Title of Invention


Abstract The invention relates to the use of lead-free sliding layers in the laminated composite materials for slide bearings or bushes. According to the invention, the laminated composite material comprises a support layer, an antifriction layer (.Y) produced from a copper alloy or an aluminum alloy, an intermediate nickel layer (2) having a thickness >4 um and a sliding layer (1 I consisting of approximately 0 to 20 % by weight of capper and/or silver and the remainder tin. The sliding layer is electrodeposited from a mcthiysulfonic acid electrolyte.
Full Text Composite multilayer material, production and use
The invention relates to a composite multilayer material, in particular for plain bearings or bushings, having a backing layer, a bearing metal layer of a copper alloy or an aluminum alloy, a nickel intermediate layer and an overlay. In addition, the invention relates to uses for the composite multilayer material.
Conventional composite multilayer materials with the structure comprising steel backing as backing layer, lead-bronze as bearing metal layer and overlay of lead-tin-copper, as described for example in Glyco-Ingenieurberichte 1/91 (Glyco Engineering Reports 1/91), have proven themselves as a result of their high reliability and mechanical load carrying capacity. In. such a structure, the overlay is electrodeposited. Such an overlay is a multifunctional layer, in which foreign particles may be embedded, which serves as corrosion protection, which exhibits emergency running characteristics and which is particularly suitable for runninq-in or mutual conforming of the sliding partners.
The bearing metal layer also exhibits adequate emergency running characteristics, in case the overlay is completely worn away at least in places.
Conventional composite multilayer materials comprise a lead-based overlay, a common alloy being for example PbSnlOCu2. Such overlays exhibit low hardnesses of around 12 - 15 H.V (Vickers Hardness) , for which reason they have good embedding properties and are in

For reasons of industrial safety and environmental
protection, ;'.t js nonetheless desirable to replace the
lead, which is a heavy metal, with other suitable
One approach is to use hard, layers as overlays in heavily loaded bearing systems. For example, aluminum-tin layers with hardnesses of around 80 HV arc deposited using PVD (physical vapor deposition) methods. These are lead-free, but are very expensive to produce. Such bearings are highly wear-resistant, but they exhibit almost no embeddability and are therefore generally combined with soft, lead-containing layers as a counter-shell. However, it is also desirable to replace the lead, in counter-shells with other materials.
Attempts have been made to use pure tin as a sliding surface. With a hardness of roughly 10 HV, however, pure tin is even softer than the conventional lead alloys and is therefore incapable of absorbing the loads which arise for example in crankshaft main bearings and connecting rod bearings.
DE 197 28 777 Al describes a composite multilayer material for sliding elements, the overlay of which consists of a lead-free alloy comprising tin and copper, wherein the copper content amounts to 3 - 20 wt.% and the tin content to 70 - 97 wt.%. The addition of copper increases the hardness of the overlay relative to pure tin. This overlay is electrodeposxted by means of a, methylsulfonic acid electrolyte with grain refining additives. The overlay produced in this way has the chsracteristx.cs of ternary lead-based overlays. In order further to improve wear resistance, DS 197 28 777 Al

ac'dit iop.a My proposes providing hard material particles dispersed in the electrolyte bath, these being incorporated into the layer. However, this is associated with additional effort and cost. Between the bearing metal and the overlay it is possible to provide a 1 - 3 pm thick nickel layer together with a 2 - 10 pm thick nicxel-tin layer as diffusion barrier layer.
DE 191 54 221 Al discloses a composite multilayer material with a.n overlay comprising 3-30 wt.% copper, 60 - 97 wt.% tin and G.5 - 10 wt.% cobalt. In this way, the mechanical load carrying capacity is further increased and embrittlement of the bonding layer between overlay and nickel diffusion barrier layer is prevented. The cobalt reduces the tendency of the tin to diffuse towards the nictcel. The addition of cobalt to the alloy, however, makes the electrodeposition process more complex, which reduces process reliability. Furthermore, as in DE 191 28 777 Al the 1 - 3 urn thick nickel layer may be combined with a 2 - 10 um thick nickel-tin layer
as diffusion barrier.
EP 1 113 180 A2 describes a composite multilayer material for pJain bearings, whose overlay has a tin matrix into which tin-copper particles are Incorporated, said particles consisting of 39 - 55 wt.I copper with the rest being tin. A characteristic feature of the composite multilayer material, is, in addition, that not only is an intermediate layer of nickel of a thickness of 1 - 4 y.m provided, but also a second 2 - 7 pm thick intermediate layer of tin and nickel is arranged between the nickel intermediate layer and the overlay. The first intermediate layer of nickel is applied onto the bearing metal layer from a. Watt's nickel electrolyte. A second"

intermediate layer consisting of nickel and tin is electroplated onto this first intermediate layer. A modified chloride/fluoride electrolyte is used for this purpose. By means of the intermediate layers of nickel ana tin-nickel, a system is produced which adapts itself to the load applied, load carrying capacity being increased, according to thermal conditions, by growth of the tin-nickel layer.
The object of the present invention is to overcome the disadvantages of the prior art.
The object of the invention is achieved by a composite
multilayer material as claimed in claim 1. In, addition,
the object is achieved by uses as claimed in claims 9 and
It has surprisingly emerged that a tin-nickel layor forms slowly even if one is not present initially. When the composite multilayer material is heated, as occurs in bushings and bearings made from the composite multilayer material according to the invention for example in the running-in phase, niclcel diffuses into the overlay consisting substantially of tin. In this way, a higher strength surface slowly forma as a result of the increasing concentration of a second hard phase of copper-fin and/or silver-tin, contained in the tin matrix. The reduction in. the supporting layer thickness increases fatigue strength.
In contrast to the prior art, according to which thin nickel layers of 1-3 urn. were applied, which served as diffusion harriers, tho nickel layer according to the invention forms a nickel source for formation of the
initially absent tin-r.iclcel layer. The nickel layer has to be thicker than. 4 pm, since otherwise the nickel layer could be completely consumed by the diffusion of the nickel into the tin layer. This would lead to detachment of the top layers now consisting of tin-nickel and the tin overlay alloy. Thicker nickel layers have hitherto been avoided as far as possible, since they do not have good sliding characteristics and are intended if necessary to allow wear quickly to reach the bearing metal beneath them.
The metals copper and silver may be present separately or in combination in the tin matrix. Their total content should amount to between a.pprox. 0.5 and 20 wt.%. Advantageously, the total content of copper and/or silver should amount to between approx. 2 and 6 wt.%.
The overlay should, advantageously exhibit a layer thickness of approx. 5-25 urn. Layer thicknesses of approx. 4 - 8 urn are preferred for the nickel intermediate layer as are layer thicknesses of approx. 6 - 14 urn for the overlay, with layer thicknesses of these orders of magnitude, it 1? pnsnred that neither the nickel layer nor the tin-based overlay is completely converted ss a result of diffusion. This would lead to problems of adhesion or undesired interactions1such as brittle pha.se formation between the tin contained in the overlay and the bearing metal.
Advantageously, the bearing metals are copper-aluminum, copper-tin, copper-tin-lead., copper-zinc, copper-zinc-sillcon, copper-zinc-aluminurn, ccpper-aluminum-iron or copper-zinc alloys. Copper- or aluminum-based bearing
metals are preferred, i.e. bearing metals whose copper or aluminum content is between 50 and 95 wt.%.
To produce the composite multilayer material according to the invention, the intermediate layer of nickel is applied in a first step chemically or e3.ectrochemica.lly to a composite of steel and bearing metal. The overlay is then deposited from a binary or ternary alkylsulfonic acid electroplating bath with the addition of non-ionic wetting agents and free alkylsulfonic acid. When producing bearings, first of all the bearings are prefabricated from the composite of steel and bearing metal, the intermediate layer of nickel and the overlay being applied in further steps.
The composite multilayer material according to the invention exhibits the great advantage that an interdiffusion layer of tin and nickel forms by itself during running-in. under operating conditions of bearingg and bushings made from, said material, said, interdif fusion layer increasing wear resistance. It does not have to be applied separately in a separate process step. It is possible t-r> oncourarje thfi \ nf r*rrli f fus'i on layer t.n arise by artificial aging of the plain bearings or bushings. For this purpose, heat treatment at approx. 150° - 170°C has proven particularly useful, said heat treatment proceeding for two or more hours to a few days.
The composite multilayer material according to the invention is particularly suitable for the production of crankshaft main bearings and of connecting rod bearings, in particular for the large connecting rod eye.
The invention is explained in greater detail with reference to an Example and Figures, in which:
Figure 1 shows a section through the bearing metal
layer, nickel intermediate layer and overlay of a composite multilayer material according to the invention;
Figure 2 shows a section through a bearing consisting of the composite multilayer material according to the invention after the running-in phase and.
Figure 3 shows the element distribution determined for the bearing according to Figure 2 in the area Ill-Ill by energy-dispersive X-ray analysis.
After appropriate pretreatment, a nickel diffusion barrier layer is applied from a Watt's nickel electrolyte onto a prefabricated bearing of a composite of steel and a bearing metal of CuPb22Sn.
The tin-based overlay is electrodeposited onto the nickel i nt P: rrnprji ate layer produced in. this way. The following aqueous-based electrolyte system, is used for this purpose:
Sn2+ as tin, me thane sulf onats 30 - 45 g/1
Cu.2'1 as copper methanosulfonate 2-3 g/l
Ag"1" as silver methanesulfonate 0.1-2 g/l
methanesulfonic acid 80 - 140 g/l
additive "N" (Cerolyt BMM-T) 30 - 45 g/l
reaorcxnol 1.5 - 4 g/l
Tin is used as anode material. The bath temperature for deposition of the overlay is 2C - 40oC. The current density used is 1.5 - 3.0 x 10-2 A/m 2. The distance between the anode and the cathode amounts to between approx. 3GO and 400 mm. The anode to cathode surface area ratio should be substantially 1:1 (+/-10%). In order continuously to remove 3n4* as it arises, the electrolyte has to be circulated via, a filtration plant.
Figure 1 is a sectional image of the layer structure of a composite multilayer material obtained as described, above with a copper-tin overlay. 1 designates the overlay of copper-tin of a thickness of 13.1 urn, 2 being the nickel intermediate layer of a thickness of 4.9 urn and 3 being the bearing metal comprising CuPb22Sn.
The boundary line between the two layers 1 and 2 is shown clearly as a pale line.
Figure 2 is a sectional image of a bearing of the composite multilayer material shown in Figure 1 after the operating state has been established, i.e. after the running-in phase. To this end, the bearing was heat-treated for 500 hours at 150°C. The tin-nickel layer of a thickness of 4.1 urn designated 4 has arisen by diffusion, said layer resulting in a more wear-resistant sliding surface with a. greater load carrying capacity. That said layer is a tin-nickel layer is confirmed by the energy-dispersive X-ray analysis results illustrated in Figure 3. The distances on the X axis match the corresponding layer thicknesses in the area IIT-III of Figure 2. The overlay 1' and the nickel layer 2 now have slightly smaller thicknesses of 10.2 um and 3.3 u.m respectively.
The boundary line between the two layers I1 and 4 in Figure 2 is shown clearly as a pale line.
Underwood teats were carried out to assess the performance of bearings made from the composite multilayer material according to the invention. In these tests, a shaft with eccentric weights rotates in rigidly mounted connecting rods. The bearing system in the connecting rods takes the form of the test bearings. The test bearings have a wall thickness of 1.4 mm and a diameter of 50 mm. The specific load is adjusted over the bearing width. The speed of rotation amounts to 4000 rpm. Overlay fatigue and wear were measured after 250 hours of continuous operation. The results obtained in this test are listed in Table 1 (Example Nos, 5 - 8). For the purpose of comparison, the values are also indicated which are achieved with materials according to the prior art (Examples 1 - 4).
As is clear from, the results listed in Table 1, the bearings made from composite multilayer material, according to the invention are markedly superior to the conventional bearings wi'ch a lead-based overlay' with regard to overlay fatigue, wear and maximum load to total wear. Even the bearing with a pure tin overlay (Example 5) becomes almost comparable, with a thick nickel layer, to the bearings with lead-containing overlay and may be used for lighter loads.
Table 1
(Table Removed)

1. A composite multilayer material, in particular for
plain bearings or bushings, having a backing layer, a bearing metal layer (3} of a copper alloy or an aluminum alloy, a nickel intermediate layer (2) and an overlay (1), wherein the overlay (1) consists of approx. 0 - 20 wt.% copper and/or silver, the rest .being tin, and the layer thickness of the nickel layer amounts to more than 4 u,m.
2. The composite multilayer material as claimed in claim
1, wherein the overlay (1) comprises at least approx. 0.5 - 20 wt.T*; copper and/or silver.
3. The composite multilayer material as claimed in claim
1 or claim 2, wherein the overlay (1) consists of
approx. 2 - 8 wt.% copper and/or silver, the rest
being tin.
4. The co.mpos.ite multilayer material as claimed in any
one of claims 1 to 3, wherein the layer thickness of
the overlay (1) amounts to approx. 5-25 pm.
5. The composite multilayer material as claimed in any
one of claims 1 to 4, wherein the layer thic3 the overlay (1) amounts to apprcx. 6 - 14 urn.
6. The composite multilayer material as claimed, in any
one of claims 1 to 5, wherein the layer thickness of
the nickel layer (2) amounts to approx. 4 - 6 urn.
1. The composite multilayer materia.l as claimed in any
one of claims 1 to 6, wherein the bearing metal layer (3) consists of a copper-aluminum/ copper-tin, copper-tin-lcad, copper-zinc, copper-zinc-ailicon, copper-•zinc-a Luminum, aluminum-zinc or copper-aluminum-iron alloy.
8. The composite multilayer material as claimed in any
one of claims 1 to 1, which has undergone an aging
process and comprises an interdiffusion layer (4) of
substantially tin and nickel between the nickel
intermediate layer (2) and the overlay (I1).
9. Use of the composite multilayer material as claimed in
claims 1 to 8 as a crankshaft main bearing.
.10. Use of the composite multilayer material as claimed in claims 1 to 8 as a connecting rod bearing, in particular in the largo connecting rod eye.





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Patent Number 260136
Indian Patent Application Number 656/DELNP/2006
PG Journal Number 14/2014
Publication Date 04-Apr-2014
Grant Date 01-Apr-2014
Date of Filing 08-Feb-2006
Applicant Address STIELSTRASSE 11, 65201 WIESBADEN, GERMANY.
# Inventor's Name Inventor's Address
PCT International Classification Number F16C 33/12
PCT International Application Number PCT/DE2004/001765
PCT International Filing date 2004-08-05
PCT Conventions:
# PCT Application Number Date of Convention Priority Country
1 103 37 030.7 2003-08-12 Germany