GB2109417A - Flame-spraying material - Google Patents
Flame-spraying material Download PDFInfo
- Publication number
- GB2109417A GB2109417A GB08232442A GB8232442A GB2109417A GB 2109417 A GB2109417 A GB 2109417A GB 08232442 A GB08232442 A GB 08232442A GB 8232442 A GB8232442 A GB 8232442A GB 2109417 A GB2109417 A GB 2109417A
- Authority
- GB
- United Kingdom
- Prior art keywords
- flame
- spraying
- mixture
- additive material
- particles
- 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
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
-
- 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
- B22F1/00—Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
- B22F1/09—Mixtures of metallic powders
-
- 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
- B22F1/00—Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
- B22F1/12—Metallic powder containing non-metallic particles
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)
Abstract
A boron-containing matrix alloy is mixed with an additive material of higher melting point, such as molybdenum, the particles of the additive material being spherical, in the grain size range from 20-150 mu m and constituting 30-80 percent by weight of the mixture. A protective layer or coating produced therefrom by flame-spraying, with simultaneous fusion, provides very good anti-friction properties with simultaneously a very high resistance to wear.
Description
SPECIFICATION
Flame-spraying material
The present invention relates to a flamespraying material which is in the form of a mixture of a pulverous boron-containing matrix alloy with a melting point below 1 0000C with particles of a metallic additive material having a melting point above 1 500 C.
Flame-spraying materials are already known, which are intended more especially for producing wear-resistant protective coatings on metallic substrates and which consist of a mixture of a boron-containing matrix alloy with additive materials, such as molybdenum, tungsten, tungsten carbide, etc.
Usually, the particles of the additive material are present in any arbitrary granule form, which may be irregular and more especially angular to flake-like and the grain size varies in the range below 20 ym.
The coatings are usually applied by plasma spraying or flame-spraying, with or without subsequent fusion.
However, it has been found that the wear resistance and the anti-friction properties of the usual coatings are not satisfactory and sometimes even the corresponding machine parts may be destroyed.
The present invention seeks to provide a flamespraying material of the type initially referred to, which permits the production of protective coatings with substantially improved properties as regards wear due to friction and sliding movements with metal-metal contact and consequently results in a longer life of the coated parts.
According to the invention, we provide flamespraying material in the form of a mixture of pulverous, boron-containing matrix alloy with a melting point lower than 1 0000C with particles of a metallic additive material with a melting point higher than 1 500 C, wherein the particles of the additive material are spherical, are in the grain size range from 20 to 1 50 ,um and the proportion of the additive material amounts to 30 to 80 percent by weight of the mixture. Preferably the proportion of the additive material amounts to 40 to 60 percent by weight of the mixture. A preferred additive material is molybdenum. Further preferred additive materials are tungsten, tungsten carbide or a mixture of molybdenum and/or tungsten and/or tungsten carbide.The invention also includes the use of a flame-spraying material as defined above for the production on a metallic substrate of a protective coating or layer which is resistant to metal-metal sliding friction stress, wherein the protective coating is applied by flamespraying of the material with simultaneous fusion on to the substrate. The invention also includes metallic parts or components which are coated in accordance with this process.
When a protective coating of the type as initially referred to is applied or melted on the surface of the particles of additive material, that is to say, at the boundary layer with respect to the matrix alloy, hard boride phases are formed, which lead to a strong embrittlement and, in operation, can even cause these particles to break away from the coating. This is more especially the case when the particles have sharp edges or are even of flake-like form, or the grain size of the particles is so small that, with the thermal coating process which is chosen, the hard boride phases completeiy permeate the incorporated particle or the edge portions thereof.
It has now been found that, by the use of spherical particles of relatively large diameter, i.e.
of 20-1 50 Mm, advantageously of 35-1 50 ,um, the formation of boride can be restricted to a thin surface layer of the particles and takes place very uniformly thereon, and that, in addition, by having a proportion of 30 to 80 and advantageously of 40 to 60 percent by weight of the additive material in the mixture, extremely good properties as regards wear and sliding properties can be produced.
The accompanying Figure shows the photomicrngraphic of the ground surface of a protective coating according to the invention, which consists of spheroidal molybdenum particles 1 with a grain size of 45-88 ym in a matrix alloy 2 of, in percent by weight, 1 SB, 2.4Si, 2Fe, 12Cr, the remainder Ni. A thin molybdenum boride layer 3 is to be seen on the pheriphery of the molybdenum particles.
The matrix alloy powder had a grain size in the range of 20-125 Mm and the proportion of the
molybdenum particles amounted to 30 percent by weight of the mixture.
The coating was applied in a layer with a
thickness of 3 mm and with simultaneous fusion to a base member consisting of steel of the type CrMo4, using the flame-spraying process known
under the Trade Name "EUTALLOY process" of
CASTOLIN S.A. It was shown that the coating is
capable of being used, as regards sliding friction,
up to a pressure of 5 kg/mm2, whereas a breaking
away of the molybdenum particles already occurs with a frictional pressure of 1 kg/mm2 when using conventional protective coatings of similar types.
It was found that particularly good results are obtained when flame-spraying with simultaneous fusion, since the time of contact of the particles of
added material in the molten matrix alloy is in this
case comparatively short, as a consequence of which there is established a very weak and uniform diffusion of the boron on the surface of the particles, with formation of boride phases.
With a subsequent fusion procedure, this contact time is substantially longer, whereas with a layer or coating produced by plasma spraying or flame spraying without fusion, there is established a less satisfactory metallic bonding thereof with the base
material and also between the matrix alloy and the
incorporated particles of the additive material.
Molybdenum is the preferred additive material
for most uses, for which good anti-friction
properties are required. However, also tungsten,
tungsten carbide or mixtures of various additive
materials can be used in the flame-spraying
materials according to the invention.
Advantageously employed as matrix alloys are
alloys having the following compositions, in
percentages by weight:
(1) 1-4 B 1.5-5 Si 0--10 Fe 0--20 Cr 0--10 W and/or Mo 0--5 Cu
remainder Ni
(2) 0.5-3.5 B 0.5-4.5 Si 0--5 Fe 5-30 Cr 0--12 W and/or Mo 30-40 Ni
remainder Co
It is apparent from the foregoing that the invention makes possible the formation on metallic substrates of a layer or coating with very good anti-friction properties and, at the same time, very high resistance to wear, more especially on machine parts which are subjected to severe stressing due to sliding friction in contact with metallic contacting members, as a result of which the effective life of the said parts can be substantially lengthened.
Claims (11)
1. Flame-spraying material in the form of a mixture of a pulverous, boron-containing matrix alloy with a melting point lower than 1 0000C with particles of a metallic additive material with a melting point higher than 1 5000 C, wherein the particles of the additive material are spherical, are in the grain size range from 20 to 1 50 ssm and the proportion of the additive material amounts to 30 to 80 percent by weight of the mixture.
2. Flame-spraying material according to claim 1, wherein the proportion of the additive material amounts to 40 to 60 percent by weight of the mixture.
3. Flame-spraying material according to claim 1 or 2, wherein the matrix alloy has the following composition, in percent by weight:
1-4 B 1.5-5 Si 0--10 Fe 0--20 Cr 0--10 W and/or Mo 0--5 Cu
remainder Ni
4. Flame-spraying material according to claim 1 or 2, wherein the matrix alloy has the following composition, in percent by weight: 0.5-3.5 B 0.5-4.5 Si 0--5 Fe 5-30 Cr 0--12 W and/or Mo 30-40 Ni
remainder Co
5. Flame-spraying material according to any one of the preceding claims, wherein molybdenum is used as an additive material.
6. Flame-spraying material according to any one of the preceding claims, wherein tungsten, tungsten carbide or a mixture of molybdenum and/or tungsten and/or tungsten carbide are used as additive material.
7. Use of a flame-spraying material according to any one of the preceding claims for the production on a metallic substrate of a protective coating or layer which is resistant to metal-metal sliding friction stress, wherein the protective coating is applied by flame-spraying of the material with simultaneous fusion on to the substrate.
8. Metallic components, which are provided with a protective coating produced in accordance with claim 7.
9. Flame-spraying material according to claim 1, substantially as described herein.
10. Flame-spraying material substantially as described herein with reference to the drawing.
11. A process for applying flame-spraying substantially as described herein.
1 2. Metallic components, provided with a coating derived from the material of any one of claims 1 to 6,9 or 10.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH7341/81A CH648357A5 (en) | 1981-11-16 | 1981-11-16 | FLAME INJECTION MATERIAL. |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2109417A true GB2109417A (en) | 1983-06-02 |
GB2109417B GB2109417B (en) | 1985-07-03 |
Family
ID=4323605
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB08232442A Expired GB2109417B (en) | 1981-11-16 | 1982-11-12 | Flame-spraying material |
Country Status (4)
Country | Link |
---|---|
CH (1) | CH648357A5 (en) |
DE (1) | DE3241377A1 (en) |
FR (1) | FR2516550B1 (en) |
GB (1) | GB2109417B (en) |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE3718779A1 (en) * | 1987-06-04 | 1988-12-22 | Krauss Maffei Ag | SNAIL OD. DGL. MACHINE PART FOR PLASTIC MACHINERY |
GB2310866A (en) * | 1996-03-05 | 1997-09-10 | Sprayforming Dev Ltd | Filling porosity or voids in articles formed by spray deposition |
EP1788104A1 (en) * | 2005-11-22 | 2007-05-23 | MEC Holding GmbH | Material for producing parts or coatings adapted for high wear and friction-intensive applications, method for producing such a material and a torque-reduction device for use in a drill string made from the material |
EP1857204A1 (en) * | 2006-05-17 | 2007-11-21 | MEC Holding GmbH | Nonmagnetic material for producing parts or coatings adapted for high wear and corrosion intensive applications, nonmagnetic drill string component, and method for the manufacture thereof |
GB2470459A (en) * | 2009-04-29 | 2010-11-24 | Reedhycalog L P | Tungsten carbide based cermets with high thermal conductivities |
US8535408B2 (en) | 2009-04-29 | 2013-09-17 | Reedhycalog, L.P. | High thermal conductivity hardfacing |
EP2808107A1 (en) * | 2013-05-31 | 2014-12-03 | Sandvik Intellectual Property AB | A method for manufacturing a MMC component |
CN107058807A (en) * | 2016-12-31 | 2017-08-18 | 天津滨海雷克斯激光科技发展有限公司 | Sprayed on material and spraying method and its application for cigarette gun of cigarette making machine |
CN115740462A (en) * | 2022-09-28 | 2023-03-07 | 铜陵有色金属集团股份有限公司 | Ball mill lining plate with high wear resistance and preparation process thereof |
Families Citing this family (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH652147A5 (en) * | 1983-02-23 | 1985-10-31 | Castolin Sa | POWDER MATERIAL FOR THERMAL SPRAYING. |
DE3709126A1 (en) * | 1987-03-23 | 1988-10-13 | Butzbacher Weichenbau Gmbh | Interacting track parts |
US4830934A (en) * | 1987-06-01 | 1989-05-16 | General Electric Company | Alloy powder mixture for treating alloys |
EP0818549B1 (en) * | 1996-06-25 | 2004-02-04 | Castolin S.A. | Nickel-based material in powder- or wireform for coating as well as the processes thereof |
DE10120326B4 (en) * | 2001-04-26 | 2009-05-20 | Knorr-Bremse Systeme für Nutzfahrzeuge GmbH | Brake drum and method for its manufacture |
DE102004052673B4 (en) * | 2004-10-29 | 2016-07-07 | Knorr-Bremse Systeme für Nutzfahrzeuge GmbH | Low-wear brake disk or brake drum and method for the production thereof |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE1185034B (en) * | 1958-04-24 | 1965-01-07 | Metco Inc | Metal powder mixture containing metal carbide for the production of coatings on metal bodies by spray welding |
DE1259170B (en) * | 1962-09-22 | 1968-01-18 | Deutsche Edelstahlwerke Ag | Process for the production of coatings by flame or plasma spraying |
US3455019A (en) * | 1964-05-11 | 1969-07-15 | Eutectic Welding Alloys | Method for producing carbide containing materials |
FR1395274A (en) * | 1964-05-13 | 1965-04-09 | Metco Inc | High temperature flame sprayable powder and method of spraying this powder |
US3407057A (en) * | 1965-10-23 | 1968-10-22 | American Metal Climax Inc | Molybdenum powder for use in spray coating |
US3617358A (en) * | 1967-09-29 | 1971-11-02 | Metco Inc | Flame spray powder and process |
US3837817A (en) * | 1972-10-18 | 1974-09-24 | Nippon Piston Ring Co Ltd | Sliding member having a spray-coated layer |
US3909241A (en) * | 1973-12-17 | 1975-09-30 | Gte Sylvania Inc | Process for producing free flowing powder and product |
US4004042A (en) * | 1975-03-07 | 1977-01-18 | Sirius Corporation | Method for applying a wear and impact resistant coating |
US4075392A (en) * | 1976-09-30 | 1978-02-21 | Eutectic Corporation | Alloy-coated ferrous metal substrate |
-
1981
- 1981-11-16 CH CH7341/81A patent/CH648357A5/en not_active IP Right Cessation
-
1982
- 1982-11-09 DE DE19823241377 patent/DE3241377A1/en active Granted
- 1982-11-12 GB GB08232442A patent/GB2109417B/en not_active Expired
- 1982-11-15 FR FR8219077A patent/FR2516550B1/en not_active Expired
Cited By (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4949836A (en) * | 1987-06-04 | 1990-08-21 | Krauss-Maffei A.G. | Screw with wear resistant surface |
DE3718779A1 (en) * | 1987-06-04 | 1988-12-22 | Krauss Maffei Ag | SNAIL OD. DGL. MACHINE PART FOR PLASTIC MACHINERY |
GB2310866A (en) * | 1996-03-05 | 1997-09-10 | Sprayforming Dev Ltd | Filling porosity or voids in articles formed by spray deposition |
NO342355B1 (en) * | 2005-11-22 | 2018-05-14 | Mec Holding Gmbh | Material for the manufacture of parts or coatings adapted to high wear and friction-intensive applications, a method of making such material and a torque-reducing equipment for use in a drill string made of the material |
EP1788104A1 (en) * | 2005-11-22 | 2007-05-23 | MEC Holding GmbH | Material for producing parts or coatings adapted for high wear and friction-intensive applications, method for producing such a material and a torque-reduction device for use in a drill string made from the material |
WO2007060088A1 (en) * | 2005-11-22 | 2007-05-31 | Mec Holding Gmbh | Material for producing parts or coatings adapted for high wear and friction-intensive applications, method for producing such a material and a torque-reduction device for use in a drill string made from the material |
EP1857204A1 (en) * | 2006-05-17 | 2007-11-21 | MEC Holding GmbH | Nonmagnetic material for producing parts or coatings adapted for high wear and corrosion intensive applications, nonmagnetic drill string component, and method for the manufacture thereof |
WO2007132020A1 (en) * | 2006-05-17 | 2007-11-22 | Mec Holding Gmbh | Nonmagnetic material for producing parts or coatings adapted for high wear and corrosion intensive applications, nonmagnetic drill string component, and method for the manufacture thereof |
NO343525B1 (en) * | 2006-05-17 | 2019-04-01 | Mec Holding Gmbh | Non-magnetic material for the manufacture of parts and coatings intended for high wear and corrosion-intensive applications, non-magnetic drill string components, and methods of making them |
US8460604B2 (en) | 2006-05-17 | 2013-06-11 | Mec Holding Gmbh | Nonmagnetic material for producing parts or coatings adapted for high wear and corrosion intensive applications, nonmagnetic drill string component, and method for the manufacture thereof |
GB2470459B (en) * | 2009-04-29 | 2011-12-14 | Reedhycalog L P | High thermal conductivity hardfacing for drilling applications |
US8535408B2 (en) | 2009-04-29 | 2013-09-17 | Reedhycalog, L.P. | High thermal conductivity hardfacing |
GB2470459A (en) * | 2009-04-29 | 2010-11-24 | Reedhycalog L P | Tungsten carbide based cermets with high thermal conductivities |
EP2808107A1 (en) * | 2013-05-31 | 2014-12-03 | Sandvik Intellectual Property AB | A method for manufacturing a MMC component |
CN107058807A (en) * | 2016-12-31 | 2017-08-18 | 天津滨海雷克斯激光科技发展有限公司 | Sprayed on material and spraying method and its application for cigarette gun of cigarette making machine |
CN115740462A (en) * | 2022-09-28 | 2023-03-07 | 铜陵有色金属集团股份有限公司 | Ball mill lining plate with high wear resistance and preparation process thereof |
Also Published As
Publication number | Publication date |
---|---|
DE3241377A1 (en) | 1983-05-26 |
DE3241377C2 (en) | 1991-10-31 |
FR2516550B1 (en) | 1987-06-26 |
CH648357A5 (en) | 1985-03-15 |
FR2516550A1 (en) | 1983-05-20 |
GB2109417B (en) | 1985-07-03 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PCNP | Patent ceased through non-payment of renewal fee |
Effective date: 19941112 |