FR3047519B1 - Systeme de mise en rotation d'une soufflante d'un turboreacteur - Google Patents

Systeme de mise en rotation d'une soufflante d'un turboreacteur Download PDF

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Publication number
FR3047519B1
FR3047519B1 FR1650970A FR1650970A FR3047519B1 FR 3047519 B1 FR3047519 B1 FR 3047519B1 FR 1650970 A FR1650970 A FR 1650970A FR 1650970 A FR1650970 A FR 1650970A FR 3047519 B1 FR3047519 B1 FR 3047519B1
Authority
FR
France
Prior art keywords
turboreactor
blower
rotating
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
FR1650970A
Other languages
English (en)
Other versions
FR3047519A1 (fr
Inventor
Guillaume Patrice KUBIAK
Edouard Romain Bordoni Nils
Gilbert Roland Brault Michel
Guillaume Cuvillier Romain
Jean Henri Gomanne Benoit
Nicolas Negri Arnaud
Xavier Trappier Nicolas
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
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 Safran Aircraft Engines SAS, SNECMA SAS filed Critical Safran Aircraft Engines SAS
Priority to FR1650970A priority Critical patent/FR3047519B1/fr
Priority to PCT/FR2017/050287 priority patent/WO2017137701A1/fr
Priority to US16/076,294 priority patent/US10859000B2/en
Priority to GB1813813.1A priority patent/GB2563352A/en
Publication of FR3047519A1 publication Critical patent/FR3047519A1/fr
Application granted granted Critical
Publication of FR3047519B1 publication Critical patent/FR3047519B1/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
    • F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • 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
    • F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
    • F01D5/3007—Fixing blades to rotors; Blade roots ; Blade spacers of axial insertion type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C1/00—Flexible shafts; Mechanical means for transmitting movement in a flexible sheathing
    • F16C1/02—Flexible shafts; Mechanical means for transmitting movement in a flexible sheathing for conveying rotary movements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H1/00—Toothed gearings for conveying rotary motion
    • F16H1/28—Toothed gearings for conveying rotary motion with gears having orbital motion
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H57/00—General details of gearing
    • F16H57/08—General details of gearing of gearings with members having orbital motion
    • F16H57/082—Planet carriers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D15/00—Transmission of mechanical power
    • 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
    • F05D2240/60—Shafts
    • F05D2240/62—Flexible
    • 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
    • F05D2260/40—Transmission of power
    • F05D2260/403—Transmission of power through the shape of the drive components
    • F05D2260/4031—Transmission of power through the shape of the drive components as in toothed gearing
    • F05D2260/40311—Transmission of power through the shape of the drive components as in toothed gearing of the epicyclical, planetary or differential type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H57/00—General details of gearing
    • F16H57/02—Gearboxes; Mounting gearing therein
    • F16H2057/02039—Gearboxes for particular applications
    • F16H2057/02078—Gearboxes for particular applications for wind turbines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16H—GEARING
    • F16H57/00—General details of gearing
    • F16H57/02—Gearboxes; Mounting gearing therein
    • F16H57/031—Gearboxes; Mounting gearing therein characterised by covers or lids for gearboxes
    • 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)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Health & Medical Sciences (AREA)
  • Oral & Maxillofacial Surgery (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1650970A 2016-02-08 2016-02-08 Systeme de mise en rotation d'une soufflante d'un turboreacteur Active FR3047519B1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
FR1650970A FR3047519B1 (fr) 2016-02-08 2016-02-08 Systeme de mise en rotation d'une soufflante d'un turboreacteur
PCT/FR2017/050287 WO2017137701A1 (fr) 2016-02-08 2017-02-08 Systeme de mise en rotation d'une soufflante d'un turboreacteur
US16/076,294 US10859000B2 (en) 2016-02-08 2017-02-08 System for rotating a fan of a turbojet engine
GB1813813.1A GB2563352A (en) 2016-02-08 2017-02-08 System for rotating a fan of a turbojet engine

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1650970 2016-02-08
FR1650970A FR3047519B1 (fr) 2016-02-08 2016-02-08 Systeme de mise en rotation d'une soufflante d'un turboreacteur

Publications (2)

Publication Number Publication Date
FR3047519A1 FR3047519A1 (fr) 2017-08-11
FR3047519B1 true FR3047519B1 (fr) 2018-01-19

Family

ID=55650562

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1650970A Active FR3047519B1 (fr) 2016-02-08 2016-02-08 Systeme de mise en rotation d'une soufflante d'un turboreacteur

Country Status (4)

Country Link
US (1) US10859000B2 (fr)
FR (1) FR3047519B1 (fr)
GB (1) GB2563352A (fr)
WO (1) WO2017137701A1 (fr)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US10641111B2 (en) * 2018-08-31 2020-05-05 Rolls-Royce Corporation Turbine blade assembly with ceramic matrix composite components
CN114810348A (zh) * 2021-01-19 2022-07-29 中国航发商用航空发动机有限责任公司 传动机构、涡轮风扇发动机、装配方法

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1575659B1 (de) * 1967-06-06 1971-07-01 Stoeckicht Alexander W Stirnzahnrad mit doppelschraegverzahnung
GB2195712B (en) * 1986-10-08 1990-08-29 Rolls Royce Plc A turbofan gas turbine engine
GB2209575A (en) * 1987-09-05 1989-05-17 Rolls Royce Plc A gearbox arrangement for driving contra-rotating multi-bladed rotors
DE19510499A1 (de) * 1995-03-23 1996-09-26 Zahnradfabrik Friedrichshafen Planetengetriebe
US7721526B2 (en) * 2006-06-28 2010-05-25 Ishikawajima-Harima Heavy Industries Co., Ltd. Turbofan engine
US8104265B2 (en) * 2007-06-28 2012-01-31 United Technologies Corporation Gas turbines with multiple gas flow paths
US9359960B2 (en) * 2007-06-28 2016-06-07 United Technologies Corporation Gas turbines with multiple gas flow paths
US8834315B2 (en) * 2008-10-12 2014-09-16 Christopher C. Sappenfield Rotary units, rotary mechanisms, and related applications
FR2972765B1 (fr) * 2011-03-17 2013-04-05 Messier Dowty Procede d'optimisation de vitesse de soufflante de turboreacteur double-corps et architecture de mise en oeuvre.
US9133729B1 (en) * 2011-06-08 2015-09-15 United Technologies Corporation Flexible support structure for a geared architecture gas turbine engine
US8756908B2 (en) * 2012-05-31 2014-06-24 United Technologies Corporation Fundamental gear system architecture
EP2971600B1 (fr) * 2013-03-13 2019-07-03 United Technologies Corporation Architecture à engrenage pour protéger un matériel essentiel lors d'une sortie de pale de soufflante
WO2014204542A2 (fr) * 2013-04-01 2014-12-24 United Technologies Corporation Aube légère destinée à un moteur à turbine à gaz
FR3005453B1 (fr) * 2013-05-13 2016-10-07 Airbus Operations Sas Nacelle de turboreacteur d'aeronef
US8869504B1 (en) * 2013-11-22 2014-10-28 United Technologies Corporation Geared turbofan engine gearbox arrangement
US10378440B2 (en) * 2013-12-20 2019-08-13 United Technologies Corporation Geared turbofan with improved gear system maintainability

Also Published As

Publication number Publication date
US20190153958A1 (en) 2019-05-23
US10859000B2 (en) 2020-12-08
FR3047519A1 (fr) 2017-08-11
GB2563352A (en) 2018-12-12
WO2017137701A1 (fr) 2017-08-17
GB201813813D0 (en) 2018-10-10

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