EP0035377A1 - Alliages pour l'obtention de couches de liaison par projection thermique - Google Patents
Alliages pour l'obtention de couches de liaison par projection thermique Download PDFInfo
- Publication number
- EP0035377A1 EP0035377A1 EP81300805A EP81300805A EP0035377A1 EP 0035377 A1 EP0035377 A1 EP 0035377A1 EP 81300805 A EP81300805 A EP 81300805A EP 81300805 A EP81300805 A EP 81300805A EP 0035377 A1 EP0035377 A1 EP 0035377A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- bond
- coat
- aluminium
- alloy
- nickel
- 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.)
- Ceased
Links
- 229910045601 alloy Inorganic materials 0.000 title claims abstract description 41
- 239000000956 alloy Substances 0.000 title claims abstract description 41
- 238000000576 coating method Methods 0.000 title abstract description 25
- 239000011248 coating agent Substances 0.000 title abstract description 16
- 238000007751 thermal spraying Methods 0.000 title description 3
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims abstract description 50
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 26
- 239000004411 aluminium Substances 0.000 claims abstract description 25
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 25
- 229910052759 nickel Inorganic materials 0.000 claims abstract description 23
- 239000000758 substrate Substances 0.000 claims abstract description 22
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims abstract description 18
- 229910052804 chromium Inorganic materials 0.000 claims abstract description 18
- 239000011651 chromium Substances 0.000 claims abstract description 18
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 claims abstract description 15
- 229910052802 copper Inorganic materials 0.000 claims abstract description 15
- 239000010949 copper Substances 0.000 claims abstract description 15
- 239000012535 impurity Substances 0.000 claims abstract description 15
- 229910052710 silicon Inorganic materials 0.000 claims abstract description 15
- 239000010703 silicon Substances 0.000 claims abstract description 15
- 239000000843 powder Substances 0.000 claims abstract description 13
- 229910052751 metal Inorganic materials 0.000 claims abstract description 12
- 239000002184 metal Substances 0.000 claims abstract description 12
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims abstract description 10
- 238000010285 flame spraying Methods 0.000 claims abstract description 6
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 claims abstract description 5
- 229910052796 boron Inorganic materials 0.000 claims abstract description 5
- 229910052742 iron Inorganic materials 0.000 claims abstract description 5
- 238000005524 ceramic coating Methods 0.000 abstract description 2
- 239000000463 material Substances 0.000 description 13
- 239000000203 mixture Substances 0.000 description 10
- 238000012360 testing method Methods 0.000 description 8
- PNEYBMLMFCGWSK-UHFFFAOYSA-N aluminium oxide Inorganic materials [O-2].[O-2].[O-2].[Al+3].[Al+3] PNEYBMLMFCGWSK-UHFFFAOYSA-N 0.000 description 7
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 6
- 238000005507 spraying Methods 0.000 description 6
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N Titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 5
- 239000011733 molybdenum Substances 0.000 description 5
- 229910052750 molybdenum Inorganic materials 0.000 description 5
- NPXOKRUENSOPAO-UHFFFAOYSA-N Raney nickel Chemical compound [Al].[Ni] NPXOKRUENSOPAO-UHFFFAOYSA-N 0.000 description 3
- 229910000831 Steel Inorganic materials 0.000 description 3
- 238000005422 blasting Methods 0.000 description 3
- 239000002131 composite material Substances 0.000 description 3
- 238000003754 machining Methods 0.000 description 3
- 238000007788 roughening Methods 0.000 description 3
- 239000010959 steel Substances 0.000 description 3
- 229910000838 Al alloy Inorganic materials 0.000 description 2
- 229910000990 Ni alloy Inorganic materials 0.000 description 2
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- FAPWRFPIFSIZLT-UHFFFAOYSA-M Sodium chloride Chemical compound [Na+].[Cl-] FAPWRFPIFSIZLT-UHFFFAOYSA-M 0.000 description 2
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 239000001301 oxygen Substances 0.000 description 2
- 229910052760 oxygen Inorganic materials 0.000 description 2
- 239000002245 particle Substances 0.000 description 2
- 239000007921 spray Substances 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910000881 Cu alloy Inorganic materials 0.000 description 1
- 230000001464 adherent effect Effects 0.000 description 1
- 238000005275 alloying Methods 0.000 description 1
- YYCNOHYMCOXPPJ-UHFFFAOYSA-N alumane;nickel Chemical class [AlH3].[Ni] YYCNOHYMCOXPPJ-UHFFFAOYSA-N 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 239000000919 ceramic Substances 0.000 description 1
- 238000009833 condensation Methods 0.000 description 1
- 230000005494 condensation Effects 0.000 description 1
- 238000005238 degreasing Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000007654 immersion Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000007935 neutral effect Effects 0.000 description 1
- 229910000907 nickel aluminide Inorganic materials 0.000 description 1
- 239000003960 organic solvent Substances 0.000 description 1
- 239000012254 powdered material Substances 0.000 description 1
- 239000002994 raw material Substances 0.000 description 1
- 235000012239 silicon dioxide Nutrition 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- 239000011780 sodium chloride Substances 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 238000010301 surface-oxidation reaction Methods 0.000 description 1
- 239000004408 titanium dioxide Substances 0.000 description 1
- OGIDPMRJRNCKJF-UHFFFAOYSA-N titanium oxide Inorganic materials [Ti]=O OGIDPMRJRNCKJF-UHFFFAOYSA-N 0.000 description 1
- 230000004580 weight loss Effects 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
- C23C4/00—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge
- C23C4/04—Coating by spraying the coating material in the molten state, e.g. by flame, plasma or electric discharge characterised by the coating material
- C23C4/06—Metallic material
- C23C4/067—Metallic material containing free particles of non-metal elements, e.g. carbon, silicon, boron, phosphorus or arsenic
Definitions
- This invention relates to bond-coating alloys for thermal spraying and particularly to an alloy suitable for flame spraying in powder form onto a metal substrate to provide a bond-coat thereon.
- bond-coats are required if the substrate is in the form of a thin section which would be distorted by grit-blasting or rough-machining.
- Such bond-coats bond metallurgically to the substrate and are capable of repeated coating applications although they need be used in all cases for repeated coating applications. In this aspect they differ from so-called "self-bonding coatings" which are normally intended as single deposit coatings which show some measure of metallurgical bonding to a metallic substrate but are not necessarily suitable for use as bond-coats on metal substrates such as hardened steels. This specification is only concerned with bond-coats.
- Such a bond- coat, sprayed on as a thin adherent layer, provides attachment for a subsequent, thicker, sprayed deposit .
- the bond-coat material must be capable of adhering with sufficient strength to a, smooth machined surface of a substrate and this conventionally is achieved by ensuring that the temperature of the bond-coat particles issuing from the spraying apparatus remains high until they meet the substrate surface.
- the additional heat necessary may be provided by an exothermic reaction between the bond coat material and oxygen in the spray flame in the case, for example, of an exothermic bond coat material such as molybdenum.
- molybdenum When molybdenum is sprayed from a wire-spray gun it reacts with oxygen either in the air or in the flame to form a volatile oxide.
- Composite materials containing or comprising nickel and aluminium, such as nickel coated aluminium powders, agglomerated nickel/aluminium powders and composite wires have been proposed for use as bond-coat materials but such materials are costly and/or in short supply. These materials, when sprayed, react to form nickel aluminide with the evolution of heat sufficient to promote metallurgical bonding at the interface. Powdered materials such as the above have been used also in association with other alloy powders to provide "self bonding" coatings, but such mixtures are not normally advocated as bond-coats.
- the invention provides an alloy, suitable for flame spraying in powder form onto a metal substrate to provide a bond-coat thereon, which contains, by weight, from 2 to 30% aluminium, from 2 to 25% chromium, from 0 to 8% silicon, from 0 to 4% boron and from 0 to 6% iron, the balance, apart from impurities, being copper and/or nickel.
- the alloy contains from 2 to 15% aluminium.
- the alloy contains not less than 5% chromium. More preferably the alloy contains 6.0% aluminium, 8.5% chromium, 4.6% silicon and 49.0% copper, the balance, apart from impurities, being nickel.
- a preferred alloy containing, by weight, 5% aluminium, 10% chromium, 5% silicon, and 45% copper, the balance, apart from impurities, being nickel.
- a further preferred alloy contains, by weight, 8% aluminium, 4% chromium, 2% silicon, and 15% nickel, the balance, apart from impurities, being copper.
- bond-coats were tested by means of a scratch test in which the bond-coatings where applied to steel samples approximately 50 mm x 50 mm x 10 mm in size and adhesion of the bond-coat was judged by observing the effects of scribing, down to the substrate, two lines approximately 3 mm apart.
- the test samples were used in the as machined condition after degreasing with an organic solvent immediately prior to spraying. The samples were preheated only sufficiently to' prevent condensation of moisture on their surfaces and each material was sprayed in a rapid series of overlapping passes, two layers being applied, with the second being at right angles to the first to give a deposit thickness of approximately 0.25 mm.
- Molybdenum powder sprayed with an oxidising flame produced a bond-coat with good cohesion and adhesion but spraying with a neutral or reducing flame gave a coating having virtually no adhesion.
- Nickel aluminium composite proprietary powders were flame sprayed to produce bond-coatings with good cohesion and adhesion whereas nickel aluminium pre-alloyed powders when flame sprayed gave a coating with good cohesion but reduced adhesion.
- a 90% copper, 10% aluminium alloy in pre-alloyed form provided a flame sprayed coating with adequate adhesion and best results were obtained with an oxidising flame.
- Bond-coatings were then produced from an alloy of the invention in powder form. Satisfactory bonding and adhesion characteristics were obtained with alloys containing, by weight, from 2 to 30%, preferably from 2 to 15%, aluminium, from 2 to 25%, preferably from 5 to 25%, chromium, from 0 to 8% silicon, from 0 to 4% boron and 0 to 6% iron, the balance, apart from impurities, being copper and/or nickel.
- a further preferred alloy composition according to the invention contained 6.0% aluminium, 8.5% chromium, 4.5% silicon and 49.5% copper, the balance, apart from impurities, being nickel.
- Such alloys according to the invention produced bond-coatings with bond strengths comparable to that of unreacted nickel-aluminium composites but superior to that of well sprayed molybdenum or aluminium bronze materials.
- An alloy according to the invention having the nominal composition given in the foregoing example, was used as a bond-coat for applying a coating of COLMONOY C290 (Trade Mark) having a nominal composition, by weight, of 13.3% chromium, 1.5% boron, 2.5% silicon, 0.4% carbon 37.0% nickel, with the balance, apart from impurities, being iron, to electric motor shafts and to an hydraulic ram.
- the shafts were satisfactorily repaired in this way.
- the ram was rough threaded to increase the coating contact area, sprayed with the bond-coat of the alloy of the invention to a thickness of 0.1 mm en which a further coating of the COLMONOY C 290 alloy was built up to a thickness sufficient to machine back to the original ram size.
- bond-coats produced from an alloy according to the invention possess very good properties of adhesion to the substrate, sufficient even to withstand the severe test of subsequent machining. These good adhesion properties enable a bond-coat produced from an alloy of the invention to be used for reclamation of areas of components which have been mismachined to dimensions below the minimum required dimensions. Such areas may be bond-coated and subsequently machined or ground to the required dimensions without the need for roughening or undercutting of the substrate area to be reclaimed.
- alloys according to the present invention may be used as bond-coats for the application of ceramic deposits, such as alumina (nominal composition by weight, 94.0% aluminium oxide, 2.5% titanium oxide, 2.0% silicon dioxide, plus usual impurities) or TITANIA (Trade Mark) (nominal composition, by weight, 50% aluminium oxide, 50% titanium dioxide) to a metal substrate.
- ceramic deposits such as alumina (nominal composition by weight, 94.0% aluminium oxide, 2.5% titanium oxide, 2.0% silicon dioxide, plus usual impurities) or TITANIA (Trade Mark) (nominal composition, by weight, 50% aluminium oxide, 50% titanium dioxide) to a metal substrate.
- TITANIA Trade Mark
- the bond-coat may be applied directly onto a machined and degreased substrate without grit-blasting being necessary.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Plasma & Fusion (AREA)
- Chemical Kinetics & Catalysis (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Coating By Spraying Or Casting (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB8006763 | 1980-02-28 | ||
| GB8006763 | 1980-02-28 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| EP0035377A1 true EP0035377A1 (fr) | 1981-09-09 |
Family
ID=10511747
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| EP81300805A Ceased EP0035377A1 (fr) | 1980-02-28 | 1981-02-26 | Alliages pour l'obtention de couches de liaison par projection thermique |
Country Status (1)
| Country | Link |
|---|---|
| EP (1) | EP0035377A1 (fr) |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3212512A1 (de) * | 1981-04-06 | 1982-11-04 | Eutectic Corp., 11358 Flushing, N.Y. | Frei fliessendes und selbst bindefaehiges flammspruehpulver |
| DE3212513A1 (de) * | 1981-04-06 | 1982-12-23 | Eutectic Corp., 11358 Flushing, N.Y. | Flammspritzpulver und dessen herstellung |
| EP0081170A3 (en) * | 1981-12-05 | 1984-09-26 | Bbc Aktiengesellschaft Brown, Boveri & Cie. | High-temperature protective coating |
| DE19900942A1 (de) * | 1999-01-13 | 2000-07-20 | Man B & W Diesel As | Verfahren zur Erzeugung eines Schutzbelags sowie Maschine mit wenigstens einem mit einem Schutzbelag versehenen Bauteil |
| RU2161211C1 (ru) * | 2000-01-12 | 2000-12-27 | Волгоградский государственный технический университет | Способ обработки поверхностей трения |
| WO2002058927A1 (fr) * | 2001-01-25 | 2002-08-01 | Jimmie Brooks Bolton | Procedes d'application d'un materiau reducteur d'usure sur des raccords de tige |
| US6428858B1 (en) * | 2001-01-25 | 2002-08-06 | Jimmie Brooks Bolton | Wire for thermal spraying system |
| DE19858913B4 (de) * | 1998-12-19 | 2004-01-15 | Mtu Aero Engines Gmbh | Schutzschicht |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4019875A (en) * | 1973-07-06 | 1977-04-26 | Metco, Inc. | Aluminum-coated nickel or cobalt core flame spray materials |
-
1981
- 1981-02-26 EP EP81300805A patent/EP0035377A1/fr not_active Ceased
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4019875A (en) * | 1973-07-06 | 1977-04-26 | Metco, Inc. | Aluminum-coated nickel or cobalt core flame spray materials |
Non-Patent Citations (1)
| Title |
|---|
| Thin Solid Films, Vol. 53, 1978 Lausanne (CH) I. KVERNES et al.: "Use of Corrosion-Resistant Plasma-Sprayed Coatings in Diesel Engines", pages 259-269 * Table 1, sample GA-B, 10 * * |
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3212512A1 (de) * | 1981-04-06 | 1982-11-04 | Eutectic Corp., 11358 Flushing, N.Y. | Frei fliessendes und selbst bindefaehiges flammspruehpulver |
| DE3212513A1 (de) * | 1981-04-06 | 1982-12-23 | Eutectic Corp., 11358 Flushing, N.Y. | Flammspritzpulver und dessen herstellung |
| EP0081170A3 (en) * | 1981-12-05 | 1984-09-26 | Bbc Aktiengesellschaft Brown, Boveri & Cie. | High-temperature protective coating |
| DE19858913B4 (de) * | 1998-12-19 | 2004-01-15 | Mtu Aero Engines Gmbh | Schutzschicht |
| DE19900942A1 (de) * | 1999-01-13 | 2000-07-20 | Man B & W Diesel As | Verfahren zur Erzeugung eines Schutzbelags sowie Maschine mit wenigstens einem mit einem Schutzbelag versehenen Bauteil |
| DE19900942C2 (de) * | 1999-01-13 | 2003-04-10 | Man B & W Diesel As Kopenhagen | Verfahren zur Erzeugung eines Schutzbelags sowie Maschine mit wenigstens einem derartigen Schutzbelag |
| RU2161211C1 (ru) * | 2000-01-12 | 2000-12-27 | Волгоградский государственный технический университет | Способ обработки поверхностей трения |
| WO2002058927A1 (fr) * | 2001-01-25 | 2002-08-01 | Jimmie Brooks Bolton | Procedes d'application d'un materiau reducteur d'usure sur des raccords de tige |
| US6428858B1 (en) * | 2001-01-25 | 2002-08-06 | Jimmie Brooks Bolton | Wire for thermal spraying system |
| US6861612B2 (en) | 2001-01-25 | 2005-03-01 | Jimmie Brooks Bolton | Methods for using a laser beam to apply wear-reducing material to tool joints |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| PUAI | Public reference made under article 153(3) epc to a published international application that has entered the european phase |
Free format text: ORIGINAL CODE: 0009012 |
|
| AK | Designated contracting states |
Designated state(s): DE FR IT |
|
| 17P | Request for examination filed |
Effective date: 19820303 |
|
| RAP1 | Party data changed (applicant data changed or rights of an application transferred) |
Owner name: WALL COLMONOY LIMITED |
|
| STAA | Information on the status of an ep patent application or granted ep patent |
Free format text: STATUS: THE APPLICATION HAS BEEN REFUSED |
|
| 18R | Application refused |
Effective date: 19840603 |
|
| RIN1 | Information on inventor provided before grant (corrected) |
Inventor name: BELL, GERALD ROBERT |