SG11201404464YA - Turbomachine rotor balancing system - Google Patents
Turbomachine rotor balancing systemInfo
- Publication number
- SG11201404464YA SG11201404464YA SG11201404464YA SG11201404464YA SG11201404464YA SG 11201404464Y A SG11201404464Y A SG 11201404464YA SG 11201404464Y A SG11201404464Y A SG 11201404464YA SG 11201404464Y A SG11201404464Y A SG 11201404464YA SG 11201404464Y A SG11201404464Y A SG 11201404464YA
- Authority
- SG
- Singapore
- Prior art keywords
- balancing system
- turbomachine rotor
- rotor balancing
- turbomachine
- rotor
- 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
- 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
- F01D5/027—Arrangements for balancing
-
- 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
- F04D29/66—Combating cavitation, whirls, noise, vibration or the like; Balancing
- F04D29/661—Combating cavitation, whirls, noise, vibration or the like; Balancing especially adapted for elastic fluid pumps
- F04D29/662—Balancing of rotors
-
- 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
- F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
- F16F15/00—Suppression of vibrations in systems; Means or arrangements for avoiding or reducing out-of-balance forces, e.g. due to motion
- F16F15/32—Correcting- or balancing-weights or equivalent means for balancing rotating bodies, e.g. vehicle wheels
- F16F15/34—Fastening arrangements therefor
-
- 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
- F05D2260/15—Load balancing
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/417,454 US8888458B2 (en) | 2012-03-12 | 2012-03-12 | Turbomachine rotor balancing system |
PCT/US2013/026631 WO2013138023A1 (en) | 2012-03-12 | 2013-02-19 | Turbomachine rotor balancing system |
Publications (1)
Publication Number | Publication Date |
---|---|
SG11201404464YA true SG11201404464YA (en) | 2014-10-30 |
Family
ID=49114274
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SG11201404464YA SG11201404464YA (en) | 2012-03-12 | 2013-02-19 | Turbomachine rotor balancing system |
Country Status (4)
Country | Link |
---|---|
US (1) | US8888458B2 (en) |
EP (1) | EP2825746B1 (en) |
SG (1) | SG11201404464YA (en) |
WO (1) | WO2013138023A1 (en) |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9410427B2 (en) | 2012-06-05 | 2016-08-09 | United Technologies Corporation | Compressor power and torque transmitting hub |
US9388697B2 (en) * | 2012-07-17 | 2016-07-12 | Solar Turbines Incorporated | First stage compressor disk configured for balancing the compressor rotor assembly |
FR3001515B1 (en) * | 2013-01-25 | 2015-03-20 | Snecma | ASSEMBLY OF BALANCING MASSELOTTE TO A ROTOR ELEMENT |
US9567857B2 (en) * | 2013-03-08 | 2017-02-14 | Rolls-Royce North American Technologies, Inc. | Turbine split ring retention and anti-rotation method |
WO2015088623A2 (en) * | 2013-09-26 | 2015-06-18 | United Technologies Corporation | Balanced rotating component for a gas powered engine |
FR3011575B1 (en) * | 2013-10-09 | 2018-02-16 | Safran Aircraft Engines | DISC FOR BALANCING A ROTOR, AND ROTOR |
FR3021065B1 (en) * | 2014-05-19 | 2016-11-25 | Snecma | BALANCED MODULE COMPRISING A ROTOR DISC, AND BALANCING METHOD |
FR3021066B1 (en) | 2014-05-19 | 2019-05-10 | Safran Aircraft Engines | BALANCED ROTOR DISC, AND BALANCING METHOD |
EP3091177B1 (en) * | 2015-05-07 | 2017-12-20 | MTU Aero Engines GmbH | Rotor for a flow engine and compressor |
US10024165B2 (en) * | 2015-11-20 | 2018-07-17 | United Technologies Corporation | De-oiler balance weights for turbomachine rotors and systems for removing excess oil from turbomachine rotors |
US10323519B2 (en) * | 2016-06-23 | 2019-06-18 | United Technologies Corporation | Gas turbine engine having a turbine rotor with torque transfer and balance features |
DE102017207283A1 (en) * | 2017-04-28 | 2018-10-31 | Rolls-Royce Deutschland Ltd & Co Kg | Rotor arrangement with balancing element and method for mounting a balancing element |
US10968744B2 (en) | 2017-05-04 | 2021-04-06 | Rolls-Royce Corporation | Turbine rotor assembly having a retaining collar for a bayonet mount |
US10865646B2 (en) | 2017-05-04 | 2020-12-15 | Rolls-Royce Corporation | Turbine assembly with auxiliary wheel |
US10774678B2 (en) | 2017-05-04 | 2020-09-15 | Rolls-Royce Corporation | Turbine assembly with auxiliary wheel |
US20180320522A1 (en) * | 2017-05-04 | 2018-11-08 | Rolls-Royce Corporation | Turbine assembly with auxiliary wheel |
DE102017109952A1 (en) * | 2017-05-09 | 2018-11-15 | Rolls-Royce Deutschland Ltd & Co Kg | Rotor device of a turbomachine |
US10697300B2 (en) * | 2017-12-14 | 2020-06-30 | Raytheon Technologies Corporation | Rotor balance weight system |
WO2019182832A1 (en) * | 2018-03-23 | 2019-09-26 | Dana Automotive Systems Group, Llc | Correcting an imbalance in a rotating shaft |
FR3081495B1 (en) * | 2018-05-24 | 2020-05-29 | Safran Aircraft Engines | BALANCING DEVICE FOR AN AIRCRAFT TURBOMACHINE ROTOR AND ROTOR COMPRISING SAME |
US10907477B2 (en) * | 2018-06-18 | 2021-02-02 | Raytheon Technologies Corporation | Clip and pin balance for rotor |
FR3091721B1 (en) * | 2019-01-10 | 2021-01-15 | Safran Aircraft Engines | MASSELOTTE TURBOMACHINE ROTOR |
US10954861B2 (en) | 2019-03-14 | 2021-03-23 | Raytheon Technologies Corporation | Seal for a gas turbine engine |
US11448081B2 (en) | 2019-10-18 | 2022-09-20 | Raytheon Technologies Corporation | Balanced circumferential seal |
US11480071B2 (en) * | 2020-06-02 | 2022-10-25 | Pratt & Whitney Canada Corp. | Balancing ring geometry |
US11578599B2 (en) * | 2021-02-02 | 2023-02-14 | Pratt & Whitney Canada Corp. | Rotor balance assembly |
FR3119647B1 (en) * | 2021-02-11 | 2023-01-13 | Safran Aircraft Engines | Turbomachine rotor flange repair process |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2404212A1 (en) | 1977-09-23 | 1979-04-20 | Snecma | ROTOR BALANCING DEVICE |
US4485678A (en) | 1982-09-27 | 1984-12-04 | Mechanical Technology Incorporated | Rotor diagnostic and balancing system |
US4879792A (en) | 1988-11-07 | 1989-11-14 | Unitedtechnologies Corporation | Method of balancing rotors |
US5412583A (en) | 1993-06-10 | 1995-05-02 | Dynamics Research Corp. | Computer implemented balancer |
US5724271A (en) | 1994-03-25 | 1998-03-03 | General Electric Company | Model-based method for optimized field balancing of rotating machinery |
US6893222B2 (en) | 2003-02-10 | 2005-05-17 | United Technologies Corporation | Turbine balancing |
FR2868807B1 (en) | 2004-04-09 | 2008-12-05 | Snecma Moteurs Sa | DEVICE FOR BALANCING A ROTATING PIECE, PARTICULARLY A TURBOJET ROTOR |
US7371042B2 (en) | 2004-12-21 | 2008-05-13 | General Electric Company | Method and apparatus for balancing gas turbine engines |
FR2885196B1 (en) | 2005-04-29 | 2007-06-29 | Snecma Moteurs Sa | DEVICE FOR BALANCING A TURBOMACHINE ROTOR |
FR2907497B1 (en) | 2006-10-24 | 2009-01-23 | Snecma Sa | BALANCING SYSTEM FOR TURBOMACHINE ROTOR |
FR2907498B1 (en) | 2006-10-24 | 2009-01-23 | Snecma Sa | BALANCING SYSTEM FOR TURBOMACHINE ROTOR |
US7685876B2 (en) | 2006-12-20 | 2010-03-30 | General Electric Company | Methods and systems for balancing a rotatable member |
DE102008016329A1 (en) * | 2008-03-28 | 2009-10-01 | Rolls-Royce Deutschland Ltd & Co Kg | Rotor balancing arrangement for gas-turbine engine, has inward aligned strips provided in outer collar of rotor disk, and axial aligned retaining groove provided in strips for balancing bodies that engage in strips and stuck onto strips |
US8353670B2 (en) | 2009-07-30 | 2013-01-15 | Pratt & Whitney Canada Corp. | Axial balancing clip weight for rotor assembly and method for balancing a rotor assembly |
US8506253B2 (en) * | 2009-08-19 | 2013-08-13 | Pratt & Whitney Canada Corp. | Balancing apparatus for rotor assembly |
US8631578B2 (en) | 2009-10-01 | 2014-01-21 | Pratt & Whitney Canada Corp. | Radial balancing clip weight for rotor assembly |
-
2012
- 2012-03-12 US US13/417,454 patent/US8888458B2/en active Active
-
2013
- 2013-02-19 EP EP13761712.2A patent/EP2825746B1/en active Active
- 2013-02-19 SG SG11201404464YA patent/SG11201404464YA/en unknown
- 2013-02-19 WO PCT/US2013/026631 patent/WO2013138023A1/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
EP2825746A1 (en) | 2015-01-21 |
EP2825746A4 (en) | 2015-10-28 |
EP2825746B1 (en) | 2019-10-02 |
US20130236310A1 (en) | 2013-09-12 |
WO2013138023A1 (en) | 2013-09-19 |
US8888458B2 (en) | 2014-11-18 |
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