JP6450382B2 - 航空機タービンエンジンの補機ギアボックス用小型構造 - Google Patents

航空機タービンエンジンの補機ギアボックス用小型構造 Download PDF

Info

Publication number
JP6450382B2
JP6450382B2 JP2016524873A JP2016524873A JP6450382B2 JP 6450382 B2 JP6450382 B2 JP 6450382B2 JP 2016524873 A JP2016524873 A JP 2016524873A JP 2016524873 A JP2016524873 A JP 2016524873A JP 6450382 B2 JP6450382 B2 JP 6450382B2
Authority
JP
Japan
Prior art keywords
gear
drive chain
drive
chain according
forming
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
JP2016524873A
Other languages
English (en)
Japanese (ja)
Other versions
JP2016525659A (ja
JP2016525659A5 (https=
Inventor
プリュネラ−ウサ，ステファーヌ
ベック，ギヨーム
ペルティエ，ジョルダーヌ
Original Assignee
イスパノ・シユイザ
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 イスパノ・シユイザ filed Critical イスパノ・シユイザ
Publication of JP2016525659A publication Critical patent/JP2016525659A/ja
Publication of JP2016525659A5 publication Critical patent/JP2016525659A5/ja
Application granted granted Critical
Publication of JP6450382B2 publication Critical patent/JP6450382B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

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)
JP2016524873A 2013-07-10 2014-07-09 航空機タービンエンジンの補機ギアボックス用小型構造 Expired - Fee Related JP6450382B2 (ja)

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 (3)

Publication Number Publication Date
JP2016525659A JP2016525659A (ja) 2016-08-25
JP2016525659A5 JP2016525659A5 (https=) 2017-08-10
JP6450382B2 true JP6450382B2 (ja) 2019-01-09

Family

ID=49322583

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2016524873A Expired - Fee Related JP6450382B2 (ja) 2013-07-10 2014-07-09 航空機タービンエンジンの補機ギアボックス用小型構造

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

Family Cites Families (12)

* Cited by examiner, † Cited by third party
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
CN105378230B (zh) 2017-04-26
CA2917227C (fr) 2021-06-08
ES2645473T3 (es) 2017-12-05
EP3019708A1 (fr) 2016-05-18

Similar Documents

Publication Publication Date Title
JP6450382B2 (ja) 航空機タービンエンジンの補機ギアボックス用小型構造
JP6549568B2 (ja) ターボ機械用ギアボックスのピニオン壁内の歯車列の組み込み
CA2776637C (en) Dual input drive agb for gas turbine engines
RU2686248C2 (ru) Передняя часть авиационного двухконтурного газотурбинного двигателя и авиационный двухконтурный газотурбинный двигатель
US20200300340A1 (en) Aircraft engine reduction gearbox
JP5619786B2 (ja) 遊星歯車列による一対の二重反転プロペラ用の駆動機構
CN106460554B (zh) 用于飞行器涡轮发动机的组件以及用于安装该组件的方法
EP3029358A1 (en) Lightweight and compliant journal pin
US11022043B2 (en) Turbine engine with fan and reduction of speed on the shaft of the power turbine
JP2006220153A (ja) 低圧および高圧ロータに動力取り出し手段を有するツインスプールタービンエンジン、タービンエンジンのための動力取り出しモジュール、およびタービンエンジンを組み立てる方法
JP2018516331A5 (ja) タービンエンジン用のエピサイクリック歯車列を有する減速装置
JP2016525659A5 (https=)
US9726149B2 (en) Spiral bevel gear set for ram air turbine
JP6621471B2 (ja) コンパクトな脊柱状トランスミッション
CA2954108C (en) Planetary gear assembly
JP2019074166A (ja) 複合遊星歯車装置
JP5858546B2 (ja) スクリュー遠心分離機の駆動装置
CN104791399B (zh) 行星齿轮减速式单向离合器
JP2013537102A5 (https=)
CN107429798A (zh) 包括改进减速齿轮的齿轮箱
JP2006218444A (ja) 竪型ミル用減速装置
RU2002105611A (ru) Редуктор скорости
CN121399402A (zh) 飞行器双螺旋桨涡轮发动机
RU69489U1 (ru) Редуктор привода соосных несущих винтов вертолета

Legal Events

Date Code Title Description
A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20170703

A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20170703

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20180711

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20180724

A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20180820

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20181127

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20181207

R150 Certificate of patent or registration of utility model

Ref document number: 6450382

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R150

LAPS Cancellation because of no payment of annual fees