FR3049978B1 - Aube et procede de rechargement d'une couche d'abradable - Google Patents
Aube et procede de rechargement d'une couche d'abradable Download PDFInfo
- Publication number
- FR3049978B1 FR3049978B1 FR1653220A FR1653220A FR3049978B1 FR 3049978 B1 FR3049978 B1 FR 3049978B1 FR 1653220 A FR1653220 A FR 1653220A FR 1653220 A FR1653220 A FR 1653220A FR 3049978 B1 FR3049978 B1 FR 3049978B1
- Authority
- FR
- France
- Prior art keywords
- abradable
- dawn
- recharging
- layer
- 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
- 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
- F01D11/122—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 erodable or abradable material
-
- 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
- F01D5/14—Form or construction
- F01D5/147—Construction, i.e. structural features, e.g. of weight-saving hollow blades
-
- 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
- F01D5/14—Form or construction
- F01D5/20—Specially-shaped blade tips to seal space between tips and stator
-
- 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
- F01D5/30—Fixing blades to rotors; Blade roots ; Blade spacers
-
- 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
- F05D2220/00—Application
- F05D2220/30—Application in turbines
- F05D2220/36—Application in turbines specially adapted for the fan of turbofan engines
-
- 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
- F05D2230/00—Manufacture
- F05D2230/80—Repairing, retrofitting or upgrading methods
-
- 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
- F05D2230/00—Manufacture
- F05D2230/90—Coating; Surface treatment
-
- 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
-
- 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
- F05D2300/40—Organic materials
- F05D2300/44—Resins
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Architecture (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (5)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1653220A FR3049978B1 (fr) | 2016-04-12 | 2016-04-12 | Aube et procede de rechargement d'une couche d'abradable |
EP17721425.1A EP3443202B1 (fr) | 2016-04-12 | 2017-04-10 | Aube et procédé de rechargement d'une couche d'abradable |
PCT/FR2017/050862 WO2017178747A1 (fr) | 2016-04-12 | 2017-04-10 | Aube et procede de rechargement d'une couche d'abradable |
CN201780025838.8A CN109072707B (zh) | 2016-04-12 | 2017-04-10 | 叶片和用于重新加载耐磨层的方法 |
US16/092,733 US10982560B2 (en) | 2016-04-12 | 2017-04-10 | Blade and method for reloading an abradable coating |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1653220A FR3049978B1 (fr) | 2016-04-12 | 2016-04-12 | Aube et procede de rechargement d'une couche d'abradable |
FR1653220 | 2016-04-12 |
Publications (2)
Publication Number | Publication Date |
---|---|
FR3049978A1 FR3049978A1 (fr) | 2017-10-13 |
FR3049978B1 true FR3049978B1 (fr) | 2018-04-27 |
Family
ID=56101699
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1653220A Active FR3049978B1 (fr) | 2016-04-12 | 2016-04-12 | Aube et procede de rechargement d'une couche d'abradable |
Country Status (5)
Country | Link |
---|---|
US (1) | US10982560B2 (fr) |
EP (1) | EP3443202B1 (fr) |
CN (1) | CN109072707B (fr) |
FR (1) | FR3049978B1 (fr) |
WO (1) | WO2017178747A1 (fr) |
Family Cites Families (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3346175A (en) * | 1966-04-01 | 1967-10-10 | Gen Motors Corp | Plastic coating for compressors |
GB0100695D0 (en) * | 2001-01-11 | 2001-02-21 | Rolls Royce Plc | a turbomachine blade |
US7252478B2 (en) * | 2004-07-21 | 2007-08-07 | Delta T Corporation | Fan blade modifications |
CN101027486A (zh) * | 2004-09-28 | 2007-08-29 | 大金工业株式会社 | 摩擦部件及流体机械 |
CN2742187Y (zh) * | 2004-10-12 | 2005-11-23 | 大庆石油管理局 | 抗磨损多级离心泵 |
US7410342B2 (en) * | 2005-05-05 | 2008-08-12 | Florida Turbine Technologies, Inc. | Airfoil support |
US9133726B2 (en) * | 2007-09-17 | 2015-09-15 | United Technologies Corporation | Seal for gas turbine engine component |
GB0911330D0 (en) * | 2009-07-01 | 2009-08-12 | Rolls Royce Plc | Actuatable seal for aerofoil blade tip |
CN101825111A (zh) * | 2010-02-09 | 2010-09-08 | 于风福 | 一种耐磨损风机 |
US20150192029A1 (en) * | 2012-09-20 | 2015-07-09 | General Electric Company | Turbomachine blade tip insert |
FR3007063B1 (fr) * | 2013-06-13 | 2015-07-03 | Composite Ind | Piece de materiau abradable pour la fabrication d'un secteur de joint annulaire abradable pour turbomachine et procede de fabrication d'une telle piece |
US10408224B2 (en) * | 2014-01-23 | 2019-09-10 | United Technologies Corporation | Fan blades with abrasive tips |
-
2016
- 2016-04-12 FR FR1653220A patent/FR3049978B1/fr active Active
-
2017
- 2017-04-10 WO PCT/FR2017/050862 patent/WO2017178747A1/fr active Application Filing
- 2017-04-10 CN CN201780025838.8A patent/CN109072707B/zh active Active
- 2017-04-10 US US16/092,733 patent/US10982560B2/en active Active
- 2017-04-10 EP EP17721425.1A patent/EP3443202B1/fr active Active
Also Published As
Publication number | Publication date |
---|---|
FR3049978A1 (fr) | 2017-10-13 |
EP3443202B1 (fr) | 2020-04-01 |
CN109072707B (zh) | 2021-05-25 |
US20190120074A1 (en) | 2019-04-25 |
WO2017178747A1 (fr) | 2017-10-19 |
US10982560B2 (en) | 2021-04-20 |
CN109072707A (zh) | 2018-12-21 |
EP3443202A1 (fr) | 2019-02-20 |
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Legal Events
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PLFP | Fee payment |
Year of fee payment: 2 |
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Effective date: 20171013 |
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Year of fee payment: 3 |
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CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20180809 |
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Year of fee payment: 4 |
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