UA79289C2 - Устройство для восстановления центрирования вала ротора после разъединения - Google Patents
Устройство для восстановления центрирования вала ротора после разъединения Download PDFInfo
- Publication number
- UA79289C2 UA79289C2 UA20041210782A UA20041210782A UA79289C2 UA 79289 C2 UA79289 C2 UA 79289C2 UA 20041210782 A UA20041210782 A UA 20041210782A UA 20041210782 A UA20041210782 A UA 20041210782A UA 79289 C2 UA79289 C2 UA 79289C2
- Authority
- UA
- Ukraine
- Prior art keywords
- bearing
- support
- ramp
- axis
- disconnection
- Prior art date
Links
- 230000033001 locomotion Effects 0.000 claims abstract description 25
- 239000002184 metal Substances 0.000 claims description 8
- 238000005096 rolling process Methods 0.000 claims description 4
- 229920001971 elastomer Polymers 0.000 claims description 3
- 239000000806 elastomer Substances 0.000 claims description 3
- 230000006378 damage Effects 0.000 description 5
- 230000009467 reduction Effects 0.000 description 4
- 125000004122 cyclic group Chemical group 0.000 description 2
- 238000000926 separation method Methods 0.000 description 2
- 230000035939 shock Effects 0.000 description 2
- 230000009471 action Effects 0.000 description 1
- 238000013459 approach Methods 0.000 description 1
- 230000005540 biological transmission Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 238000006073 displacement reaction Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000012634 fragment Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 230000003993 interaction Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 238000004321 preservation Methods 0.000 description 1
- 230000008569 process Effects 0.000 description 1
- 230000003068 static effect Effects 0.000 description 1
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
- F02C7/06—Arrangements of bearings; Lubricating
-
- 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
-
- 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
- F16C19/52—Bearings with rolling contact, for exclusively rotary movement with devices affected by abnormal or undesired conditions
-
- 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
- F16C23/00—Bearings for exclusively rotary movement adjustable for aligning or positioning
- F16C23/10—Bearings, parts of which are eccentrically adjustable with respect to each other
-
- 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
- F16C35/00—Rigid support of bearing units; Housings, e.g. caps, covers
- F16C35/04—Rigid support of bearing units; Housings, e.g. caps, covers in the case of ball or roller bearings
- F16C35/06—Mounting or dismounting of ball or roller bearings; Fixing them onto shaft or in housing
- F16C35/07—Fixing them on the shaft or housing with interposition of an element
- F16C35/077—Fixing them on the shaft or housing with interposition of an element between housing and outer race ring
-
- 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
- F16C2360/00—Engines or pumps
- F16C2360/23—Gas turbine engines
-
- 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)
- Support Of The Bearing (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Motor Or Generator Frames (AREA)
- Iron Core Of Rotating Electric Machines (AREA)
Abstract
Устройство для восстановления центрировки вала (1) ротора относительно продольной оси Х конструкции (3) статора в случае разъединения, вызванного появлением чрезмерного перекоса, при этом вал при нормальных условиях работы является коаксиальным относительно оси Х и стопорится в радиальном направлении опорой (5) подшипника, установленной в отверстии с осью Х названной конструкции (3) статора. Опора (5) подшипника имеет внешний диаметр, меньший диаметра отверстия, для обеспечения орбитального вращения опоры подшипника вокруг оси Х в случае разъединения, и соединена с конструкцией (3) статора с помощью предохранительных элементов (6), которые радиально разрушаются. Устройство имеет средства для восстановления центровки опоры подшипника после разъединения. Средства восстановления центровки опоры (5) подшипника содержат средства (10) генерирования прецессионного движения Р опоры (5) подшипника в направлении, противоположном ее орбитальному вращению после разъединения, и по крайней мере два устройства (20), предназначенных для уменьшения допустимого отклонения опоры (5) подшипника относительно оси X. При этом устройства уменьшения отклонения равномерно распределены вокруг осей (X, 11) обоих деталей, которые представляют собой конструкцию (3) статора и опору (5) подшипника и каждая из которых имеет первую рампу (21), выполненную на одной с двух деталей, и выступ (22), выполненный на другой из названных деталей, который при условии отсутствия разъединения отдален в радиальном направлении от первой рампы (21) и выполнен с возможностью контакта с первой рампой во время прецессионного движения Р опоры (5) подшипника.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0207978A FR2841592B1 (fr) | 2002-06-27 | 2002-06-27 | Recentrage d'un rotor apres decouplage |
PCT/FR2003/001957 WO2004007915A1 (fr) | 2002-06-27 | 2003-06-25 | Recentrage d'un rotor apres decouplage |
Publications (1)
Publication Number | Publication Date |
---|---|
UA79289C2 true UA79289C2 (ru) | 2007-06-11 |
Family
ID=29724921
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
UA20041210782A UA79289C2 (ru) | 2002-06-27 | 2003-06-25 | Устройство для восстановления центрирования вала ротора после разъединения |
Country Status (9)
Country | Link |
---|---|
US (1) | US7404678B2 (ru) |
EP (1) | EP1540143B1 (ru) |
JP (1) | JP4203473B2 (ru) |
AU (1) | AU2003253081A1 (ru) |
DE (1) | DE60309183T2 (ru) |
FR (1) | FR2841592B1 (ru) |
RU (1) | RU2309300C2 (ru) |
UA (1) | UA79289C2 (ru) |
WO (1) | WO2004007915A1 (ru) |
Families Citing this family (29)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2444935B (en) * | 2006-12-06 | 2009-06-10 | Rolls Royce Plc | A turbofan gas turbine engine |
US8262353B2 (en) * | 2007-11-30 | 2012-09-11 | General Electric Company | Decoupler system for rotor assemblies |
FR2926603B1 (fr) * | 2008-01-23 | 2010-03-26 | Snecma | Guidage d'un arbre dans une turbomachine |
GB0812832D0 (en) * | 2008-07-15 | 2008-08-20 | Rolls Royce Plc | A centering device |
FR2955615B1 (fr) * | 2010-01-28 | 2012-02-24 | Snecma | Systeme de decouplage pour arbre rotatif d'un turboreacteur d'aeronef |
DE102010012228B4 (de) * | 2010-03-19 | 2021-01-14 | Rolls-Royce Deutschland Ltd & Co Kg | Strahltriebwerk mit einer Sollbruchstellenvorrichtung für den Überlastfall |
FR2961865B1 (fr) * | 2010-06-28 | 2014-05-09 | Snecma | Turboreacteur d'aeronef comprenant des moyens de recentrage de l'arbre d'entrainement du rotor de soufflante apres une perte d'aube |
US9080461B2 (en) | 2012-02-02 | 2015-07-14 | Pratt & Whitney Canada Corp. | Fan and boost joint |
US9777596B2 (en) | 2013-12-23 | 2017-10-03 | Pratt & Whitney Canada Corp. | Double frangible bearing support |
US9777592B2 (en) | 2013-12-23 | 2017-10-03 | Pratt & Whitney Canada Corp. | Post FBO windmilling bumper |
DE102014220317A1 (de) * | 2014-10-07 | 2016-04-07 | Rolls-Royce Deutschland Ltd & Co Kg | Fluggasturbinentriebwerk mit Stoßdämpfungselement für Fanschaufelverlust |
EP3296525B1 (en) * | 2016-09-20 | 2019-11-27 | 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 |
EP3296540B1 (en) | 2016-09-20 | 2019-01-23 | 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 |
US10197102B2 (en) | 2016-10-21 | 2019-02-05 | General Electric Company | Load reduction assemblies for a gas turbine engine |
FR3063310B1 (fr) * | 2017-02-28 | 2019-04-26 | Safran Aircraft Engines | Moteur d'aeronef comprenant un palier entre deux arbres concentriques |
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 |
DE102018116018A1 (de) * | 2018-07-02 | 2020-01-02 | Rolls-Royce Deutschland Ltd & Co Kg | Lagervorrichtung zur Lastreduzierung |
DE102018116019A1 (de) | 2018-07-02 | 2020-01-02 | Rolls-Royce Deutschland Ltd & Co Kg | Lagervorrichtung zur Lastreduzierung |
US11021995B2 (en) | 2018-08-06 | 2021-06-01 | Raytheon Technologies Corporation | Imbalance damping devices for gas turbine engine fan shaft bearings |
FR3096744B1 (fr) * | 2019-06-03 | 2022-01-14 | Safran Aircraft Engines | Ensemble de support et de guidage d’un arbre d’entrainement de turbomachine d’aeronef |
US11420755B2 (en) | 2019-08-08 | 2022-08-23 | General Electric Company | Shape memory alloy isolator for a gas turbine engine |
US11105223B2 (en) | 2019-08-08 | 2021-08-31 | General Electric Company | Shape memory alloy reinforced casing |
US11274557B2 (en) | 2019-11-27 | 2022-03-15 | General Electric Company | Damper assemblies for rotating drum rotors of gas turbine engines |
US11280219B2 (en) | 2019-11-27 | 2022-03-22 | General Electric Company | Rotor support structures for rotating drum rotors of gas turbine engines |
US11319833B2 (en) * | 2020-04-24 | 2022-05-03 | General Electric Company | Fan case with crack-arresting backsheet structure and removable containment cartridge |
US11828235B2 (en) | 2020-12-08 | 2023-11-28 | General Electric Company | Gearbox for a gas turbine engine utilizing shape memory alloy dampers |
Family Cites Families (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2079402B (en) * | 1980-06-27 | 1984-02-22 | Rolls Royce | System for supporting a rotor in conditions of dynamic imbalance |
US5433584A (en) * | 1994-05-05 | 1995-07-18 | Pratt & Whitney Canada, Inc. | Bearing support housing |
GB2320526B (en) * | 1996-12-20 | 2000-09-20 | Rolls Royce Plc | Ducted fan gas turbine engine |
GB2322914B (en) * | 1997-03-05 | 2000-05-24 | Rolls Royce Plc | Ducted fan gas turbine engine |
US5791789A (en) * | 1997-04-24 | 1998-08-11 | United Technologies Corporation | Rotor support for a turbine engine |
GB2326679B (en) * | 1997-06-25 | 2000-07-26 | Rolls Royce Plc | Ducted fan gas turbine engine |
US6082959A (en) * | 1998-12-22 | 2000-07-04 | United Technologies Corporation | Method and apparatus for supporting a rotatable shaft within a gas turbine engine |
US6331078B1 (en) * | 1998-12-23 | 2001-12-18 | United Technologies Corporation | Turbine engine bearing |
US6325546B1 (en) * | 1999-11-30 | 2001-12-04 | General Electric Company | Fan assembly support system |
US6491497B1 (en) * | 2000-09-22 | 2002-12-10 | General Electric Company | Method and apparatus for supporting rotor assemblies during unbalances |
US6783319B2 (en) * | 2001-09-07 | 2004-08-31 | General Electric Co. | Method and apparatus for supporting rotor assemblies during unbalances |
FR2837240B1 (fr) * | 2002-03-14 | 2004-07-09 | Snecma Moteurs | Dispositif de support et de recentrage d'un arbre d'une soufflante d'un turboreacteur apres decouplage |
DE10218459B3 (de) * | 2002-04-25 | 2004-01-15 | Mtu Aero Engines Gmbh | Verdichter in mehrstufiger Axialbauart |
US7097413B2 (en) * | 2004-05-12 | 2006-08-29 | United Technologies Corporation | Bearing support |
-
2002
- 2002-06-27 FR FR0207978A patent/FR2841592B1/fr not_active Expired - Fee Related
-
2003
- 2003-06-25 RU RU2005101882/06A patent/RU2309300C2/ru active
- 2003-06-25 WO PCT/FR2003/001957 patent/WO2004007915A1/fr active IP Right Grant
- 2003-06-25 US US10/517,763 patent/US7404678B2/en active Active
- 2003-06-25 JP JP2004520715A patent/JP4203473B2/ja not_active Expired - Lifetime
- 2003-06-25 DE DE60309183T patent/DE60309183T2/de not_active Expired - Lifetime
- 2003-06-25 UA UA20041210782A patent/UA79289C2/ru unknown
- 2003-06-25 EP EP03763921A patent/EP1540143B1/fr not_active Expired - Lifetime
- 2003-06-25 AU AU2003253081A patent/AU2003253081A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
US7404678B2 (en) | 2008-07-29 |
AU2003253081A1 (en) | 2004-02-02 |
EP1540143B1 (fr) | 2006-10-18 |
RU2005101882A (ru) | 2005-10-27 |
US20050220384A1 (en) | 2005-10-06 |
WO2004007915A1 (fr) | 2004-01-22 |
RU2309300C2 (ru) | 2007-10-27 |
DE60309183T2 (de) | 2007-09-06 |
FR2841592B1 (fr) | 2004-09-10 |
JP2005530958A (ja) | 2005-10-13 |
EP1540143A1 (fr) | 2005-06-15 |
FR2841592A1 (fr) | 2004-01-02 |
DE60309183D1 (de) | 2006-11-30 |
JP4203473B2 (ja) | 2009-01-07 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
UA79289C2 (ru) | Устройство для восстановления центрирования вала ротора после разъединения | |
US10815825B2 (en) | Post FBO windmilling bumper | |
US6109022A (en) | Turbofan with frangible rotor support | |
RU2418208C2 (ru) | Узел подшипника вращающегося вала и турбореактивный двигатель, оборудованный указанным узлом | |
CA2861291C (en) | Double frangible bearing support | |
US6009701A (en) | Ducted fan gas turbine engine having a frangible connection | |
JP4617166B2 (ja) | 第1および第2の軸受に支持される駆動シャフトと一体化したファンを有するターボジェットエンジン | |
RU2362888C2 (ru) | Турбомашина с разъединяющим устройством, общим для первого и второго подшипников ее приводного вала, компрессор, содержащий разъединяющее устройство, и разъединяющее устройство | |
US6494032B2 (en) | Ducted fan gas turbine engine with frangible connection | |
US20040156669A1 (en) | Retaining device for a connection device, decoupling system equipped with such a device | |
US2647380A (en) | Flexible shaft | |
US10760617B2 (en) | Bearing device for load reduction | |
US10344806B2 (en) | Shaft assembly comprising a frangible coupling and a flexible coupling | |
US20170037911A1 (en) | Flexible coupling means, a mechanical transmission, and an aircraft | |
GB2130340A (en) | Gas turbine rotor assembly | |
EP0374769B1 (en) | Coil spring for a spring clutch assembly | |
US11795840B2 (en) | Assembly for supporting and guiding a drive shaft for an aircraft turbine engine | |
US11215076B2 (en) | Bearing device for load reduction | |
US5503541A (en) | Reverse rotation preventing clutch | |
RU2793926C2 (ru) | Трансмиссионный вал, содержащий разрывную секцию, и способ защиты такого трансмиссионного вала от превышения крутящего момента | |
JP2003322223A (ja) | 歯車装置 |