CA2879380A1 - Damper system and corresponding turbine - Google Patents
Damper system and corresponding turbine Download PDFInfo
- Publication number
- CA2879380A1 CA2879380A1 CA2879380A CA2879380A CA2879380A1 CA 2879380 A1 CA2879380 A1 CA 2879380A1 CA 2879380 A CA2879380 A CA 2879380A CA 2879380 A CA2879380 A CA 2879380A CA 2879380 A1 CA2879380 A1 CA 2879380A1
- Authority
- CA
- Canada
- Prior art keywords
- tip shroud
- damper
- turbine
- cmc
- adjacent
- 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.)
- Abandoned
Links
- 239000011153 ceramic matrix composite Substances 0.000 claims description 35
- 239000002184 metal Substances 0.000 claims description 12
- 229910052751 metal Inorganic materials 0.000 claims description 12
- 238000013016 damping Methods 0.000 abstract 1
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 6
- 230000008901 benefit Effects 0.000 description 5
- 150000002739 metals Chemical class 0.000 description 4
- 229910000531 Co alloy Inorganic materials 0.000 description 3
- 229910045601 alloy Inorganic materials 0.000 description 3
- 239000000956 alloy Substances 0.000 description 3
- 239000007789 gas Substances 0.000 description 3
- 239000000463 material Substances 0.000 description 3
- 229910001092 metal group alloy Inorganic materials 0.000 description 3
- 229910052759 nickel Inorganic materials 0.000 description 3
- 229910000601 superalloy Inorganic materials 0.000 description 3
- -1 but not limited to Chemical class 0.000 description 2
- RLQJEEJISHYWON-UHFFFAOYSA-N flonicamid Chemical compound FC(F)(F)C1=CC=NC=C1C(=O)NCC#N RLQJEEJISHYWON-UHFFFAOYSA-N 0.000 description 2
- 229920002134 Carboxymethyl cellulose Polymers 0.000 description 1
- 235000010948 carboxy methyl cellulose Nutrition 0.000 description 1
- 229920006184 cellulose methylcellulose Polymers 0.000 description 1
- 238000012710 chemistry, manufacturing and control Methods 0.000 description 1
- 238000002485 combustion reaction Methods 0.000 description 1
- 230000000295 complement effect Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 239000007769 metal material Substances 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 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]
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US201261674086P | 2012-07-20 | 2012-07-20 | |
US61/674,086 | 2012-07-20 | ||
US13/656,098 | 2012-10-19 | ||
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 |
---|---|
CA2879380A1 true CA2879380A1 (en) | 2014-01-23 |
Family
ID=49946696
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CA2879380A Abandoned CA2879380A1 (en) | 2012-07-20 | 2013-06-21 | Damper system and corresponding turbine |
Country Status (7)
Country | Link |
---|---|
US (1) | US20140023506A1 (ja) |
EP (1) | EP2885505A1 (ja) |
JP (1) | JP2015524891A (ja) |
CN (1) | CN104471192A (ja) |
BR (1) | BR112015001224A2 (ja) |
CA (1) | CA2879380A1 (ja) |
WO (1) | WO2014014616A1 (ja) |
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 (zh) * | 2018-09-25 | 2024-02-02 | 中国船舶重工集团公司第七0三研究所 | 一种自带冠叶片带状阻尼拉筋条减振结构 |
FR3113300B1 (fr) * | 2020-08-06 | 2023-12-22 | Safran Aircraft Engines | Aubage de rotor de turbomachine |
US11739645B2 (en) | 2020-09-30 | 2023-08-29 | General Electric Company | Vibrational dampening elements |
US11536144B2 (en) | 2020-09-30 | 2022-12-27 | General Electric Company | Rotor blade damping structures |
FR3137127B1 (fr) * | 2022-06-22 | 2024-07-12 | Safran Aircraft Engines | Ensemble aubagé de turbomachine comportant des moyens de limitations de vibrations entre plateformes |
FR3137122B1 (fr) * | 2022-06-22 | 2024-06-21 | Safran Aircraft Engines | Ensemble aubagé à liaison inter-plateformes par organe de friction |
FR3137128A1 (fr) * | 2022-06-22 | 2023-12-29 | Safran Aircraft Engines | Ensemble de turbomachine comportant des aubes portant des léchettes et un câble reliant les léchettes les unes aux autres |
FR3137124B1 (fr) * | 2022-06-22 | 2024-05-31 | Safran Aircraft Engines | Ensemble de turbomachine comportant des aubes portant des léchettes dont les extrémités se recouvrent mutuellement selon la direction circonférentielle |
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 (fr) * | 2010-01-13 | 2013-08-23 | Snecma | Amortisseur de vibrations a pion entre talons d'aubes adjacentes en materiau composite d'une roue mobile de turbomachine. |
FR2955608B1 (fr) * | 2010-01-26 | 2013-01-11 | Snecma | Amortisseur de vibrations a lamelle et chemises entre talons d'aubes adjacentes en materiau composite d'une roue mobile de turbomachine. |
FR2956152B1 (fr) * | 2010-02-09 | 2012-07-06 | Snecma | Dispositif d'amortissement de vibrations entre talons d'aubes adjacentes en materiau composite d'une roue mobile de turbomachine. |
FR2957969B1 (fr) * | 2010-03-26 | 2013-03-29 | Snecma | Dispositif d'etancheite entre les talons d'aubes adjacentes en materiau compositie d'une roue mobile de turbomachine |
FR2960021B1 (fr) * | 2010-05-12 | 2014-04-25 | Snecma | Roue mobile de turbomachine munie d'un jonc d'amortissement des vibrations |
FR2975123B1 (fr) * | 2011-05-13 | 2013-06-14 | Snecma Propulsion Solide | Rotor de turbomachine comprenant des aubes en materiau composite avec talon rapporte |
-
2012
- 2012-10-19 US US13/656,098 patent/US20140023506A1/en not_active Abandoned
-
2013
- 2013-06-21 CN CN201380038635.4A patent/CN104471192A/zh active Pending
- 2013-06-21 WO PCT/US2013/046963 patent/WO2014014616A1/en active Application Filing
- 2013-06-21 EP EP13734256.4A patent/EP2885505A1/en not_active Withdrawn
- 2013-06-21 BR BR112015001224A patent/BR112015001224A2/pt not_active IP Right Cessation
- 2013-06-21 CA CA2879380A patent/CA2879380A1/en not_active Abandoned
- 2013-06-21 JP JP2015523095A patent/JP2015524891A/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
WO2014014616A1 (en) | 2014-01-23 |
BR112015001224A2 (pt) | 2017-07-04 |
JP2015524891A (ja) | 2015-08-27 |
EP2885505A1 (en) | 2015-06-24 |
CN104471192A (zh) | 2015-03-25 |
US20140023506A1 (en) | 2014-01-23 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FZDE | Discontinued |
Effective date: 20170621 |