SG11201403114WA - Turbomachine geared architecture support assembly - Google Patents
Turbomachine geared architecture support assemblyInfo
- Publication number
- SG11201403114WA SG11201403114WA SG11201403114WA SG11201403114WA SG11201403114WA SG 11201403114W A SG11201403114W A SG 11201403114WA SG 11201403114W A SG11201403114W A SG 11201403114WA SG 11201403114W A SG11201403114W A SG 11201403114WA SG 11201403114W A SG11201403114W A SG 11201403114WA
- Authority
- SG
- Singapore
- Prior art keywords
- support assembly
- geared architecture
- architecture support
- turbomachine geared
- turbomachine
- Prior art date
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
- 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
- F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
- F01D25/162—Bearing supports
-
- 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
- F01D25/16—Arrangement of bearings; Supporting or mounting bearings in casings
- F01D25/162—Bearing supports
- F01D25/164—Flexible supports; Vibration damping means associated with the bearing
-
- 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
-
- 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
- F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
-
- 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
- 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
- F05D2230/00—Manufacture
- F05D2230/50—Building or constructing in particular ways
- F05D2230/53—Building or constructing in particular ways by integrally manufacturing a component, e.g. by milling from a billet or one piece 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
- F05D2230/00—Manufacture
- F05D2230/60—Assembly methods
- F05D2230/64—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins
- F05D2230/642—Assembly methods using positioning or alignment devices for aligning or centring, e.g. pins using maintaining alignment while permitting differential dilatation
-
- 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
- F05D2250/40—Movement of components
- F05D2250/41—Movement of components with one degree of freedom
-
- 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
- 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
- F05D2300/00—Materials; Properties thereof
- F05D2300/50—Intrinsic material properties or characteristics
- F05D2300/501—Elasticity
-
- 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)
- General Details Of Gearings (AREA)
- Retarders (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/362,389 US9017010B2 (en) | 2012-01-31 | 2012-01-31 | Turbomachine geared architecture support assembly |
PCT/US2013/021897 WO2013154642A1 (en) | 2012-01-31 | 2013-01-17 | Turbomachine geared architecture support assembly |
Publications (1)
Publication Number | Publication Date |
---|---|
SG11201403114WA true SG11201403114WA (en) | 2014-09-26 |
Family
ID=48870357
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SG11201403114WA SG11201403114WA (en) | 2012-01-31 | 2013-01-17 | Turbomachine geared architecture support assembly |
Country Status (7)
Country | Link |
---|---|
US (2) | US9017010B2 (en) |
EP (2) | EP2809889B8 (en) |
JP (1) | JP5893761B2 (en) |
CN (1) | CN104081007B (en) |
RU (1) | RU2644421C2 (en) |
SG (1) | SG11201403114WA (en) |
WO (1) | WO2013154642A1 (en) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9017010B2 (en) * | 2012-01-31 | 2015-04-28 | United Technologies Corporation | Turbomachine geared architecture support assembly |
US8961112B2 (en) * | 2012-03-26 | 2015-02-24 | United Technologies Corporation | Torque frame bushing arrangement for gas turbine engine fan drive gear system |
US9145830B2 (en) * | 2012-06-04 | 2015-09-29 | United Technologies Corporation | Turbomachine geared architecture support assembly |
US10221771B2 (en) * | 2014-09-24 | 2019-03-05 | United Technologies Corporation | Fan drive gear system |
CN104948301A (en) * | 2015-05-20 | 2015-09-30 | 西安交通大学 | Hot end bearing of gas turbine |
CN107816528B (en) * | 2016-09-13 | 2022-05-24 | 博格华纳公司 | Compliant planet carrier |
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 |
FR3078110B1 (en) * | 2018-02-19 | 2020-03-06 | Safran Aircraft Engines | ASSEMBLY FOR HOLDING A GEAR TRAIN IN A TURBOMACHINE |
FR3113701B1 (en) * | 2020-09-03 | 2023-01-20 | Safran Aircraft Engines | AIRCRAFT TURBOMACHINE ASSEMBLY INCLUDING AXIAL AND RADIAL FAN RETENTION MEANS |
FR3128264B1 (en) * | 2021-10-14 | 2024-02-09 | Safran Trans Systems | Improved device and method for centering an annular assembly of a planetary gearbox |
US11639688B1 (en) | 2022-04-06 | 2023-05-02 | General Electric Company | Mounting for planetary gear systems |
Family Cites Families (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SU853122A1 (en) * | 1979-10-12 | 1981-08-07 | Предприятие П/Я М-5906 | Turbomachine bearing assembly |
FR2504980B1 (en) * | 1981-04-29 | 1985-06-14 | Snecma | BEARING ASSEMBLY, PARTICULARLY FOR TURBOMACHINES |
US5433674A (en) * | 1994-04-12 | 1995-07-18 | United Technologies Corporation | Coupling system for a planetary gear train |
JP2000220472A (en) | 1998-12-23 | 2000-08-08 | United Technol Corp <Utc> | Fan case liner |
DE10307221A1 (en) | 2003-02-20 | 2004-09-02 | Zf Friedrichshafen Ag | planet |
FR2853382B1 (en) * | 2003-04-04 | 2006-04-28 | Hispano Suiza Sa | FLEXIBLE BONDING SYSTEM BETWEEN A SATELLITE HOLDER AND THE FIXED SUPPORT IN A SPEED REDUCER |
US7490460B2 (en) * | 2005-10-19 | 2009-02-17 | General Electric Company | Gas turbine engine assembly and methods of assembling same |
US7685808B2 (en) * | 2005-10-19 | 2010-03-30 | General Electric Company | Gas turbine engine assembly and methods of assembling same |
US7591754B2 (en) | 2006-03-22 | 2009-09-22 | United Technologies Corporation | Epicyclic gear train integral sun gear coupling design |
US8672606B2 (en) * | 2006-06-30 | 2014-03-18 | Solar Turbines Inc. | Gas turbine engine and system for servicing a gas turbine engine |
US8585538B2 (en) | 2006-07-05 | 2013-11-19 | United Technologies Corporation | Coupling system for a star gear train in a gas turbine engine |
US7926260B2 (en) | 2006-07-05 | 2011-04-19 | United Technologies Corporation | Flexible shaft for gas turbine engine |
US7694505B2 (en) | 2006-07-31 | 2010-04-13 | General Electric Company | Gas turbine engine assembly and method of assembling same |
US9228534B2 (en) | 2007-07-02 | 2016-01-05 | United Technologies Corporation | Variable contour nacelle assembly for a gas turbine engine |
US8672801B2 (en) | 2009-11-30 | 2014-03-18 | United Technologies Corporation | Mounting system for a planetary gear train in a gas turbine engine |
US8845277B2 (en) * | 2010-05-24 | 2014-09-30 | United Technologies Corporation | Geared turbofan engine with integral gear and bearing supports |
US9017010B2 (en) * | 2012-01-31 | 2015-04-28 | United Technologies Corporation | Turbomachine geared architecture support assembly |
-
2012
- 2012-01-31 US US13/362,389 patent/US9017010B2/en active Active
-
2013
- 2013-01-17 CN CN201380007455.XA patent/CN104081007B/en active Active
- 2013-01-17 EP EP13775951.0A patent/EP2809889B8/en active Active
- 2013-01-17 EP EP20205202.3A patent/EP3798427B1/en active Active
- 2013-01-17 JP JP2014555566A patent/JP5893761B2/en active Active
- 2013-01-17 WO PCT/US2013/021897 patent/WO2013154642A1/en active Application Filing
- 2013-01-17 SG SG11201403114WA patent/SG11201403114WA/en unknown
- 2013-01-17 RU RU2014134422A patent/RU2644421C2/en active
-
2014
- 2014-04-07 US US14/246,424 patent/US8961113B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
US9017010B2 (en) | 2015-04-28 |
EP2809889A1 (en) | 2014-12-10 |
RU2644421C2 (en) | 2018-02-12 |
EP2809889A4 (en) | 2015-11-18 |
JP5893761B2 (en) | 2016-03-23 |
JP2015507126A (en) | 2015-03-05 |
RU2014134422A (en) | 2016-03-27 |
EP3798427A1 (en) | 2021-03-31 |
US20130195604A1 (en) | 2013-08-01 |
EP3798427B1 (en) | 2023-08-30 |
WO2013154642A1 (en) | 2013-10-17 |
EP2809889B1 (en) | 2020-11-04 |
US20140219774A1 (en) | 2014-08-07 |
US8961113B2 (en) | 2015-02-24 |
EP2809889B8 (en) | 2020-12-30 |
CN104081007A (en) | 2014-10-01 |
CN104081007B (en) | 2016-11-09 |
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