PL3289189T3 - Silnik turbinowy, który może być osadzony w skrzyni redukcyjnej - Google Patents

Silnik turbinowy, który może być osadzony w skrzyni redukcyjnej

Info

Publication number
PL3289189T3
PL3289189T3 PL16722309.8T PL16722309T PL3289189T3 PL 3289189 T3 PL3289189 T3 PL 3289189T3 PL 16722309 T PL16722309 T PL 16722309T PL 3289189 T3 PL3289189 T3 PL 3289189T3
Authority
PL
Poland
Prior art keywords
turbine engine
reduction gearbox
gearbox
reduction
turbine
Prior art date
Application number
PL16722309.8T
Other languages
English (en)
Inventor
Olivier Lafargue
Sébastien BROTIER
Alphonse Puerto
Original Assignee
Safran Helicopter Engines
Airbus Helicopters
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 Helicopter Engines, Airbus Helicopters filed Critical Safran Helicopter Engines
Publication of PL3289189T3 publication Critical patent/PL3289189T3/pl

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/16Arrangement of bearings; Supporting or mounting bearings in casings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/16Arrangement of bearings; Supporting or mounting bearings in casings
    • F01D25/162Bearing supports
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C3/00Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/10Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor
    • F02C3/103Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor the compressor being of the centrifugal type
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/06Arrangements of bearings; Lubricating
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/32Arrangement, mounting, or driving, of auxiliaries
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/36Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/30Application in turbines
    • F05D2220/32Application in turbines in gas turbines
    • F05D2220/329Application in turbines in gas turbines in helicopters
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/50Building or constructing in particular ways
    • F05D2230/51Building or constructing in particular ways in a modular way, e.g. using several identical or complementary parts or features
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/70Disassembly methods
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/72Maintenance
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00Function
    • F05D2260/40Transmission of power
    • F05D2260/403Transmission of power through the shape of the drive components
    • F05D2260/4031Transmission of power through the shape of the drive components as in toothed gearing
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/60Efficient 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)
  • Mounting Of Bearings Or Others (AREA)
  • General Details Of Gearings (AREA)
PL16722309.8T 2015-04-27 2016-04-26 Silnik turbinowy, który może być osadzony w skrzyni redukcyjnej PL3289189T3 (pl)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1553751A FR3035446B1 (fr) 2015-04-27 2015-04-27 Turbomoteur encastrable dans un boitier reducteur
PCT/FR2016/050977 WO2016174341A1 (fr) 2015-04-27 2016-04-26 Turbomoteur encastrable dans un boitier reducteur

Publications (1)

Publication Number Publication Date
PL3289189T3 true PL3289189T3 (pl) 2021-02-22

Family

ID=55129941

Family Applications (1)

Application Number Title Priority Date Filing Date
PL16722309.8T PL3289189T3 (pl) 2015-04-27 2016-04-26 Silnik turbinowy, który może być osadzony w skrzyni redukcyjnej

Country Status (10)

Country Link
US (1) US10961867B2 (pl)
EP (1) EP3289189B1 (pl)
JP (1) JP6764878B2 (pl)
KR (1) KR20170140218A (pl)
CN (1) CN107532482B (pl)
CA (1) CA2981171C (pl)
FR (1) FR3035446B1 (pl)
PL (1) PL3289189T3 (pl)
RU (1) RU2706855C2 (pl)
WO (1) WO2016174341A1 (pl)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
PL3703176T3 (pl) 2017-10-26 2025-04-07 Lg Energy Solution, Ltd. Urządzenie, system i sposób do zbierania gazu wytwarzanego w ogniwie wtórnym
FR3096081B1 (fr) * 2019-05-15 2021-04-23 Safran Helicopter Engines Pignon d’arbre de turbomachine à voile comportant une structure réticulée
CN110905653B (zh) * 2019-11-25 2021-05-25 航天时代飞鸿技术有限公司 一种二冲程航空活塞发动机增压器
FR3166166A1 (fr) 2024-09-06 2026-03-13 Safran Helicopter Engines Groupe propulsif pour un aeronef comprenant un turbomoteur et un reducteur

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1291164B (de) * 1967-05-18 1969-03-20 Man Turbo Gmbh Zweiwellengasturbinentriebwerk
DE3642506A1 (de) * 1986-12-12 1988-06-23 Mtu Muenchen Gmbh Gasturbinenanlage
US6969235B2 (en) * 2003-05-19 2005-11-29 Honeywell International, Inc. Air turbine starter with angular contact thrust bearing
US7089728B2 (en) 2003-12-17 2006-08-15 Ingersoll-Rand Energy Systems Corporation Single-piece turbine rotor and pinion gear and manufacturing technique for same
US7055303B2 (en) * 2003-12-22 2006-06-06 Pratt & Whitney Canada Corp. Gas turbine engine architecture
FR2905414B1 (fr) * 2006-08-29 2013-03-01 Snecma Dispositif d'entrainement du rotor d'un equipement auxiliaire d'un turbomoteur.
US8794107B2 (en) * 2010-05-05 2014-08-05 Hamilton Sundstrand Corporation Submerged gear and bearing guard
FR2961260B1 (fr) * 2010-06-15 2014-05-02 Turbomeca Architecture de turbomoteur non lubrifie
FR2962488B1 (fr) * 2010-07-06 2014-05-02 Turbomeca Procede et architecture de recombinaison de puissance de turbomachine
US20130180262A1 (en) * 2012-01-18 2013-07-18 Hung Duong Gas turbine engine accessory gearbox
FR2989140B1 (fr) * 2012-04-06 2014-09-05 Snecma Systeme de transmission de puissance pour une turbomachine
FR3018860B1 (fr) * 2014-03-21 2021-10-15 Hispano Suiza Sa Relais d'accessoires pour moteur a turbine a gaz

Also Published As

Publication number Publication date
CA2981171C (fr) 2022-12-06
JP2018519450A (ja) 2018-07-19
EP3289189A1 (fr) 2018-03-07
RU2017137244A3 (pl) 2019-10-07
RU2706855C2 (ru) 2019-11-21
CN107532482A (zh) 2018-01-02
KR20170140218A (ko) 2017-12-20
WO2016174341A1 (fr) 2016-11-03
US10961867B2 (en) 2021-03-30
CA2981171A1 (fr) 2016-11-03
JP6764878B2 (ja) 2020-10-07
FR3035446A1 (fr) 2016-10-28
US20180119571A1 (en) 2018-05-03
RU2017137244A (ru) 2019-05-28
FR3035446B1 (fr) 2019-08-02
CN107532482B (zh) 2019-09-20
EP3289189B1 (fr) 2020-10-28

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