FR2979135B1 - Joint a brosse comprenant une plaque d'appui pourvue d'une dent - Google Patents
Joint a brosse comprenant une plaque d'appui pourvue d'une dentInfo
- Publication number
- FR2979135B1 FR2979135B1 FR1257672A FR1257672A FR2979135B1 FR 2979135 B1 FR2979135 B1 FR 2979135B1 FR 1257672 A FR1257672 A FR 1257672A FR 1257672 A FR1257672 A FR 1257672A FR 2979135 B1 FR2979135 B1 FR 2979135B1
- Authority
- FR
- France
- Prior art keywords
- tooth
- support plate
- brush joint
- brush
- joint
- 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.)
- Active
Links
Classifications
-
- 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
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/16—Sealings between relatively-moving surfaces
-
- 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
- F01D11/00—Preventing or minimising internal leakage of working-fluid, e.g. between stages
- F01D11/08—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator
- F01D11/12—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part
- F01D11/127—Preventing or minimising internal leakage of working-fluid, e.g. between stages for sealing space between rotor blade tips and stator using a rubstrip, e.g. erodible. deformable or resiliently-biased part with a deformable or crushable structure, e.g. honeycomb
-
- 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
- F02C7/28—Arrangement of seals
-
- 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
- F16J—PISTONS; CYLINDERS; SEALINGS
- F16J15/00—Sealings
- F16J15/16—Sealings between relatively-moving surfaces
- F16J15/32—Sealings between relatively-moving surfaces with elastic sealings, e.g. O-rings
- F16J15/3284—Sealings between relatively-moving surfaces with elastic sealings, e.g. O-rings characterised by their structure; Selection of materials
- F16J15/3288—Filamentary structures, e.g. brush seals
-
- 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
- F05D2240/00—Components
- F05D2240/55—Seals
- F05D2240/56—Brush seals
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Sealing Devices (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US13/209,668 US8657298B2 (en) | 2011-08-15 | 2011-08-15 | Brush seal with backing plate tooth |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2979135A1 FR2979135A1 (fr) | 2013-02-22 |
FR2979135B1 true FR2979135B1 (fr) | 2015-02-20 |
Family
ID=47625366
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1257672A Active FR2979135B1 (fr) | 2011-08-15 | 2012-08-07 | Joint a brosse comprenant une plaque d'appui pourvue d'une dent |
Country Status (4)
Country | Link |
---|---|
US (1) | US8657298B2 (fr) |
DE (1) | DE102012107320A1 (fr) |
FR (1) | FR2979135B1 (fr) |
RU (1) | RU2601026C2 (fr) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104196637A (zh) * | 2014-08-15 | 2014-12-10 | 江苏透平密封高科技有限公司 | 一种新型燃气轮机尾筒气封及其制造方法 |
JP6276209B2 (ja) * | 2015-02-20 | 2018-02-07 | 三菱日立パワーシステムズ株式会社 | タービン用シール装置及びタービン、並びにシール装置用の薄板 |
US9896955B2 (en) * | 2015-04-13 | 2018-02-20 | United Technologies Corporation | Static axial brush seal with dual bristle packs |
US20170260868A1 (en) * | 2016-03-11 | 2017-09-14 | General Electric Company | Method of treating a brush seal, treated brush seal, and brush seal assembly |
US10487687B1 (en) * | 2016-09-15 | 2019-11-26 | United Technologies Corporation | Gas turbine engine having a seal damper assembly |
CN106761955A (zh) * | 2016-12-30 | 2017-05-31 | 江苏鑫信润科技有限公司 | F型横齿双腔式刷式汽封 |
US10465546B2 (en) * | 2017-08-28 | 2019-11-05 | United Technologies Corporation | Brush seal with extended backing plate |
GB201814674D0 (en) * | 2018-09-10 | 2018-10-24 | Rolls Royce Plc | Radially dispaceable brush seal |
GB202213999D0 (en) * | 2022-09-26 | 2022-11-09 | Rolls Royce Plc | Dynamic sealing assembly |
Family Cites Families (36)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2474305A (en) * | 1945-04-06 | 1949-06-28 | Riley Stoker Corp | Beater element for pulverizing apparatus |
GB9020317D0 (en) | 1990-09-18 | 1990-10-31 | Cross Mfg Co | Sealing devices |
IT1284468B1 (it) | 1995-07-28 | 1998-05-21 | Mtu Muenchen Gmbh | Guarnizione a spazzola per turbomacchine |
US6173962B1 (en) | 1995-12-09 | 2001-01-16 | Rolls Royce Plc | Brush seal |
US5630590A (en) * | 1996-03-26 | 1997-05-20 | United Technologies Corporation | Method and apparatus for improving the airsealing effectiveness in a turbine engine |
US6139018A (en) | 1998-03-25 | 2000-10-31 | General Electric Co. | Positive pressure-actuated brush seal |
US6231047B1 (en) | 1998-05-29 | 2001-05-15 | Eg&G Engineered Products | Brush seal |
US6168162B1 (en) | 1998-08-05 | 2001-01-02 | General Electric Co. | Self-centering brush seal |
GB9900102D0 (en) | 1999-01-06 | 1999-02-24 | Rolls Royce Plc | A seal arrangement |
US6168377B1 (en) | 1999-01-27 | 2001-01-02 | General Electric Co. | Method and apparatus for eliminating thermal bowing of steam turbine rotors |
US6416057B1 (en) | 1999-04-16 | 2002-07-09 | Flowserve Management Company | Brush seal |
US6244599B1 (en) | 1999-04-28 | 2001-06-12 | Flowserve Management Company | Floating brush seal |
GB9929587D0 (en) * | 1999-12-16 | 2000-02-09 | Rolls Royce Plc | A seal arrangement |
DE19962316C2 (de) * | 1999-12-23 | 2002-07-18 | Mtu Aero Engines Gmbh | Bürstendichtung |
US6540231B1 (en) | 2000-02-29 | 2003-04-01 | General Electric Company | Surface following brush seal |
DE10018273B4 (de) | 2000-04-13 | 2005-10-20 | Mtu Aero Engines Gmbh | Bürstendichtung |
WO2002023069A2 (fr) | 2000-09-14 | 2002-03-21 | Turbocare, Inc. | Joint a brosse toroidale eventuellement placee dans une presse-garniture a labyrinthe |
JP4644378B2 (ja) * | 2001-03-27 | 2011-03-02 | イーグル・エンジニアリング・エアロスペース株式会社 | ブラシシール装置 |
US6550777B2 (en) | 2001-06-19 | 2003-04-22 | General Electric Company | Split packing ring segment for a brush seal insert in a rotary machine |
US6589012B2 (en) | 2001-09-24 | 2003-07-08 | General Electric Company | Method and apparatus for eliminating thermal bowing using brush seals in the diaphragm packing area of steam turbines |
GB0201666D0 (en) * | 2002-01-25 | 2002-03-13 | Cross Mfg 1938 Company Ltd | A brush seal element |
US6669203B1 (en) | 2002-07-11 | 2003-12-30 | General Electric Company | Brush seal placement between rotating and stationary components with reversely bent leaf spring |
US7093835B2 (en) | 2002-08-27 | 2006-08-22 | United Technologies Corporation | Floating brush seal assembly |
US7270333B2 (en) | 2002-11-27 | 2007-09-18 | United Technologies Corporation | Brush seal with adjustable clearance |
DE10258096A1 (de) * | 2002-12-11 | 2004-06-24 | Alstom (Switzerland) Ltd. | Bürstendichtung zum Dichten eines Spaltes zwischen einem Rotor und einem Stator |
US6910858B2 (en) * | 2002-12-26 | 2005-06-28 | United Technologies Corporation | Seal |
US8641045B2 (en) * | 2003-05-01 | 2014-02-04 | Advanced Technologies Group, Inc. | Seal with stacked sealing elements |
US7410173B2 (en) * | 2003-05-01 | 2008-08-12 | Justak John F | Hydrodynamic brush seal |
US20040217549A1 (en) * | 2003-05-01 | 2004-11-04 | Justak John F. | Hydrodynamic brush seal |
DE10320450B4 (de) | 2003-05-08 | 2013-07-18 | Mtu Aero Engines Gmbh | Dichtungsanordnung |
DE102004038933A1 (de) | 2004-08-11 | 2006-02-23 | Mtu Aero Engines Gmbh | Dichtungsanordnung |
US7413194B2 (en) * | 2004-10-28 | 2008-08-19 | Rolls-Royce Plc | Pressure balanced annular seal |
GB0423923D0 (en) | 2004-10-28 | 2004-12-01 | Rolls Royce Plc | Segmented annular seal for a gas turbine engine |
US8167313B2 (en) * | 2005-11-21 | 2012-05-01 | General Electric Company | Seal member, assembly and method |
US7461847B2 (en) | 2005-12-12 | 2008-12-09 | Eaton Corporation | Self centering, floating brush seal assembly |
FR2918144B1 (fr) * | 2007-06-29 | 2009-11-06 | Snecma Sa | Joint a brosse dynamique. |
-
2011
- 2011-08-15 US US13/209,668 patent/US8657298B2/en active Active
-
2012
- 2012-08-07 FR FR1257672A patent/FR2979135B1/fr active Active
- 2012-08-09 DE DE102012107320A patent/DE102012107320A1/de active Pending
- 2012-08-14 RU RU2012134709/06A patent/RU2601026C2/ru active
Also Published As
Publication number | Publication date |
---|---|
US8657298B2 (en) | 2014-02-25 |
RU2601026C2 (ru) | 2016-10-27 |
FR2979135A1 (fr) | 2013-02-22 |
RU2012134709A (ru) | 2014-02-20 |
DE102012107320A1 (de) | 2013-02-21 |
US20130043658A1 (en) | 2013-02-21 |
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Legal Events
Date | Code | Title | Description |
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PLFP | Fee payment |
Year of fee payment: 5 |
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PLFP | Fee payment |
Year of fee payment: 6 |
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PLFP | Fee payment |
Year of fee payment: 7 |
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PLFP | Fee payment |
Year of fee payment: 8 |
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PLFP | Fee payment |
Year of fee payment: 9 |
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PLFP | Fee payment |
Year of fee payment: 10 |
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PLFP | Fee payment |
Year of fee payment: 11 |
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PLFP | Fee payment |
Year of fee payment: 12 |
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TP | Transmission of property |
Owner name: GENERAL ELECTRIC TECHNOLOGY GMBH, CH Effective date: 20240301 |