FR3062972B1 - Dispositif de generation d'energie electrique auxiliaire et turbomachine comportant un tel dispositif - Google Patents

Dispositif de generation d'energie electrique auxiliaire et turbomachine comportant un tel dispositif Download PDF

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Publication number
FR3062972B1
FR3062972B1 FR1751130A FR1751130A FR3062972B1 FR 3062972 B1 FR3062972 B1 FR 3062972B1 FR 1751130 A FR1751130 A FR 1751130A FR 1751130 A FR1751130 A FR 1751130A FR 3062972 B1 FR3062972 B1 FR 3062972B1
Authority
FR
France
Prior art keywords
turbomachine
electrical energy
auxiliary electrical
drive shaft
coupled
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
FR1751130A
Other languages
English (en)
Other versions
FR3062972A1 (fr
Inventor
Michael Alain Eric Sauve
Mohamed-Lamine Boutaleb
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
Safran Aircraft Engines 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 Safran Aircraft Engines SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1751130A priority Critical patent/FR3062972B1/fr
Publication of FR3062972A1 publication Critical patent/FR3062972A1/fr
Application granted granted Critical
Publication of FR3062972B1 publication Critical patent/FR3062972B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • 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
    • F02C7/14—Cooling of plants of fluids in the plant, e.g. lubricant or fuel
    • 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
    • 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
    • F02C7/26—Starting; Ignition
    • F02C7/268—Starting drives for the rotor, acting directly on the rotor of the gas turbine to be started
    • F02C7/275—Mechanical drives
    • 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
    • F05D2220/00—Application
    • F05D2220/70—Application in combination with
    • F05D2220/76—Application in combination with an electrical generator
    • 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
    • F05D2260/213—Heat transfer, e.g. cooling by the provision of a heat exchanger within the cooling circuit
    • 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)
  • Connection Of Motors, Electrical Generators, Mechanical Devices, And The Like (AREA)

Abstract

Dispositif de génération d’énergie électrique auxiliaire et turbomachine comportant un tel dispositif. Un dispositif de génération d’énergie électrique auxiliaire (20) destiné à être couplé à un arbre moteur (2) d’une turbomachine (1) dotée d’une veine primaire (11) et d’une veine secondaire (12), le dispositif (20) comprenant un arbre radial de transmission (23) apte à être couplé à l’arbre moteur (2) de ladite turbomachine (1), une boîte de transmission (24) mécaniquement couplée en entrée à l’arbre radial (23), un générateur électrique (21) entraîné par un arbre d’entraînement (25) mécaniquement couplé en sortie de la boîte de transmission (24). Le dispositif comprend un compresseur (22) configuré pour refroidir le générateur électrique (21) à l’aide d’un flux d’air de refroidissement en prélevant et compressant une portion du flux d’air circulant dans la veine secondaire (12) de ladite turbomachine (1) dans laquelle le dispositif (20) est destiné à être monté. Figure pour l’abrégé : Fig. 1
FR1751130A 2017-02-10 2017-02-10 Dispositif de generation d'energie electrique auxiliaire et turbomachine comportant un tel dispositif Active FR3062972B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1751130A FR3062972B1 (fr) 2017-02-10 2017-02-10 Dispositif de generation d'energie electrique auxiliaire et turbomachine comportant un tel dispositif

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1751130A FR3062972B1 (fr) 2017-02-10 2017-02-10 Dispositif de generation d'energie electrique auxiliaire et turbomachine comportant un tel dispositif
FR1751130 2017-02-10

Publications (2)

Publication Number Publication Date
FR3062972A1 FR3062972A1 (fr) 2018-08-17
FR3062972B1 true FR3062972B1 (fr) 2021-06-11

Family

ID=58632467

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1751130A Active FR3062972B1 (fr) 2017-02-10 2017-02-10 Dispositif de generation d'energie electrique auxiliaire et turbomachine comportant un tel dispositif

Country Status (1)

Country Link
FR (1) FR3062972B1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3128734A1 (fr) 2021-10-28 2023-05-05 Safran Aircraft Engines Intégration de génératrices dans un flux d’air de réacteur d’avion

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2960592B1 (fr) * 2010-05-27 2016-02-26 Snecma Procede de demarrage d'un moteur d'aeronef
EP2594766B1 (fr) * 2011-11-18 2014-06-18 Hamilton Sundstrand Corporation Turbine à gaz comprenant alternateur à aimant permanent avec ventilateur de refroidissement intégré
GB201311072D0 (en) * 2013-06-21 2013-08-07 Rolls Royce Deutschland & Co Kg An accessory mounting for a gas turbine engine

Also Published As

Publication number Publication date
FR3062972A1 (fr) 2018-08-17

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