FR3044946B1 - Revetement abradable a densite variable - Google Patents
Revetement abradable a densite variable Download PDFInfo
- Publication number
- FR3044946B1 FR3044946B1 FR1562324A FR1562324A FR3044946B1 FR 3044946 B1 FR3044946 B1 FR 3044946B1 FR 1562324 A FR1562324 A FR 1562324A FR 1562324 A FR1562324 A FR 1562324A FR 3044946 B1 FR3044946 B1 FR 3044946B1
- Authority
- FR
- France
- Prior art keywords
- variable density
- abradable coating
- abradable
- coating
- variable
- 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
- 239000011248 coating agent Substances 0.000 title 1
- 238000000576 coating method 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
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
- B22F3/10—Sintering only
- B22F3/105—Sintering only by using electric current other than for infrared radiant energy, laser radiation or plasma ; by ultrasonic bonding
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
- B22F5/009—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of turbine components other than turbine blades
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
- B22F7/02—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite layers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F7/00—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression
- B22F7/06—Manufacture of composite layers, workpieces, or articles, comprising metallic powder, by sintering the powder, with or without compacting wherein at least one part is obtained by sintering or compression of composite workpieces or articles from parts, e.g. to form tipped tools
-
- C—CHEMISTRY; METALLURGY
- C23—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
- C23C—COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
- C23C24/00—Coating starting from inorganic powder
- C23C24/08—Coating starting from inorganic powder by application of heat or pressure and heat
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
- B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
- B22F2998/10—Processes characterised by the sequence of their steps
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05B—INDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
- F05B2230/00—Manufacture
- F05B2230/90—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
- F05D2230/00—Manufacture
- F05D2230/20—Manufacture essentially without removing material
- F05D2230/22—Manufacture essentially without removing material by sintering
-
- 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
- F05D2230/30—Manufacture with deposition of material
-
- 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
- F05D2300/50—Intrinsic material properties or characteristics
- F05D2300/514—Porosity
-
- 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
- F05D2300/50—Intrinsic material properties or characteristics
- F05D2300/522—Density
-
- 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
- F05D2300/609—Grain size
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Manufacturing & Machinery (AREA)
- Materials Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Composite Materials (AREA)
- Physics & Mathematics (AREA)
- Optics & Photonics (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Other Surface Treatments For Metallic Materials (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
Priority Applications (5)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1562324A FR3044946B1 (fr) | 2015-12-14 | 2015-12-14 | Revetement abradable a densite variable |
| EP16825487.8A EP3389903B1 (fr) | 2015-12-14 | 2016-12-13 | Procédé de fabrication d'un revêtement abradable à densité variable |
| CN201680073260.9A CN108367359B (zh) | 2015-12-14 | 2016-12-13 | 具有变密度的耐磨涂层 |
| PCT/FR2016/053360 WO2017103422A1 (fr) | 2015-12-14 | 2016-12-13 | Revêtement abradable a densité variable |
| US16/062,249 US11174749B2 (en) | 2015-12-14 | 2016-12-13 | Abradable coating having variable densities |
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR1562324A FR3044946B1 (fr) | 2015-12-14 | 2015-12-14 | Revetement abradable a densite variable |
| FR1562324 | 2015-12-14 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| FR3044946A1 FR3044946A1 (fr) | 2017-06-16 |
| FR3044946B1 true FR3044946B1 (fr) | 2018-01-12 |
Family
ID=55542848
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| FR1562324A Active FR3044946B1 (fr) | 2015-12-14 | 2015-12-14 | Revetement abradable a densite variable |
Country Status (5)
| Country | Link |
|---|---|
| US (1) | US11174749B2 (fr) |
| EP (1) | EP3389903B1 (fr) |
| CN (1) | CN108367359B (fr) |
| FR (1) | FR3044946B1 (fr) |
| WO (1) | WO2017103422A1 (fr) |
Families Citing this family (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR3082765B1 (fr) * | 2018-06-25 | 2021-04-30 | Safran Aircraft Engines | Procede de fabrication d'une couche abradable |
| FR3102694B1 (fr) * | 2019-10-30 | 2022-06-03 | Safran Aircraft Engines | Procede de compactage d’un revetement anti-corrosion |
| US11215070B2 (en) * | 2019-12-13 | 2022-01-04 | Pratt & Whitney Canada Corp. | Dual density abradable panels |
| CN111546006B (zh) * | 2020-05-12 | 2022-04-12 | 华能国际电力股份有限公司玉环电厂 | 一种通过泡沫铝提高锅炉管弯头耐磨性的方法 |
| US11661855B2 (en) * | 2021-10-25 | 2023-05-30 | Raytheon Technologies Corporation | Low density hybrid knife seal |
| US11828196B2 (en) * | 2022-01-28 | 2023-11-28 | Rtx Corporation | Gas turbine engine article with serpentine groove for coating interlock |
| US12163434B1 (en) * | 2023-06-28 | 2024-12-10 | Rtx Corporation | Advanced thermally conductive lightweight elastomeric seal |
| US12291971B1 (en) | 2024-02-13 | 2025-05-06 | Rtx Corporation | Blade outer air seal with graded coating |
Family Cites Families (26)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CA963497A (en) * | 1970-12-21 | 1975-02-25 | Gould Inc. | Powder metal honeycomb |
| SU997111A1 (ru) | 1981-08-06 | 1983-02-15 | Предприятие П/Я В-8769 | Способ намотки провода на многогранный каркас |
| US4914794A (en) | 1986-08-07 | 1990-04-10 | Allied-Signal Inc. | Method of making an abradable strain-tolerant ceramic coated turbine shroud |
| US5236151A (en) | 1991-12-23 | 1993-08-17 | General Electric Company | Thermal barrier structure |
| JP4166977B2 (ja) | 2001-12-17 | 2008-10-15 | 三菱重工業株式会社 | 耐高温腐食合金材、遮熱コーティング材、タービン部材、及びガスタービン |
| RU2320776C2 (ru) | 2002-10-09 | 2008-03-27 | Исикавадзима-Харима Хэви Индастриз Ко.,Лтд. | Вращающийся элемент и способ нанесения покрытия на него |
| US8079806B2 (en) * | 2007-11-28 | 2011-12-20 | United Technologies Corporation | Segmented ceramic layer for member of gas turbine engine |
| JP2009256759A (ja) | 2008-04-21 | 2009-11-05 | Fujifilm Corp | 遮熱コーティング構造及び遮熱コーティング製造方法 |
| FR2930590B1 (fr) * | 2008-04-23 | 2013-05-31 | Snecma | Carter de turbomachine comportant un dispositif empechant une instabilite lors d'un contact entre le carter et le rotor |
| EP2317079B1 (fr) * | 2009-10-30 | 2020-05-20 | Ansaldo Energia Switzerland AG | Système de revêtement abradable |
| US20120107103A1 (en) * | 2010-09-28 | 2012-05-03 | Yoshitaka Kojima | Gas turbine shroud with ceramic abradable layer |
| FR2972379B1 (fr) | 2011-03-07 | 2014-01-17 | Snecma | Procede de rechargement local de piece thermomecanique endommagee et piece ainsi realisee, en particulier piece de turbine |
| US8999226B2 (en) | 2011-08-30 | 2015-04-07 | Siemens Energy, Inc. | Method of forming a thermal barrier coating system with engineered surface roughness |
| US9034479B2 (en) | 2011-10-13 | 2015-05-19 | General Electric Company | Thermal barrier coating systems and processes therefor |
| US9186866B2 (en) * | 2012-01-10 | 2015-11-17 | Siemens Aktiengesellschaft | Powder-based material system with stable porosity |
| US10215033B2 (en) | 2012-04-18 | 2019-02-26 | General Electric Company | Stator seal for turbine rub avoidance |
| FR2996474B1 (fr) | 2012-10-05 | 2014-12-12 | Snecma | Procede pour l'integration de materiau abradable dans un logement par compression isostatique |
| FR2996475B1 (fr) * | 2012-10-05 | 2014-12-19 | Snecma | Procede pour l'integration de materiau abradable dans un logement par projection a froid |
| US9102015B2 (en) * | 2013-03-14 | 2015-08-11 | Siemens Energy, Inc | Method and apparatus for fabrication and repair of thermal barriers |
| US9151175B2 (en) * | 2014-02-25 | 2015-10-06 | Siemens Aktiengesellschaft | Turbine abradable layer with progressive wear zone multi level ridge arrays |
| US10309243B2 (en) * | 2014-05-23 | 2019-06-04 | United Technologies Corporation | Grooved blade outer air seals |
| US20150354392A1 (en) | 2014-06-10 | 2015-12-10 | General Electric Company | Abradable coatings |
| CN104451519B (zh) * | 2014-11-26 | 2017-01-18 | 华东理工大学 | 一种多层热障涂层及其形成方法 |
| US10273192B2 (en) * | 2015-02-17 | 2019-04-30 | Rolls-Royce Corporation | Patterned abradable coating and methods for the manufacture thereof |
| US20160305319A1 (en) | 2015-04-17 | 2016-10-20 | General Electric Company | Variable coating porosity to influence shroud and rotor durability |
| FR3044945B1 (fr) | 2015-12-14 | 2018-01-12 | Centre National De La Recherche Scientifique | Revetement abradable a densite variable |
-
2015
- 2015-12-14 FR FR1562324A patent/FR3044946B1/fr active Active
-
2016
- 2016-12-13 CN CN201680073260.9A patent/CN108367359B/zh active Active
- 2016-12-13 US US16/062,249 patent/US11174749B2/en active Active
- 2016-12-13 EP EP16825487.8A patent/EP3389903B1/fr active Active
- 2016-12-13 WO PCT/FR2016/053360 patent/WO2017103422A1/fr not_active Ceased
Also Published As
| Publication number | Publication date |
|---|---|
| CN108367359A (zh) | 2018-08-03 |
| EP3389903B1 (fr) | 2022-04-13 |
| US11174749B2 (en) | 2021-11-16 |
| CN108367359B (zh) | 2021-07-27 |
| WO2017103422A1 (fr) | 2017-06-22 |
| FR3044946A1 (fr) | 2017-06-16 |
| EP3389903A1 (fr) | 2018-10-24 |
| US20180371932A1 (en) | 2018-12-27 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PLFP | Fee payment |
Year of fee payment: 2 |
|
| PLSC | Publication of the preliminary search report |
Effective date: 20170616 |
|
| PLFP | Fee payment |
Year of fee payment: 3 |
|
| CD | Change of name or company name |
Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20180809 |
|
| PLFP | Fee payment |
Year of fee payment: 5 |
|
| PLFP | Fee payment |
Year of fee payment: 6 |
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| PLFP | Fee payment |
Year of fee payment: 7 |
|
| 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 |