GB2246145A - Nickel-born alloy composite slidable surface - Google Patents
Nickel-born alloy composite slidable surface Download PDFInfo
- Publication number
- GB2246145A GB2246145A GB9109588A GB9109588A GB2246145A GB 2246145 A GB2246145 A GB 2246145A GB 9109588 A GB9109588 A GB 9109588A GB 9109588 A GB9109588 A GB 9109588A GB 2246145 A GB2246145 A GB 2246145A
- Authority
- GB
- United Kingdom
- Prior art keywords
- particles
- slidable
- nickel
- boron
- slidable member
- 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.)
- Withdrawn
Links
Classifications
-
- C—CHEMISTRY; METALLURGY
- C25—ELECTROLYTIC OR ELECTROPHORETIC PROCESSES; APPARATUS THEREFOR
- C25D—PROCESSES FOR THE ELECTROLYTIC OR ELECTROPHORETIC PRODUCTION OF COATINGS; ELECTROFORMING; APPARATUS THEREFOR
- C25D15/00—Electrolytic or electrophoretic production of coatings containing embedded materials, e.g. particles, whiskers, wires
- C25D15/02—Combined electrolytic and electrophoretic processes with charged materials
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
- F05C2203/00—Non-metallic inorganic materials
- F05C2203/04—Phosphor
Abstract
Slidable members, such as piston rings and cylinder liners made from cast iron or steel, have their slidable surfaces coated with a composite nickel-boron plate which is composed of a nickel alloy matrix containing 0.1 to 10 wt.% boron, and 5 to 30 vol.% of solid particles dispersed in the matrix. The particles are hard particles and/or solid-lubricant particles 0.1 to 10 mu m in diameter. The boron in the nickel alloy matrix increases hardness, and improves abrasion-, seizure- and corrosion-resistance.
Description
SLIDABLB MEMBER
The present invention relates to a slidable member having a slidable surface coated with a composite nickel plate.
Slidable members, such as piston rings and the like for use in an internal combustion engine, are subjected in service to a high load at high temperatures, so that they are mostly coated with a hard chrome plate to improve their anti-abrasion property. However, chrome plating is costly. The reasons for this are that it needs a long time for treatment and that it discharges pollutant water which must be purified at a high cost. Furthermore, the chrome plate is soon dfgraded in anti-abrasion, anti-seizure, and anti-corrosion when mounted in a high lead-content gasoline engine,
To solve the problems, such a composite plate is shown in JP B 56-18080 that has a nickel-phosphorus alloy matrix and hard particles of nitrides, carbides, and oxides dispersed in the matrix. The composite plate has good anti-abrasion, anti-seizure, and anti-corrosion properties when the particles are selected properly in sort, size, and amount, and available to coat the slidable surface of such a member as a cylinder liner and a piston ring.
However, the composite plate as described above becomes somewhat brittle when subjected to such a high load under high temperatures that dominate in an internal combustion engine during high speed running. The slidable member coated with the composite plate is still insufficient in anti-abrasion, anti-seizure, and anti-corrosion for use with the high speed engine,
It would therefore be desirable to be able to provide a slidable member coated with an improved composite plate that is sufficient in anti-abrasion, anti-seizure, and anti-corrosion for use with a high speed engine in which severe conditions dominate.
The present invention provides a slidable member which comprises a oetal surface coated with a composite plate which is compose of a nickel alloy matrix containing 0. 1 to 10%, by weight, of boron and 5 to 30X, by volume, of (e. g. hard and/or solid-lubricant) particles dispersed in the matrix.
The particles are selected to have a diameter not more than 10 Fm, preferably le s than 10 ym.
Boron, contained in the nickel alloy matrix, is effective to increase the hardness of plate and improve the plate in anti-abrasion, anti-seizure, and anti-corrosion. It is added by an amount of 0. 1 to 10X by weight. The reasons for this are that less than 0. 1% of boron has no effect and that more than 10% of boron oakes the plate rather brittle and has a negative effect on inpact strength and adhesion.
As hard particles dispersed in the nickel alloy matrix, one or more is selected from amont Sis4, SiC, NC. AI, Os, ZrO2, Cr2Os and the like. As solid lubricant particles, one or more is selected froc long sulfides, borides, and self-lubricating synthetic resins. In preference, the particles are of 0. 1 to 10 . diameter and dispersed in the matrix by an amount of 5 to 30X, by volume. hhen the particles are of less than 0. 1 FLm or dispersed in the matrix by an amount of less than 5X by volute, they may not improve the plate in anti-abrasion, When they are of more than 10 m diameter or dispersed in the matrix by an amont of sore than 30 X by volume, the plate may deteriorate in strength and give an abrasion to the other slidable member.
Advantages which may be achieved are that the plated slidable webers are superior both in anti-abrasion and in anti-scuffing and they are suitable for use with a high speed internal combustion engine in which dominate very severe conditions. The plated slidable member reduces the cost for production because it is available without beat-treatment or with heat-treatmsntat relatively low temperatures.
In theaccompanying drawings:
FIG. 1 is a graph illustrating the results of a hardness test before and after heat-treatoent ;
FIG. 2 is a graph illustrating the results of an abrasion test; and
FIG. 3 is a graph illustrating the results of a scuffing test.
The following are examples of the slidable member of the present invention, in which trioethylaoine-borane is called "TMAB".
BXAMPLBS: (1) Plating Condition texperature : 55 C pH : 3. 5 electric current density : 5A/doz (2) Bath Composition
Coaparison 1 : nickel sulfate 240 grams/liter nickel chloride 45 grams/liter boric acid 30 graos/liter silicon nitride 100 graws/liter (Si2N4, 0.7 m average diameter)
Comparison 2 : hypophosphorous acid 3. 0 grams/liter added to the composition of Comparaison 1
Example 1 : TMAB 6. 0 grams/liter added to the composition of Comparison 1
Example 2 : nickel sulfate 240 graos/liter nickel chloride 45 grams/liter
boric acid 30 grams/liter
boron nitride 100 grams/liter
(BN, 2. 0 m average diameter)
TMAB 6. 0 graos/liter Bxample 3 : TMAB 6. 6 graas/liter molybdenum disulfide 100 graos/liter (MoS2, 0,1 m average diameter)
added to the composition of Comparison 1
The respective composite plates were deposited fro the
Comparisons and Examples. The same hard plate can be obtained from the bath prepared by adding TMAB to the composition of Comparison 1 from which boric acid is removed. However, the bath desirably includes boric acid to maintain its useful life and stability.
HARDNBSS TEST :
The individual plates obtained from the five above-mentioned baths were tested with Micro Vickers
Hardness Tester before and after being subjected to one-hour heat-treatment at preselective temperatures. The test results are plotted in PIG, 1 The results show that the plates froo Comparisons 1 and 2 having no boron additives are insufficient in hardness without being heat-treated and that the plate from
Comparison 1 remarkably reduces its hardness when treated at temperatures of higher than 300 C. On the other hand, the plate from Bxample having boron additives has a sufficient hardness without being heat-treated and maintins its hardness after being heat-treated at temperatures of 300 to 350 C. This means that the addition of boron compound also improves the plate in heat-resistance The plate from Comparison 2 containing phosphorous additives is better than that from Comparison 1 containing no phosphorus additives. But, it is inferior in hardness to the plate from Example before being heat-treated This means that the bath containing the boron additives is more advantageous than the bath containing the phosphorus
additives to deposit a composite plate on the slidable
member. The sliding member plated in Comparisons would not
be used under severe conditions without heat-treated at
temperatures of 350 to 380 C The inventive member plat-ed
in Examples can be used under severe conditions without
being heat-treated or after heat-treated at a temperature of 300 C or less, resulting in an avantage that the plating
cost is reduced,
ABRASION TBST :
The slidable members plated in Comparisons 1 and 2 and the Exampleswere tested under an abrasion condition as shown in
Table 1. In Assoler tester, the test piece (18 an X 12 as X
6 mm) is fixed while the rotary contact piece is
doughnut-shaped with 40 on outer diameter, 16 mm inner
diameter, and 10 thickness, The plate on the test piece was
arranged to be in contact with the plate on the rotary piece
The test results are plotted in FIG. 2.
TABLB 1 : ABRASION TEST CONDITION tester AMSLER ABRASION TESTER oethod rotary piece contact half immersed
in oil and loaded rotary contact piece FC25 (HRB 98) lubricating oil 1030 oil temperature room temperature peripheral speed 0. 89 m# (500 rp) load 60 kg test time 3 h abrasion amount difference in level (JL m) zetsured by a contact profile meter
SCUFFING TEST :
The slidable webers obtained from Cozparison8 1 and 2 and Example were tested for anti-scuffing under a scuffing condition as shown in Table 2. The results are plotted in
PI6 3. It shows that the plate from the inventive bath. containing Ni-B-SiaN4 is superior in anti-scuffing to those from Comparisons 1 and 2 containing Ni-Si2N4 and Ni-P-Si. N4 TABLE 2 : SCUPFFING TEST CONDITION tester HIGH-SPEED FRICTIONAL ABRASION TBSTBR type rotary-disc flat-contact sliding-friction rethod suspending the supply of lubricating oil
after 20 minute breaking-in with 25 kg/ct'planar pressure,
entering test with 30 kg/cm2.
incresing the pressure by 10 kt/cwa, every 2 minute running until scuffing
occurs in which the final planar pressure
is determined as the limit. rotary disc made from FC aterial paired piece FC25 (HRB98) lubricating oil SAEt30 (50X) and white kerosene (50%) oil amont 0. 02 liter/rin oil texperature 50 C (inside tank) peripheral speed 3. 75 m/s (300 rp) From foregoing, the preferred slidable member has its slidable surface coated with a composite plate of the type having a nickel-boron alloy matrix and hard and/or solid-lubricant type particles dispersed in the matrix. The composite plate will not become brittle under a high load at high temperatures in which the conventional plate with a nickel-phosphorus alloy matrix becomes brittle, The slidable members of the invention, such as piston rings and cylinder liners made from cast iron or steel and coated with the composite nickel-boron plate, are superior both in anti-abrasion and in anti-scuffing and advantageously suitable for use with a high speed internal combustion engine in which dominate very severe conditions.
Claims (8)
- Claims:1. A slidable member comprising a slidable surface coated with a composite plate composed of a nickel alloy matrix containing 0.1 to 10 wt. % boron, and 5 to 30 vol. % solid particles with a diameter of not more than 10 pm dispersed in the matrix.
- 2. A slidable member as claimed in claim 1, wherein the particles have a diameter of 0.1 to 10 Jum.
- 3. A slidable member as claimed in claim 1 or 2, wherein the particles comprise hard particles.
- 4. A slidable member as claimed in claim 1 or 2, wherein the particles comprise solid-lubricant particles.
- 5. A slidable member as claimed in claim 1 or 2, wherein the particles comprise hard and solid-lubricant particles.
- 6. A slidable member as claimed in any preceding claim, wherein the amount of particles is not more than 10 vol. %.
- 7. A slidable member as claimed in any preceding claim, being a piston ring or a cylinder liner.
- 8. A slidable member substantially as described with reference to any of Examples 1 to 3.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP18804690A JPH03180491A (en) | 1989-08-11 | 1990-07-18 | Sliding member |
GB919106557A GB9106557D0 (en) | 1990-07-18 | 1991-03-27 | Slidable member |
Publications (2)
Publication Number | Publication Date |
---|---|
GB9109588D0 GB9109588D0 (en) | 1991-06-26 |
GB2246145A true GB2246145A (en) | 1992-01-22 |
Family
ID=26298644
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB9109588A Withdrawn GB2246145A (en) | 1990-07-18 | 1991-05-02 | Nickel-born alloy composite slidable surface |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2246145A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2253412A (en) * | 1991-02-20 | 1992-09-09 | T & N Technology Ltd | Wear resistant bearing overlay |
US5770323A (en) * | 1991-02-20 | 1998-06-23 | T & N Technology Limited | Bearings |
GB2348210A (en) * | 1999-03-26 | 2000-09-27 | Miba Gleitlager Ag | Electrodeposited alloy layer used as an overlay of a plain bearing |
WO2004097272A1 (en) * | 2003-04-28 | 2004-11-11 | Man B & W Diesel A/S | Piston for a large-size engine, and method for the production of a wear-resistant layer in such a piston |
US20090155479A1 (en) * | 2006-09-21 | 2009-06-18 | Inframat Corporation | Lubricant-hard-ductile nanocomposite coatings and methods of making |
US8104530B2 (en) | 2005-12-19 | 2012-01-31 | Siemens Aktiengesellschaft | Component of a steelworks, such as a continuous casting installation or a rolling mill, method for producing such a component and installation for creating or processing semifinished metallic products |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1200410A (en) * | 1967-09-09 | 1970-07-29 | Nsu Motorenwerke Ag | Process and apparatus for electro-deposition |
GB1382101A (en) * | 1971-01-25 | 1975-01-29 | Du Pont | Electroless plating |
US3936577A (en) * | 1971-12-15 | 1976-02-03 | E. I. Du Pont De Nemours & Company | Method for concomitant particulate diamond deposition in electroless plating, and the product thereof |
JPS5383938A (en) * | 1976-12-29 | 1978-07-24 | Suzuki Motor Co | Complex alloy plating method |
GB2014189A (en) * | 1977-12-21 | 1979-08-22 | Bristol Aerojet Ltd | Processes for the electrodeposition of composite coatings |
EP0288364A1 (en) * | 1987-04-17 | 1988-10-26 | Regie Nationale Des Usines Renault | Process for improving the interior wear resistance of an internal-combustion engine |
-
1991
- 1991-05-02 GB GB9109588A patent/GB2246145A/en not_active Withdrawn
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB1200410A (en) * | 1967-09-09 | 1970-07-29 | Nsu Motorenwerke Ag | Process and apparatus for electro-deposition |
GB1382101A (en) * | 1971-01-25 | 1975-01-29 | Du Pont | Electroless plating |
US3936577A (en) * | 1971-12-15 | 1976-02-03 | E. I. Du Pont De Nemours & Company | Method for concomitant particulate diamond deposition in electroless plating, and the product thereof |
JPS5383938A (en) * | 1976-12-29 | 1978-07-24 | Suzuki Motor Co | Complex alloy plating method |
GB2014189A (en) * | 1977-12-21 | 1979-08-22 | Bristol Aerojet Ltd | Processes for the electrodeposition of composite coatings |
EP0288364A1 (en) * | 1987-04-17 | 1988-10-26 | Regie Nationale Des Usines Renault | Process for improving the interior wear resistance of an internal-combustion engine |
Cited By (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2253412A (en) * | 1991-02-20 | 1992-09-09 | T & N Technology Ltd | Wear resistant bearing overlay |
GB2253412B (en) * | 1991-02-20 | 1995-07-05 | T & N Technology Ltd | Bearings |
US5770323A (en) * | 1991-02-20 | 1998-06-23 | T & N Technology Limited | Bearings |
GB2348210A (en) * | 1999-03-26 | 2000-09-27 | Miba Gleitlager Ag | Electrodeposited alloy layer used as an overlay of a plain bearing |
GB2348210B (en) * | 1999-03-26 | 2004-01-21 | Miba Gleitlager Ag | Electrodeposited alloy layer, in particular an overlay of a plain bearing |
WO2004097272A1 (en) * | 2003-04-28 | 2004-11-11 | Man B & W Diesel A/S | Piston for a large-size engine, and method for the production of a wear-resistant layer in such a piston |
CN100408891C (en) * | 2003-04-28 | 2008-08-06 | Manb&W柴油机公司 | Piston for a large-size engine, and method for the production of a wear-resistant layer in such a piston |
HRP20050931B1 (en) * | 2003-04-28 | 2013-03-31 | Man B & W Diesel A/S | Piston for a large-size engine, and method for the production of a wear-resistant layer in such a piston |
US8104530B2 (en) | 2005-12-19 | 2012-01-31 | Siemens Aktiengesellschaft | Component of a steelworks, such as a continuous casting installation or a rolling mill, method for producing such a component and installation for creating or processing semifinished metallic products |
US20090155479A1 (en) * | 2006-09-21 | 2009-06-18 | Inframat Corporation | Lubricant-hard-ductile nanocomposite coatings and methods of making |
US8541349B2 (en) * | 2006-09-21 | 2013-09-24 | Inframat Corporation | Lubricant-hard-ductile nanocomposite coatings and methods of making |
Also Published As
Publication number | Publication date |
---|---|
GB9109588D0 (en) | 1991-06-26 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
WAP | Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1) |