FR3003323B1 - Fixation d'une boite d'engrenages en v sur une turbomachine - Google Patents

Fixation d'une boite d'engrenages en v sur une turbomachine

Info

Publication number
FR3003323B1
FR3003323B1 FR1352284A FR1352284A FR3003323B1 FR 3003323 B1 FR3003323 B1 FR 3003323B1 FR 1352284 A FR1352284 A FR 1352284A FR 1352284 A FR1352284 A FR 1352284A FR 3003323 B1 FR3003323 B1 FR 3003323B1
Authority
FR
France
Prior art keywords
turbomachine
fixing
gear box
gear
box
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
FR1352284A
Other languages
English (en)
Other versions
FR3003323A1 (fr
Inventor
Bruno Albert Beutin
Carmen Ancuta
Lambert Olivier Marie Demoulin
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 FR1352284A priority Critical patent/FR3003323B1/fr
Priority to PCT/FR2014/050391 priority patent/WO2014140441A1/fr
Priority to US14/775,292 priority patent/US10054001B2/en
Publication of FR3003323A1 publication Critical patent/FR3003323A1/fr
Application granted granted Critical
Publication of FR3003323B1 publication Critical patent/FR3003323B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • F02C7/32—Arrangement, mounting, or driving, of auxiliaries
    • 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
    • F01D15/00—Adaptations of machines or engines for special use; Combinations of engines with devices driven thereby
    • F01D15/12—Combinations with mechanical gearing
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • 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
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/28—Supporting or mounting arrangements, e.g. for turbine casing
    • 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
    • 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
    • F16H57/025—Support of gearboxes, e.g. torque arms, or attachment to other devices
    • 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
    • F16H57/03—Gearboxes; Mounting gearing therein characterised by means for reinforcing gearboxes, e.g. ribs
    • 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
    • F05D2220/30—Application in 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
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/36—Application in turbines specially adapted for the fan of turbofan engines
    • 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
    • F05D2250/00—Geometry
    • F05D2250/30—Arrangement of components
    • F05D2250/38—Arrangement of components angled, e.g. sweep angle
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR1352284A 2013-03-14 2013-03-14 Fixation d'une boite d'engrenages en v sur une turbomachine Active FR3003323B1 (fr)

Priority Applications (3)

Application Number Priority Date Filing Date Title
FR1352284A FR3003323B1 (fr) 2013-03-14 2013-03-14 Fixation d'une boite d'engrenages en v sur une turbomachine
PCT/FR2014/050391 WO2014140441A1 (fr) 2013-03-14 2014-02-25 Boite d'engrenages en v pour entraînement d'équipements de turbomachine
US14/775,292 US10054001B2 (en) 2013-03-14 2014-02-25 V-shaped gearbox for driving turbomachine equipment

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1352284A FR3003323B1 (fr) 2013-03-14 2013-03-14 Fixation d'une boite d'engrenages en v sur une turbomachine

Publications (2)

Publication Number Publication Date
FR3003323A1 FR3003323A1 (fr) 2014-09-19
FR3003323B1 true FR3003323B1 (fr) 2016-10-07

Family

ID=48407727

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1352284A Active FR3003323B1 (fr) 2013-03-14 2013-03-14 Fixation d'une boite d'engrenages en v sur une turbomachine

Country Status (3)

Country Link
US (1) US10054001B2 (fr)
FR (1) FR3003323B1 (fr)
WO (1) WO2014140441A1 (fr)

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3014953B1 (fr) * 2013-12-12 2016-01-01 Snecma Turbomachine d'aeronef comportant un echangeur de chaleur et une boite d'engrenages en v
GB201417123D0 (en) * 2014-09-29 2014-11-12 Rolls Royce Plc Apparatus for mounting a component in a gas turbine engine
US20160169118A1 (en) * 2014-12-12 2016-06-16 United Technologies Corporation Dual tower shaft gearbox for gas turbine engine
US10883424B2 (en) 2016-07-19 2021-01-05 Pratt & Whitney Canada Corp. Multi-spool gas turbine engine architecture
US11415063B2 (en) 2016-09-15 2022-08-16 Pratt & Whitney Canada Corp. Reverse-flow gas turbine engine
US11035293B2 (en) 2016-09-15 2021-06-15 Pratt & Whitney Canada Corp. Reverse flow gas turbine engine with offset RGB
US10465611B2 (en) 2016-09-15 2019-11-05 Pratt & Whitney Canada Corp. Reverse flow multi-spool gas turbine engine with aft-end accessory gearbox drivingly connected to both high pressure spool and low pressure spool
US10815899B2 (en) 2016-11-15 2020-10-27 Pratt & Whitney Canada Corp. Gas turbine engine accessories arrangement
US10808624B2 (en) 2017-02-09 2020-10-20 Pratt & Whitney Canada Corp. Turbine rotor with low over-speed requirements
US20180230519A1 (en) * 2017-02-15 2018-08-16 OraVital Inc. Methods and kits for selecting treatment for oral infections
US10746188B2 (en) 2017-03-14 2020-08-18 Pratt & Whitney Canada Corp. Inter-shaft bearing connected to a compressor boost system
US10526976B2 (en) 2017-04-27 2020-01-07 United Technologies Corporation Tangential drive for gas turbine engine accessories
EP4339440A3 (fr) 2018-08-08 2024-05-22 Pratt & Whitney Canada Corp. Système et procédé multimoteur
US11674449B2 (en) * 2021-03-12 2023-06-13 Pratt & Whitney Canada Corp. Mount assembly for accessory gearbox of aircraft engine and associated method of assembly
US11674414B2 (en) 2021-03-19 2023-06-13 Pratt & Whitney Canada Corp. Gas turbine engine and mount assembly therefor

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4571936A (en) * 1985-07-10 1986-02-25 The United States Of America As Represented By The Secretary Of The Air Force Length adjustable strut link with low aerodynamic drag
US6212974B1 (en) * 1998-12-17 2001-04-10 United Technologies Corporation Variable stiffness positioning link for a gearbox
US20110239660A1 (en) * 2010-03-30 2011-10-06 United Technologies Corporation Mounting arrangement for gas turbine engine accessories and gearbox therefor
US8347637B2 (en) * 2010-05-25 2013-01-08 United Technologies Corporation Accessory gearbox with internal layshaft
US8490411B2 (en) * 2010-11-17 2013-07-23 United Technologies Corporation Axial accessory gearbox
US20130042630A1 (en) * 2011-08-19 2013-02-21 United Technologies Corporation Gas turbine engine accessory mount
US8973465B2 (en) * 2012-07-20 2015-03-10 United Technologies Corporation Gearbox for gas turbine engine

Also Published As

Publication number Publication date
US10054001B2 (en) 2018-08-21
FR3003323A1 (fr) 2014-09-19
US20160032755A1 (en) 2016-02-04
WO2014140441A1 (fr) 2014-09-18

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