BR112015001224A2 - damping system and turbine - Google Patents
damping system and turbineInfo
- Publication number
- BR112015001224A2 BR112015001224A2 BR112015001224A BR112015001224A BR112015001224A2 BR 112015001224 A2 BR112015001224 A2 BR 112015001224A2 BR 112015001224 A BR112015001224 A BR 112015001224A BR 112015001224 A BR112015001224 A BR 112015001224A BR 112015001224 A2 BR112015001224 A2 BR 112015001224A2
- Authority
- BR
- Brazil
- Prior art keywords
- turbine
- damping system
- damping
- Prior art date
Links
- 238000013016 damping Methods 0.000 title 1
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
- F01D5/12—Blades
- F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
- F01D5/225—Blade-to-blade connections, e.g. for damping vibrations by shrouding
-
- 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
- F01D5/12—Blades
- F01D5/22—Blade-to-blade connections, e.g. for damping vibrations
- F01D5/24—Blade-to-blade connections, e.g. for damping vibrations using wire or the like
-
- 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
- F05D2300/60—Properties or characteristics given to material by treatment or manufacturing
- F05D2300/603—Composites; e.g. fibre-reinforced
- F05D2300/6033—Ceramic matrix composites [CMC]
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201261674086P | 2012-07-20 | 2012-07-20 | |
US13/656,098 US20140023506A1 (en) | 2012-07-20 | 2012-10-19 | Damper system and a turbine |
PCT/US2013/046963 WO2014014616A1 (en) | 2012-07-20 | 2013-06-21 | Damper system and corresponding turbine |
Publications (1)
Publication Number | Publication Date |
---|---|
BR112015001224A2 true BR112015001224A2 (en) | 2017-07-04 |
Family
ID=49946696
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112015001224A BR112015001224A2 (en) | 2012-07-20 | 2013-06-21 | damping system and turbine |
Country Status (7)
Country | Link |
---|---|
US (1) | US20140023506A1 (en) |
EP (1) | EP2885505A1 (en) |
JP (1) | JP2015524891A (en) |
CN (1) | CN104471192A (en) |
BR (1) | BR112015001224A2 (en) |
CA (1) | CA2879380A1 (en) |
WO (1) | WO2014014616A1 (en) |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10316673B2 (en) | 2016-03-24 | 2019-06-11 | General Electric Company | CMC turbine blade platform damper |
US10724380B2 (en) | 2017-08-07 | 2020-07-28 | General Electric Company | CMC blade with internal support |
CN109026172B (en) * | 2018-09-25 | 2024-02-02 | 中国船舶重工集团公司第七0三研究所 | From banded damping lacing wire strip vibration attenuation structure of taking guan leaf |
FR3113300B1 (en) * | 2020-08-06 | 2023-12-22 | Safran Aircraft Engines | Turbomachine rotor blade |
US11536144B2 (en) | 2020-09-30 | 2022-12-27 | General Electric Company | Rotor blade damping structures |
US11739645B2 (en) | 2020-09-30 | 2023-08-29 | General Electric Company | Vibrational dampening elements |
FR3137127A1 (en) * | 2022-06-22 | 2023-12-29 | Safran Aircraft Engines | Bladed turbomachine assembly comprising means of limiting vibrations between platforms |
FR3137122A1 (en) * | 2022-06-22 | 2023-12-29 | Safran Aircraft Engines | Bladed assembly with inter-platform connection by friction member |
FR3137124A1 (en) * | 2022-06-22 | 2023-12-29 | Safran Aircraft Engines | Turbomachine assembly comprising blades carrying liplets whose ends overlap each other in the circumferential direction |
FR3137128A1 (en) * | 2022-06-22 | 2023-12-29 | Safran Aircraft Engines | Turbomachine assembly comprising blades carrying lips and a cable connecting the lips to each other |
Family Cites Families (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1723321A (en) * | 1929-08-06 | of baden | ||
US2942843A (en) * | 1956-06-15 | 1960-06-28 | Westinghouse Electric Corp | Blade vibration damping structure |
GB1195012A (en) * | 1966-06-21 | 1970-06-17 | Rolls Royce | Rotor for Bladed Fluid Flow Machines. |
US4741205A (en) * | 1986-12-22 | 1988-05-03 | Westinghouse Electric Corp. | "V" notched integrally shrouded turbine blade and method for determining shroud tightness and wear of a circular array of rotating blades disposed in a rotor |
US6409472B1 (en) * | 1999-08-09 | 2002-06-25 | United Technologies Corporation | Stator assembly for a rotary machine and clip member for a stator assembly |
US6482533B2 (en) * | 2001-03-05 | 2002-11-19 | The Boeing Company | Article having imbedded cavity |
US8714932B2 (en) * | 2008-12-31 | 2014-05-06 | General Electric Company | Ceramic matrix composite blade having integral platform structures and methods of fabrication |
FR2955142B1 (en) * | 2010-01-13 | 2013-08-23 | Snecma | PIONE VIBRATION SHOCK ABSORBER BETWEEN ADJACENT AUB THREADS IN COMPOSITE MATERIAL OF A TURBOMACHINE MOBILE WHEEL. |
FR2955608B1 (en) * | 2010-01-26 | 2013-01-11 | Snecma | LAMINATED VIBRATION SHOCK ABSORBER AND SHOES BETWEEN ADJACENT BLADE HEADS IN COMPOSITE MATERIAL OF A TURBOMACHINE MOBILE WHEEL. |
FR2956152B1 (en) * | 2010-02-09 | 2012-07-06 | Snecma | VIBRATION DAMPING DEVICE BETWEEN ADJACENT BLADE HEADS IN COMPOSITE MATERIAL OF A MOBILE TURBOMACHINE WHEEL. |
FR2957969B1 (en) * | 2010-03-26 | 2013-03-29 | Snecma | DEVICE FOR SEALING BETWEEN ADJACENT BLADE HEADS IN MATERIAL COMPOSED OF A TURBOMACHINE MOBILE WHEEL |
FR2960021B1 (en) * | 2010-05-12 | 2014-04-25 | Snecma | TURBOMACHINE MOBILE WHEEL HAVING A VIBRATION DAMPING ROUND |
FR2975123B1 (en) * | 2011-05-13 | 2013-06-14 | Snecma Propulsion Solide | ROTOR OF TURBOMACHINE COMPRISING AUBES IN COMPOSITE MATERIAL WITH REPORTED HEEL |
-
2012
- 2012-10-19 US US13/656,098 patent/US20140023506A1/en not_active Abandoned
-
2013
- 2013-06-21 BR BR112015001224A patent/BR112015001224A2/en not_active IP Right Cessation
- 2013-06-21 EP EP13734256.4A patent/EP2885505A1/en not_active Withdrawn
- 2013-06-21 WO PCT/US2013/046963 patent/WO2014014616A1/en active Application Filing
- 2013-06-21 CA CA2879380A patent/CA2879380A1/en not_active Abandoned
- 2013-06-21 CN CN201380038635.4A patent/CN104471192A/en active Pending
- 2013-06-21 JP JP2015523095A patent/JP2015524891A/en active Pending
Also Published As
Publication number | Publication date |
---|---|
EP2885505A1 (en) | 2015-06-24 |
WO2014014616A1 (en) | 2014-01-23 |
JP2015524891A (en) | 2015-08-27 |
CA2879380A1 (en) | 2014-01-23 |
US20140023506A1 (en) | 2014-01-23 |
CN104471192A (en) | 2015-03-25 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
B08F | Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette] | ||
B08K | Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette] |