CN106661959B - 包括使风扇脱联接的装置的涡轮机 - Google Patents
包括使风扇脱联接的装置的涡轮机 Download PDFInfo
- Publication number
- CN106661959B CN106661959B CN201580037563.0A CN201580037563A CN106661959B CN 106661959 B CN106661959 B CN 106661959B CN 201580037563 A CN201580037563 A CN 201580037563A CN 106661959 B CN106661959 B CN 106661959B
- Authority
- CN
- China
- Prior art keywords
- turbine
- fan
- shaft
- reduction device
- decoupling
- 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
Links
Classifications
-
- 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
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
- F01D21/045—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position special arrangements in stators or in rotors dealing with breaking-off of part of rotor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/05—Shafts or bearings, or assemblies thereof, specially adapted for elastic fluid pumps
- F04D29/053—Shafts
- F04D29/054—Arrangements for joining or assembling shafts
-
- 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
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F01D21/003—Arrangements for testing or measuring
-
- 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
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F01D21/04—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for responsive to undesired position of rotor relative to stator or to breaking-off of a part of the rotor, e.g. indicating such position
- F01D21/06—Shutting-down
-
- 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
- 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
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
- F02C3/107—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with two or more rotors connected by power transmission
- F02C3/113—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with two or more rotors connected by power transmission with variable power transmission between rotors
-
- 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
- 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
- F02K3/06—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 with front fan
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D25/00—Pumping installations or systems
- F04D25/02—Units comprising pumps and their driving means
- F04D25/04—Units comprising pumps and their driving means the pump being fluid-driven
- F04D25/045—Units comprising pumps and their driving means the pump being fluid-driven the pump wheel carrying the fluid driving means, e.g. turbine blades
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/325—Rotors specially for elastic fluids for axial flow pumps for axial flow fans
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F04—POSITIVE - DISPLACEMENT MACHINES FOR LIQUIDS; PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
- F04D—NON-POSITIVE-DISPLACEMENT PUMPS
- F04D29/00—Details, component parts, or accessories
- F04D29/26—Rotors specially for elastic fluids
- F04D29/32—Rotors specially for elastic fluids for axial flow pumps
- F04D29/38—Blades
- F04D29/388—Blades characterised by construction
-
- 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
- F05D2220/32—Application in turbines in gas 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
- F05D2240/00—Components
- F05D2240/60—Shafts
-
- 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
- F05D2260/30—Retaining components in desired mutual position
- F05D2260/31—Retaining bolts or nuts
- F05D2260/311—Retaining bolts or nuts of the frangible or shear type
-
- 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
-
- 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
-
- 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)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Control Of Turbines (AREA)
- Control Of Positive-Displacement Air Blowers (AREA)
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1455939 | 2014-06-25 | ||
| FR1455939A FR3022890B1 (fr) | 2014-06-25 | 2014-06-25 | Turbomachine comportant un moyen de decouplage d'une soufflante |
| PCT/FR2015/051614 WO2015197949A1 (fr) | 2014-06-25 | 2015-06-17 | Turbomachine comportant un moyen de decouplage d'une soufflante |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN106661959A CN106661959A (zh) | 2017-05-10 |
| CN106661959B true CN106661959B (zh) | 2018-11-13 |
Family
ID=51659800
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201580037563.0A Active CN106661959B (zh) | 2014-06-25 | 2015-06-17 | 包括使风扇脱联接的装置的涡轮机 |
Country Status (9)
| Country | Link |
|---|---|
| US (2) | US20170175753A1 (cg-RX-API-DMAC7.html) |
| EP (1) | EP3161270B1 (cg-RX-API-DMAC7.html) |
| JP (1) | JP6682458B2 (cg-RX-API-DMAC7.html) |
| CN (1) | CN106661959B (cg-RX-API-DMAC7.html) |
| BR (1) | BR112016030489B1 (cg-RX-API-DMAC7.html) |
| CA (1) | CA2952914C (cg-RX-API-DMAC7.html) |
| FR (1) | FR3022890B1 (cg-RX-API-DMAC7.html) |
| RU (1) | RU2681392C2 (cg-RX-API-DMAC7.html) |
| WO (1) | WO2015197949A1 (cg-RX-API-DMAC7.html) |
Families Citing this family (32)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB201419859D0 (en) * | 2014-11-07 | 2014-12-24 | Rolls Royce Plc | No title listed |
| EP3296540B1 (en) * | 2016-09-20 | 2019-01-23 | Rolls-Royce Deutschland Ltd & Co KG | Gas turbine engine with a geared turbofan arrangement |
| EP3296524B1 (en) | 2016-09-20 | 2019-02-27 | Rolls-Royce Deutschland Ltd & Co KG | Gas turbine engine with a geared turbofan arrangement |
| EP3296525B1 (en) * | 2016-09-20 | 2019-11-27 | Rolls-Royce Deutschland Ltd & Co KG | Gas turbine engine with a geared turbofan arrangement |
| EP3296552B1 (en) | 2016-09-20 | 2019-06-05 | Rolls-Royce Deutschland Ltd & Co KG | Gas turbine engine with a geared turbofan arrangement |
| US10737801B2 (en) * | 2016-10-31 | 2020-08-11 | Rolls-Royce Corporation | Fan module with rotatable vane ring power system |
| FR3061238B1 (fr) * | 2016-12-23 | 2020-09-04 | Safran Aircraft Engines | Turbomachine a reducteur pour un aeronef equipee de moyens fusibles |
| US12060837B2 (en) * | 2017-02-10 | 2024-08-13 | Pratt & Whitney Canada Corp. | Reduction gearbox for gas turbine engine |
| EP3396115A1 (en) * | 2017-04-28 | 2018-10-31 | Rolls-Royce Deutschland Ltd & Co KG | Gas turbine engine |
| US10738646B2 (en) | 2017-06-12 | 2020-08-11 | Raytheon Technologies Corporation | Geared turbine engine with gear driving low pressure compressor and fan at common speed, and failsafe overspeed protection and shear section |
| US10612555B2 (en) * | 2017-06-16 | 2020-04-07 | United Technologies Corporation | Geared turbofan with overspeed protection |
| US10954813B2 (en) * | 2017-08-18 | 2021-03-23 | Rolls-Royce Deutschland Ltd & Co Kg | Planetary gearbox system and method for operating a planetary gearbox system |
| EP3444495A1 (en) | 2017-08-18 | 2019-02-20 | Rolls-Royce Deutschland Ltd & Co KG | Mechanical clutch device and method for operating a mechanical clutch device |
| FR3075878B1 (fr) * | 2017-12-22 | 2019-11-22 | Safran Aircraft Engines | Dispositif d'accouplement de deux arbres de turbomachine d'aeronef |
| FR3078750B1 (fr) * | 2018-03-09 | 2020-04-03 | Safran Aircraft Engines | Accouplement flexible comprenant des soufflets et des dents de reprise de couple |
| FR3079550B1 (fr) | 2018-03-27 | 2020-10-23 | Safran Aircraft Engines | Arbre de turbine d'une turbomachine et procede de protection contre une survitesse dudit arbre |
| FR3082906B1 (fr) * | 2018-06-25 | 2020-06-05 | Safran Aircraft Engines | Turbomachine d'aeronef comportant des roulements a rouleaux coniques a chaque extremite d'un arbre et une liaison flexible entre lesdits roulements |
| EP3587768A1 (en) * | 2018-06-27 | 2020-01-01 | Rolls-Royce Deutschland Ltd & Co KG | Gas turbine |
| FR3087233B1 (fr) * | 2018-10-10 | 2021-02-12 | Safran Aircraft Engines | Module de soufflante a pales a calage variable |
| FR3093146B1 (fr) | 2019-02-21 | 2021-01-29 | Safran Aircraft Engines | Arbre de transmission comprenant une section fusible et procédé de protection contre un sur-couple d’un tel arbre de transmission |
| GB201917773D0 (en) * | 2019-12-05 | 2020-01-22 | Rolls Royce Plc | High power epicyclic gearbox and operation thereof |
| US11181046B1 (en) * | 2019-09-10 | 2021-11-23 | Florida Turbine Technologies, Inc. | High speed shaft flexible coupling |
| GB201914042D0 (en) | 2019-09-30 | 2019-11-13 | Rolls Royce Plc | Gas turbine engine |
| US11353089B2 (en) | 2019-10-03 | 2022-06-07 | Rolls-Royce Corporation | Epicyclical gear system housing assembly |
| US11215265B2 (en) * | 2019-10-03 | 2022-01-04 | Rolls-Royce Corporation | Static curvic joint for epicyclical gear system housing assembly |
| US11391217B2 (en) | 2019-10-03 | 2022-07-19 | Rolls-Royce Corporation | Stiffening member for epicyclical gear system housing assembly |
| GB201917760D0 (en) * | 2019-12-05 | 2020-01-22 | Rolls Royce Plc | Aircraft engine |
| FR3106363B1 (fr) | 2020-01-22 | 2022-09-09 | Safran Aircraft Engines | Module de soufflante pour un banc d’essai de turbomachine d’aeronef |
| IT202000028520A1 (it) * | 2020-11-26 | 2022-05-26 | Ge Avio Srl | Sistema e metodo per la mitigazione di velocita' eccessiva di rotore |
| US11691745B1 (en) * | 2022-04-30 | 2023-07-04 | Beta Air, Llc | Systems and methods for locking an electric propulsion system |
| US20230348087A1 (en) * | 2022-04-30 | 2023-11-02 | Beta Air, Llc | Systems and methods for locking an electric propulsion system |
| FR3169933A1 (fr) * | 2024-12-12 | 2026-06-19 | Safran Aircraft Engines | Turbomachine d’aeronef comportant un dispositif de decouplage mecanique du reducteur. |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4651521A (en) * | 1985-11-21 | 1987-03-24 | Avco Corporation | Convertible turbo-fan, turbo-shaft aircraft propulsion system |
| US20020189231A1 (en) * | 2001-06-19 | 2002-12-19 | Snecma Moteurs | Emergency device for relighting a windmilling turbojet |
| US20090092487A1 (en) * | 2007-10-09 | 2009-04-09 | United Technologies Corp. | Systems and Methods Involving Multiple Torque Paths for Gas Turbine Engines |
| CN203271949U (zh) * | 2013-04-18 | 2013-11-06 | 李宇霞 | 新型小型涵道涡扇发动机 |
| CN105745400A (zh) * | 2013-11-21 | 2016-07-06 | 斯奈克玛 | 在具有减速齿轮的涡轮喷气发动机的模块化拆卸期间密封的前罩壳 |
Family Cites Families (17)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR1251656A (fr) | 1960-03-18 | 1961-01-20 | Raccord pour conduites en matière plastique et autres | |
| FR1251655A (fr) | 1960-03-18 | 1961-01-20 | Tente de camping | |
| GB2080486B (en) * | 1980-07-15 | 1984-02-15 | Rolls Royce | Shafts |
| US4871296A (en) * | 1988-11-07 | 1989-10-03 | Allied-Signal Inc. | Decoupler shaft and air turbine starter having such a decoupler |
| JPH04105635A (ja) | 1990-08-24 | 1992-04-07 | Toshiba Corp | 内視鏡 |
| JPH04105635U (ja) * | 1991-02-22 | 1992-09-11 | 日立造船株式会社 | シヤーピン切断検出器 |
| GB2377731A (en) * | 2001-07-21 | 2003-01-22 | Rolls Royce Plc | Rotor shaft assembly for a gas turbine engine |
| FR2845126B1 (fr) * | 2002-09-26 | 2004-12-03 | Snecma Moteurs | Dispositif decoupleur en traction |
| US7603844B2 (en) * | 2005-10-19 | 2009-10-20 | General Electric Company | Gas turbine engine assembly and methods of assembling same |
| FR2905414B1 (fr) * | 2006-08-29 | 2013-03-01 | Snecma | Dispositif d'entrainement du rotor d'un equipement auxiliaire d'un turbomoteur. |
| EP2085631A1 (en) * | 2008-02-04 | 2009-08-05 | Siemens Aktiengesellschaft | Torque protection device and torque transmission assembly |
| KR101352118B1 (ko) | 2008-08-08 | 2014-01-14 | 엘지디스플레이 주식회사 | 발광 표시장치 및 이의 제조방법 |
| FR2955615B1 (fr) * | 2010-01-28 | 2012-02-24 | Snecma | Systeme de decouplage pour arbre rotatif d'un turboreacteur d'aeronef |
| FR2970196B1 (fr) * | 2011-01-10 | 2012-12-28 | Snecma | Procede de realisation d'un renfort metallique |
| US9169780B2 (en) * | 2011-07-15 | 2015-10-27 | Pratt & Whitney Canada Corp. | Connection for generator in a gas turbine engine |
| US8777576B2 (en) * | 2011-08-22 | 2014-07-15 | General Electric Company | Metallic fan blade platform |
| FR2991421B1 (fr) * | 2012-05-30 | 2015-07-31 | Snecma | Reducteur a train epicycloidal avec axes de satellites montes sur roulements |
-
2014
- 2014-06-25 FR FR1455939A patent/FR3022890B1/fr active Active
-
2015
- 2015-06-17 CN CN201580037563.0A patent/CN106661959B/zh active Active
- 2015-06-17 CA CA2952914A patent/CA2952914C/fr active Active
- 2015-06-17 JP JP2016574387A patent/JP6682458B2/ja active Active
- 2015-06-17 BR BR112016030489-6A patent/BR112016030489B1/pt active IP Right Grant
- 2015-06-17 WO PCT/FR2015/051614 patent/WO2015197949A1/fr not_active Ceased
- 2015-06-17 RU RU2017100264A patent/RU2681392C2/ru active
- 2015-06-17 EP EP15738729.1A patent/EP3161270B1/fr active Active
-
2016
- 2016-12-23 US US15/390,353 patent/US20170175753A1/en not_active Abandoned
-
2019
- 2019-12-27 US US16/728,992 patent/US11391290B2/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4651521A (en) * | 1985-11-21 | 1987-03-24 | Avco Corporation | Convertible turbo-fan, turbo-shaft aircraft propulsion system |
| US20020189231A1 (en) * | 2001-06-19 | 2002-12-19 | Snecma Moteurs | Emergency device for relighting a windmilling turbojet |
| US20090092487A1 (en) * | 2007-10-09 | 2009-04-09 | United Technologies Corp. | Systems and Methods Involving Multiple Torque Paths for Gas Turbine Engines |
| CN203271949U (zh) * | 2013-04-18 | 2013-11-06 | 李宇霞 | 新型小型涵道涡扇发动机 |
| CN105745400A (zh) * | 2013-11-21 | 2016-07-06 | 斯奈克玛 | 在具有减速齿轮的涡轮喷气发动机的模块化拆卸期间密封的前罩壳 |
Also Published As
| Publication number | Publication date |
|---|---|
| EP3161270B1 (fr) | 2020-08-05 |
| BR112016030489A2 (cg-RX-API-DMAC7.html) | 2017-08-22 |
| RU2681392C2 (ru) | 2019-03-06 |
| US11391290B2 (en) | 2022-07-19 |
| US20170175753A1 (en) | 2017-06-22 |
| RU2017100264A3 (cg-RX-API-DMAC7.html) | 2019-01-09 |
| JP6682458B2 (ja) | 2020-04-15 |
| US20200149542A1 (en) | 2020-05-14 |
| BR112016030489B1 (pt) | 2022-12-06 |
| CN106661959A (zh) | 2017-05-10 |
| CA2952914C (fr) | 2023-02-28 |
| RU2017100264A (ru) | 2018-07-25 |
| EP3161270A1 (fr) | 2017-05-03 |
| JP2017531116A (ja) | 2017-10-19 |
| CA2952914A1 (fr) | 2015-12-30 |
| WO2015197949A1 (fr) | 2015-12-30 |
| FR3022890A1 (fr) | 2016-01-01 |
| FR3022890B1 (fr) | 2018-01-05 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP6682458B2 (ja) | ファンを分離する手段を備えるターボ機械 | |
| CN110088427B (zh) | 包括用于使风扇脱联接的装置的涡轮机 | |
| US10190440B2 (en) | Emergency shut-down detection system for a gas turbine | |
| CN106150701B (zh) | 用于支承间接驱动的涡扇发动机的转子轴的系统 | |
| JP2017141827A (ja) | ガスタービンエンジンの形状記憶合金構成要素を備えたロータ支持システム | |
| EP2535525B1 (en) | Surge margin control for a gas turbine engine | |
| CN109519238B (zh) | 燃气涡轮发动机 | |
| CN102472295B (zh) | 用于具有可变斜度叶片的螺旋桨的毂 | |
| US20140119903A1 (en) | Gas Turbine Engine With Inlet Particle Separator and Thermal Management | |
| CN111954752B (zh) | 涡轮机的涡轮轴以及用于保护所述轴免于超速的方法 | |
| US6827548B2 (en) | Rotor assemblies for gas turbine engines | |
| GB2550478A (en) | Aircraft turbine engine comprising a discharge device | |
| CN105531463A (zh) | 排气涡轮增压器 | |
| CN119712320A (zh) | 用于发动机中的超速检测和保护的系统和方法 | |
| CA2929832A1 (en) | Emergency shut-down detection system for a gas turbine | |
| GB2377731A (en) | Rotor shaft assembly for a gas turbine engine | |
| US12071854B2 (en) | Curvilinear coupling for aircraft turbomachinery | |
| CN117580763A (zh) | 用于飞行器的涡轮发动机的具有可变桨距轮叶和齿轮传动配重装置的螺旋桨 | |
| US12352178B2 (en) | Turbine overspeed protection | |
| US12486784B2 (en) | Turbine overspeed protection |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| GR01 | Patent grant | ||
| GR01 | Patent grant |