The properties of Engine bearing materials determine how a bearing functions under conditions of alternating load, intermittent metal-to-metal contact with the journal and in the presence of impurities transported in the oil.
The structure and the characteristics of the materials used in a high performance bearing are particularly important because of the severe conditions under which it must operate, including high loads and high rotation speeds.
Here are the main properties of materials for engine bearings:
Thus, in order to achieve durability and reliability from an engine bearing, its materials should paradoxically combine contradictory properties: high strength (load capacity, wear resistance, cavitation resistance) with softness (compatibility, conformability, embedability.) .
The contradictory combination of strength and softness may be achieved if the bearing material has a composite structure.
Engine bearings are composed of a steel back, onto which is applied a relatively strong base (copper or aluminum) combined with a solid lubricant in the form of either a thin overlay or small particles distributed throughout the base material.
Bearing material having a thin overlay is called tri-metal, in contrast to materials without any overlay – bi-metal.
Typical tri-metal and bi-metal engine bearing construction is shown in Fig. 1:
Microstructure of a typical tri-metal bearing is shown in Fig. 2:
Conventional tri-metal bearings are composed of the following layers :
The load capacity of a tri-metal bearing is determined by the fatigue strength of both the overlay and the intermediate layer.
The fatigue strength of the copper based intermediate layer is commonly higher than that of the soft lead based overlay. Therefore fatigue cracks initiate on the overlay surface. Overlay fatigue itself does not cause engine failure. However, bearings working with a fatigued overlay for an extended period of time will undergo partial flaking of their overlay. This will lower the oil film thickness and allow the possibility of destructive contact between the crankshaft journal and the bearing surface.
The fatigue of a copper based intermediate lining begins with the fatigue of its overlay. The overlay flakes out from the copper lining, resulting in a breaking of the oil film. This changes the lubrication regime from hydrodynamic to boundary. The load localizes at the contact area, causing a formation of small cracks on the lining surface .The cracks then propagate throughout the lining thickness, meet the steel back surface and continue to advance along the steel-copper boundary. As a result, parts of the intermediate layer detach from the steel surface . Thus, both the strength of the overlay and the strength of the intermediate layer affect bearing operation and durability.
Load capacity for the pMax Black™ intermediate layer was reached (up to 17,000 psi) by changing two parameters: an increase of the tin content in the copper base alloy and a greater cold work treatment (cold rolling) of the steel-bronze strip.
Tin strengthens copper alloys. Intermediate layer alloys of conventional high performance bearings contain 2-3% tin. The hardness of such alloys is commonly 90-95 HV.
The hardness of the intermediate layer of pMax Black™ was increased (by 20-25%) to 110-115 HV. This was achieved by increasing the tin content of the copper alloy to 4-5%, and by a greater amount of cold work (cold rolling of the strip with an increased thickness reduction). The harder intermediate layer provides more reliable bearing operation under high load.
The main factor affecting the load capacity of a tri-metal bearing is the fatigue strength of the overlay. Therefore the primary focus for pMax Black™ was to develop an overlay having increased fatigue strength.
Consider the overlay properties that exert an influence on its fatigue strength:
In the case of tri-metal bearings, the substrate is an intermediate copper based alloy. The overlay is adhered to the substrate surface. Therefore the overlay dimensions at the interface between the two materials cannot distort more than the dimensions of the intermediate material when a load is applied to the bearing.
Since the modulus of elasticity of the copper alloy (15*106 psi) in the intermediate layer is much higher than that of the overlay leaded alloy (2*106 psi), the stress in the overlay induced by the load is much lower than the stress in the intermediate layer. This is in accordance with the relationship: σ = E*ε (E- modulus of elasticity, ε – the strain at the interface).
However, the ratio between the elasticity modules of the materials is equal to the ratio between the stresses only for ultra-thin overlays. The thicker the overlay, the less its surface is affected by the mechanical properties of the substrate material. The graph in Fig. 3 demonstrates the effect of the thickness of a lead base overlay on its fatigue strength. The data was obtained in experiments performed with the King test rig.
Conventional tri-metal bearings for street use engines have an overlay with a thickness of about 0.0007”.
The thickness of the overlay for highly loaded race use bearings should be less than that of street engine versions.
The pMax Black™ structure features an overlay of 0.0005”, which combines increased fatigue strength with good anti-friction properties.
Our tests prove that an increase of copper from 2.6% to 5.1% in a leaded alloy results in an increase of alloy hardness from 12.3 HV to 18.3 HV. Higher copper content also increases the fatigue strength of the overlay alloy.
In contrast to conventional high performance bearings, the pMax Black™ overlay material of King XP series high performance bearings contains 5% copper, providing higher fatigue strength.
One of the most effective methods of increasing fatigue strength of a metal part is Shot peening. This is a cold work process in which a metal part is struck by a stream of small hard spheres (shot). They create numerous overlapped dimples on the part surface . Shot peening produces a hardened compression stressed skin which resists the formation of fatigue cracks. Unfortunately, shot peening is not effective as a treatment for soft leaded alloys, due to their low strain hardening effect.
An alternative and effective method of surface hardening lead based overlays has been developed by King Engine Bearings. This innovative technique enables the formation of an ultra thin hardening of the overlay surface. It is an essential component of the pMax Black™ overlay.
All King XP series high performance bearings are manufactured with the pMax Black™ structure and its hardened pMax Black™ overlay. These bearings are easily recognizable by their distinctive dark black color. This is an attribute resulting from King’s proprietary surface hardening process (Fig. 4).
The pMax Black™ overlay surface hardness has a nano-scale thickness. It is sufficient to suppress the formation of fatigue cracks on the overlay surface. It has proven its effectiveness in increasing the fatigue strength of high performance tri-metal bearings.
pMax Black™ was tested by two different methods:
a. Validation of pMax Black™ in Test Rig Machine
The tests were performed in the test rig designed and manufactured by King Engine Bearings (Fig. 5)
The test rig uses an eccentric shaft located between two concentric shaft parts. The test bearing coupled with the eccentric shaft is mounted in the big end of the connecting rod. Rotation of the eccentric shaft results in reciprocating motion of the connecting rod .
The shaft is driven by an electric motor. The rotation speed of the test rig may be varied within the range of 1500-5000 RPM. Load is created by a hydraulic cylinder.
The experimental bearings were tested with a reciprocating load in the range of 9500 to 12,000 psi.
Test duration: 24 hrs;
Rotation speed: 3000 RPM
Number of cycles: 4,300,000
All our data regarding the load capacity of different materials was obtained in our test rig under similar test conditions. It is incorrect to compare load carrying capacity measured in different test rigs. There is no standardized scale method of bearing fatigue testing. Bearing manufacturers use different equipment and different test conditions, which produce different results for the same material. Therefore, only results obtained under the same conditions and in the same test machine may be compared.
The rig tests results:
The effects of increased copper content in the pMax Black™ overlay alloy and of the surface hardening treatment on the load capacity of the bearings have been determined in a series of rig tests using King high performance bearing C 697.
The bearings were tested at a load of 9500 psi, which is above the load capacity of conventional tri-metal bearings.
The bearings with conventional overlay composition (Sn 10.3%, Cu 2.6%, Pb balance) and hardened surfaces passed the test without the formation of fatigue cracks. However, their sufaces did exhibit shiny areas of slight wear (Fig. 6A).
Also similar in appearance were the bearings with a non-hardened surface – but with an increased copper content in the overlay (5.1% Cu) (Fig. 6B).
A – copper content 2.6%, hardened surface
B - copper content 5.1%, non-hardened surface
C – copper content 5.1%, hardened surface (XP bearing)
Bearing performance improves significantly when both factors (higher copper content and surface hardening treatment) take place. The bearing completes the test in excellent condition: no fatigue cracks, no wear marks, no seizure (Fig. 6C).
For comparison purposes, a conventional high performance bearing (non-King bearing) was tested under the same conditions. The bearing was similar to King C 697. It had the same dimensions, but its overlay was conventional (copper content 2.8%, no surface treatment).
The tested bearing is shown in Fig. 7.
Overlay fatigue cracks are clearly seen in the magnified picture.
It is evident that the load capacity of the bearing material was below the test load (9500 psi).
According to our rig tests, the conventional lead based overlay has a fatigue limit of about 8700 psi.
In order to determine the load capacity of the developed pMax Black™ structure, King high performance bearings C 807XP were tested under different loads in the range of 9500 to 12,000 psi.
The bearings proved excellent performance under loads of 9500 psi and 10,200 psi (Fig. 8).
A further increase of load resulted in the formation of overlay fatigue cracks.
The test were repeated several times. According to their results, the fatigue strength of pMax Black™ was determined: 10,200 psi. It is 17% greater than the fatigue limit of conventional tri-metal bearings.
A conventional high performance bearing similar to King C 807XP was tested at a load equal to the fatigue resistance of pMax Black™.
A photograph of the tested bearing is presented in Fig.9.
In contrast to King XP series bearings, the conventional high performance bearing has a large area of overlay fatigue cracks. The cracks are shown in the magnified image (Fig. 9).
b. Validation of pMax Black™ in dynamometer
The tests were performed on King’s Power Test dynamometer.
Tested engine: high performance Chevy 355.
King bearings: CR 807XP (connecting rod bearings) and MB 557XP (main bearings) were installed in the engine.
Two types of King connecting rod bearings C 807XP were tested: full surface bearings and bearings with a reduced surface area (a groove with a width of 1/3 of the full surface).
The two types of bearings, after dynamometer testing, are shown in Fig. 11.
 Dmitri Kopeliovich (2011), The Proper Selection of Engine Bearing Materials, AERA., April-June 2011, p.48-62
 Dmitri Kopeliovich (2013), Engine bearing materials, SubsTech (Substances&Technologies), Available from http://www.substech.com/dokuwiki/doku.php?id=engine_bearing_materials
 Dmitri Kopeliovich (2013), Shot peening, SubsTech (Substances&Technologies), Available from http://www.substech.com/dokuwiki/doku.php?id=shot_peening
 Dmitri Kopeliovich (2013), Engine bearing fatigue test, SubsTech (Substances&Technologies), Available from http://www.substech.com/dokuwiki/doku.php?id=engine_bearing_fatigue_test