) de la turbomachine (10), un conduit aval (3) de circulation d'air de refroidissement (A3) pour l'acheminement d'air de refroidissement (A4) vers les aubes (24a) de turbine (24), et un échangeur thermique (4) positionné entre le conduit amont (2) et le conduit aval (3) pour refroidir l'air de refroidissement (A1) prélevé depuis le compresseur (22) avant son acheminement vers les aubes (24a) de turbine (24) par l'intermédiaire du conduit aval (3).
FR1458695A 2014-09-16 2014-09-16 Systeme de circulation d'air de refroidissement d'aubes de turbine de turbomachine Active FR3025835B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1458695A FR3025835B1 (fr) 2014-09-16 2014-09-16 Systeme de circulation d'air de refroidissement d'aubes de turbine de turbomachine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1458695A FR3025835B1 (fr) 2014-09-16 2014-09-16 Systeme de circulation d'air de refroidissement d'aubes de turbine de turbomachine

Publications (2)

Publication Number Publication Date
FR3025835A1 FR3025835A1 (fr) 2016-03-18
FR3025835B1 true FR3025835B1 (fr) 2020-08-14

Family

ID=52465463

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1458695A Active FR3025835B1 (fr) 2014-09-16 2014-09-16 Systeme de circulation d'air de refroidissement d'aubes de turbine de turbomachine

Country Status (1)

Country Link
FR (1) FR3025835B1 (fr)

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2656657A1 (fr) * 1989-12-28 1991-07-05 Snecma Turbomachine refroidie par air et procede de refroidissement de cette turbomachine.
US6672072B1 (en) * 1998-08-17 2004-01-06 General Electric Company Pressure boosted compressor cooling system
US6250061B1 (en) * 1999-03-02 2001-06-26 General Electric Company Compressor system and methods for reducing cooling airflow
US6968696B2 (en) * 2003-09-04 2005-11-29 Siemens Westinghouse Power Corporation Part load blade tip clearance control
GB201121428D0 (en) * 2011-12-14 2012-01-25 Rolls Royce Plc Controller

Also Published As

Publication number Publication date
FR3025835A1 (fr) 2016-03-18

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