CA2917227C - Structure compacte de boitier d'entrainement pour turbomachine d'aeronef - Google Patents

Structure compacte de boitier d'entrainement pour turbomachine d'aeronef Download PDF

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Publication number
CA2917227C
CA2917227C CA2917227A CA2917227A CA2917227C CA 2917227 C CA2917227 C CA 2917227C CA 2917227 A CA2917227 A CA 2917227A CA 2917227 A CA2917227 A CA 2917227A CA 2917227 C CA2917227 C CA 2917227C
Authority
CA
Canada
Prior art keywords
gear
drive chain
main
chain according
pinion
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.)
Expired - Fee Related
Application number
CA2917227A
Other languages
English (en)
French (fr)
Other versions
CA2917227A1 (fr
Inventor
Stephane Prunera-Usach
Guillaume BECK
Jordane PELTIER
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 Transmission Systems SAS
Original Assignee
Hispano Suiza SA
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 Hispano Suiza SA filed Critical Hispano Suiza SA
Publication of CA2917227A1 publication Critical patent/CA2917227A1/fr
Application granted granted Critical
Publication of CA2917227C publication Critical patent/CA2917227C/fr
Expired - Fee Related 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/04—Helicopters
    • B64C27/12—Rotor drives
    • 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
    • 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
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C19/00—Bearings with rolling contact, for exclusively rotary movement
    • F16C19/54—Systems consisting of a plurality of bearings with rolling friction
    • 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
    • F16H2001/2881—Toothed gearings for conveying rotary motion with gears having orbital motion comprising two axially spaced central gears, i.e. ring or sun gear, engaged by at least one common orbital gear wherein one of the central gears is forming the output
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Retarders (AREA)
  • Gear Transmission (AREA)
  • Gears, Cams (AREA)
CA2917227A 2013-07-10 2014-07-09 Structure compacte de boitier d'entrainement pour turbomachine d'aeronef Expired - Fee Related CA2917227C (fr)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1356788A FR3008463B1 (fr) 2013-07-10 2013-07-10 Structure compacte de boitier d'entrainement pour turbomachine d'aeronef
FR1356788 2013-07-10
PCT/FR2014/051758 WO2015004385A1 (fr) 2013-07-10 2014-07-09 Structure compacte de boitier d'entrainement pour turbomachine d'aeronef

Publications (2)

Publication Number Publication Date
CA2917227A1 CA2917227A1 (fr) 2015-01-15
CA2917227C true CA2917227C (fr) 2021-06-08

Family

ID=49322583

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2917227A Expired - Fee Related CA2917227C (fr) 2013-07-10 2014-07-09 Structure compacte de boitier d'entrainement pour turbomachine d'aeronef

Country Status (9)

Country Link
US (1) US10323576B2 (https=)
EP (1) EP3019708B1 (https=)
JP (1) JP6450382B2 (https=)
CN (1) CN105378230B (https=)
CA (1) CA2917227C (https=)
ES (1) ES2645473T3 (https=)
FR (1) FR3008463B1 (https=)
RU (1) RU2674299C2 (https=)
WO (1) WO2015004385A1 (https=)

Families Citing this family (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3007462B1 (fr) * 2013-06-21 2017-11-24 Hispano-Suiza Boitier d'accessoires de turbomachine equipe d'une pompe centrifuge
FR3016407B1 (fr) 2014-01-16 2016-02-19 Hispano Suiza Sa Boitier d'entrainement pour equipements
RS61579B1 (sr) 2014-01-17 2021-04-29 Drillform Technical Services Ltd Integrisani cilindrični prenosnik za alate za rotaciono bušenje
US20160290489A1 (en) * 2015-04-02 2016-10-06 Hamilton Sundstrand Corporation Ring gear for an integrated drive generator
US9759305B2 (en) 2015-04-02 2017-09-12 Hamilton Sundstrand Corporation Planet gear for an integrated drive generator
US9709157B2 (en) 2015-04-03 2017-07-18 Hamilton Sundstrand Corporation Carrier shaft for a differential
PT3380525T (pt) 2015-11-25 2024-02-05 Immunogen Inc Formulações farmacêuticas e métodos que as utilizam
JP6787806B2 (ja) * 2017-02-03 2020-11-18 アズビル株式会社 操作器
FR3062692B1 (fr) * 2017-02-09 2019-04-19 Safran Transmission Systems Roulement a rotule sur rouleaux presentant une evacuation de lubrifiant amelioree, de preference pour reducteur de vitesse de turbopropulseur d'aeronef
FR3111400B1 (fr) 2020-06-11 2022-05-13 Safran Trans Systems Reducteur mecanique de turbomachine d’aeronef
FR3111390B1 (fr) 2020-06-11 2022-05-13 Safran Trans Systems Reducteur mecanique de turbomachine d’aeronef
US11572838B2 (en) 2020-09-29 2023-02-07 General Electric Company Accessory gearbox for a turbine engine
FR3116095B1 (fr) 2020-11-10 2023-04-21 Safran Trans Systems Reducteur mecanique de turbomachine d’aeronef
FR3116318B1 (fr) 2020-11-16 2023-07-28 Safran Collecteur d’huile pour un dispositif de transmission de couple d’une turbomachine d’aéronef
FR3118646B1 (fr) 2021-01-05 2024-02-16 Safran Trans Systems Porte-satellites pour un reducteur mecanique de turbomachine d’aeronef
FR3119204B1 (fr) 2021-01-26 2022-12-09 Safran Trans Systems Turbomachine d’aeronef a triple flux equipee d’un module de transmission de puissance
FR3125319B1 (fr) 2021-07-16 2023-06-09 Safran Trans Systems Ensemble mecanique et reducteur mecanique de turbomachine d’aeronef comportant un tel ensemble
FR3127256B1 (fr) 2021-09-21 2024-10-25 Safran Trans Systems Module de transmission de puissance pour une turbomachine d’aeronef
US12404821B2 (en) 2022-04-15 2025-09-02 General Electric Company Suspension of a triple-flow aircraft turbine engine
FR3134867B1 (fr) 2022-04-22 2024-05-17 Safran Trans Systems Reducteur mecanique de turbomachine d’aeronef
FR3136531B1 (fr) 2022-06-13 2024-06-14 Safran Trans Systems Train d’engrenages compact pour réducteur de turbomachine
FR3136532B1 (fr) 2022-06-13 2024-06-14 Safran Trans Systems Train d’engrenages compact pour réducteur de turbomachine
FR3139602A1 (fr) 2022-09-13 2024-03-15 Safran Transmission Systems Turbomachine d’aeronef a reducteur mecanique
US12215629B2 (en) 2023-02-06 2025-02-04 General Electric Company Turbine engine including transfer gearbox and accessory gearbox
US20250075662A1 (en) * 2023-09-05 2025-03-06 General Electric Company Turbine Engine having First and Second Accessory Gearboxes
FR3153867B1 (fr) 2023-10-10 2025-09-19 Safran Trans Systems Reducteur mecanique de turbomachine d’aeronef
US12372030B2 (en) 2023-12-15 2025-07-29 General Electric Company Turbine engine having a fire box
FR3157914B1 (fr) 2023-12-27 2025-11-21 Safran Trans Systems Mecanisme de reduction pour système propulsif aeronautique
FR3157911B1 (fr) 2023-12-27 2025-11-21 Safran Trans Systems Mecanisme de reduction pour système propulsif aeronautique
FR3157913A1 (fr) 2023-12-27 2025-07-04 Safran Transmission Systems Mecanisme de reduction pour système propulsif aeronautique
FR3157910B1 (fr) 2023-12-27 2025-11-21 Safran Trans Systems Mecanisme de reduction pour système propulsif aeronautique
FR3157912A1 (fr) 2023-12-27 2025-07-04 Safran Transmission Systems Mecanisme de reduction pour système propulsif aeronautique
IT202400002653A1 (it) * 2024-02-08 2025-08-08 Ge Avio Srl Gruppo di trasmissione ad ingranaggi per un motore a turbina

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Publication number Priority date Publication date Assignee Title
US2951631A (en) * 1956-01-25 1960-09-06 Fairchild Engine & Airplane Engine accessory drive
US2880628A (en) * 1957-09-18 1959-04-07 Vyzk A Zkusebni Letecky Ustav Transmission gear for a combined device
CH406769A (de) * 1960-06-01 1966-01-31 Mitsubishi Shipbuilding & Eng Planetengetriebe
JP2003139030A (ja) * 1995-10-19 2003-05-14 Denso Corp 車両用始動兼補機装置及び車両用始動装置
JP3763166B2 (ja) * 1996-07-10 2006-04-05 株式会社デンソー 減速装置
US5947854A (en) * 1997-05-08 1999-09-07 Worksmart Energy Enterprises, Inc. Combined variable-speed drive and speed reducer for pumps and fans
JP2000074163A (ja) * 1998-08-28 2000-03-07 Homare Shoji:Kk 歯車噛合機構
JP2008008460A (ja) * 2006-06-30 2008-01-17 Ｇｋｎ ドライブライン トルクテクノロジー株式会社 デファレンシャル装置
WO2008122276A2 (de) * 2007-04-05 2008-10-16 Neumayer Tekfor Holding Gmbh Mit einem antriebsrad versehenes differential
US20110146434A1 (en) * 2009-12-18 2011-06-23 Short Keith E Jack shaft disconnect
US20120006137A1 (en) * 2010-07-07 2012-01-12 Hamilton Sundstrand Corporation Gear driven accessory for gearbox
US9650964B2 (en) * 2010-12-28 2017-05-16 General Electric Company Accessory gearbox with a starter/generator

Also Published As

Publication number Publication date
US10323576B2 (en) 2019-06-18
FR3008463B1 (fr) 2015-08-07
RU2016103314A3 (https=) 2018-05-14
US20160146111A1 (en) 2016-05-26
EP3019708B1 (fr) 2017-08-30
CA2917227A1 (fr) 2015-01-15
RU2674299C2 (ru) 2018-12-06
JP2016525659A (ja) 2016-08-25
RU2016103314A (ru) 2017-08-14
FR3008463A1 (fr) 2015-01-16
WO2015004385A1 (fr) 2015-01-15
CN105378230A (zh) 2016-03-02
JP6450382B2 (ja) 2019-01-09
CN105378230B (zh) 2017-04-26
ES2645473T3 (es) 2017-12-05
EP3019708A1 (fr) 2016-05-18

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EEER Examination request

Effective date: 20190611

MKLA Lapsed

Effective date: 20210709