FR2996475A1 - Procede pour l'integration de materiau abradable dans un logement par projection a froid - Google Patents
Procede pour l'integration de materiau abradable dans un logement par projection a froid Download PDFInfo
- Publication number
- FR2996475A1 FR2996475A1 FR1259515A FR1259515A FR2996475A1 FR 2996475 A1 FR2996475 A1 FR 2996475A1 FR 1259515 A FR1259515 A FR 1259515A FR 1259515 A FR1259515 A FR 1259515A FR 2996475 A1 FR2996475 A1 FR 2996475A1
- Authority
- FR
- France
- Prior art keywords
- abradable material
- temperature
- housing
- particles
- abradable
- 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.)
- Granted
Links
- 239000000463 material Substances 0.000 title claims abstract description 81
- 239000002245 particle Substances 0.000 title claims abstract description 26
- 238000005245 sintering Methods 0.000 title claims abstract description 13
- 238000004519 manufacturing process Methods 0.000 title claims description 10
- 238000010438 heat treatment Methods 0.000 title abstract 4
- 238000000034 method Methods 0.000 claims abstract description 28
- 238000003754 machining Methods 0.000 claims abstract description 8
- 238000010288 cold spraying Methods 0.000 claims abstract description 6
- 238000003825 pressing Methods 0.000 abstract 1
- 239000007789 gas Substances 0.000 description 10
- 239000000843 powder Substances 0.000 description 8
- 238000000151 deposition Methods 0.000 description 5
- 239000007921 spray Substances 0.000 description 3
- XKRFYHLGVUSROY-UHFFFAOYSA-N Argon Chemical compound [Ar] XKRFYHLGVUSROY-UHFFFAOYSA-N 0.000 description 2
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 230000008021 deposition Effects 0.000 description 2
- 230000008018 melting Effects 0.000 description 2
- 238000002844 melting Methods 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 230000003647 oxidation Effects 0.000 description 2
- 238000007254 oxidation reaction Methods 0.000 description 2
- 230000002028 premature Effects 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 229910052786 argon Inorganic materials 0.000 description 1
- 238000006243 chemical reaction Methods 0.000 description 1
- 238000005056 compaction Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 230000008034 disappearance Effects 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 239000001307 helium Substances 0.000 description 1
- 229910052734 helium Inorganic materials 0.000 description 1
- SWQJXJOGLNCZEY-UHFFFAOYSA-N helium atom Chemical compound [He] SWQJXJOGLNCZEY-UHFFFAOYSA-N 0.000 description 1
- 239000011261 inert gas Substances 0.000 description 1
- 238000012423 maintenance Methods 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 238000005498 polishing Methods 0.000 description 1
- 239000007779 soft material Substances 0.000 description 1
- 238000009718 spray deposition Methods 0.000 description 1
Classifications
-
- 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
- C23C24/02—Coating starting from inorganic powder by application of pressure only
- C23C24/04—Impact or kinetic deposition of particles
-
- 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
- B22F7/08—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 with one or more parts not made from powder
-
- 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
-
- 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
- F01D11/14—Adjusting or regulating tip-clearance, i.e. distance between rotor-blade tips and stator casing
-
- 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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Mechanical Engineering (AREA)
- Materials Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Composite Materials (AREA)
- Manufacturing & Machinery (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
Description
Claims (5)
- REVENDICATIONS1. Procédé de fabrication d'une pièce (10) présentant un logement (20) qui comprend une ouverture (25) débouchant sur une surface libre (15) de ladite pièce (10), ledit logement (20) étant destiné à recevoir un matériau abradable (50), caractérisé en ce qu'il comprend l'étape suivante : (a) On remplit ledit logement (20) avec un matériau abradable (50) constitué de particules en utilisant la technique de projection à froid à vitesse supersonique à une température T1 inférieure à 150°C, (b) On chauffe ensuite ledit matériau abradable (50) à une température T2 supérieure à 150°C et on maintient ledit matériau abradable (50) à cette température T2 jusqu'à ce qu'il se produise un frittage entre les particules dudit matériau abradable (50), (c) On abaisse ensuite la température jusqu'à la température ambiante.
- 2. Procédé de fabrication selon la revendication 1, caractérisé en ce qu'après l'étape (c), on effectue l'étape (d) : (d) On usine la surface (55) dudit matériau abradable (50) au niveau de ladite ouverture (25) de telle sorte que ladite surface (55) après usinage se situe dans le prolongement de ladite surface libre (15) de la pièce (10).
- 3. Procédé de fabrication selon la revendication 1 ou 2, caractérisé en ce qu'à l'étape (b) on applique une pression sur ledit matériau abradable (50) de façon à le compacter.
- 4. Procédé de fabrication selon l'une quelconque des revendications 1 à 3, caractérisé en ce que ladite température T2 est supérieure à la température à laquelle un maximum des porosités dudit matériau abradable (50) est résorbé.
- 5. Procédé de fabrication selon l'une quelconque des revendications 1 à 3, caractérisé en ce qu'à l'étape (a), on remplit ledit logement 20 avec une pluralité de couches de matériaux abradables (50), chaque couche étant de nature différente d'une couche adjacente.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1259515A FR2996475B1 (fr) | 2012-10-05 | 2012-10-05 | Procede pour l'integration de materiau abradable dans un logement par projection a froid |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1259515A FR2996475B1 (fr) | 2012-10-05 | 2012-10-05 | Procede pour l'integration de materiau abradable dans un logement par projection a froid |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2996475A1 true FR2996475A1 (fr) | 2014-04-11 |
FR2996475B1 FR2996475B1 (fr) | 2014-12-19 |
Family
ID=47557221
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1259515A Active FR2996475B1 (fr) | 2012-10-05 | 2012-10-05 | Procede pour l'integration de materiau abradable dans un logement par projection a froid |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2996475B1 (fr) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9644662B2 (en) * | 2014-03-18 | 2017-05-09 | Goodrich Corporation | Cold spray nodes, studs, stud assemblies, and methods of manufacture |
FR3044945A1 (fr) * | 2015-12-14 | 2017-06-16 | Snecma | Revetement abradable a densite variable |
FR3044946A1 (fr) * | 2015-12-14 | 2017-06-16 | Snecma | Revetement abradable a densite variable |
Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1921181A1 (fr) * | 2006-10-27 | 2008-05-14 | United Technologies Corporation | Bandes métalliques poreuses à pulvérisation froide |
US20090297331A1 (en) * | 2008-04-23 | 2009-12-03 | Snecma | Turbomachine casing including a device for preventing instability during contact between the casing and the rotor |
US20120032404A1 (en) * | 2010-08-03 | 2012-02-09 | Dresser-Rand Company | Low deflection bi-metal rotor seals |
US20120099973A1 (en) * | 2010-10-25 | 2012-04-26 | United Technologies Corporation | Low density abradable coating with fine porosity |
-
2012
- 2012-10-05 FR FR1259515A patent/FR2996475B1/fr active Active
Patent Citations (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1921181A1 (fr) * | 2006-10-27 | 2008-05-14 | United Technologies Corporation | Bandes métalliques poreuses à pulvérisation froide |
US20090297331A1 (en) * | 2008-04-23 | 2009-12-03 | Snecma | Turbomachine casing including a device for preventing instability during contact between the casing and the rotor |
US20120032404A1 (en) * | 2010-08-03 | 2012-02-09 | Dresser-Rand Company | Low deflection bi-metal rotor seals |
US20120099973A1 (en) * | 2010-10-25 | 2012-04-26 | United Technologies Corporation | Low density abradable coating with fine porosity |
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9644662B2 (en) * | 2014-03-18 | 2017-05-09 | Goodrich Corporation | Cold spray nodes, studs, stud assemblies, and methods of manufacture |
FR3044945A1 (fr) * | 2015-12-14 | 2017-06-16 | Snecma | Revetement abradable a densite variable |
FR3044946A1 (fr) * | 2015-12-14 | 2017-06-16 | Snecma | Revetement abradable a densite variable |
WO2017103422A1 (fr) * | 2015-12-14 | 2017-06-22 | Safran Aircraft Engines | Revêtement abradable a densité variable |
WO2017103420A1 (fr) * | 2015-12-14 | 2017-06-22 | Safran Aircraft Engines | Revetement abradable a densite variable. |
CN108367359A (zh) * | 2015-12-14 | 2018-08-03 | 赛峰航空器发动机 | 具有变密度的耐磨涂层 |
CN108367360A (zh) * | 2015-12-14 | 2018-08-03 | 赛峰航空器发动机 | 具有可变密度的耐磨损涂层 |
US11174749B2 (en) | 2015-12-14 | 2021-11-16 | Safran Aircraft Engines | Abradable coating having variable densities |
Also Published As
Publication number | Publication date |
---|---|
FR2996475B1 (fr) | 2014-12-19 |
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Owner name: SAFRAN AIRCRAFT ENGINES, FR Effective date: 20170719 |
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