Testing Philosophy

Testing Methods

WAM High Speed Load Capacity Test Method

WAM Load Capacity Testing for Lubricating Capability of Oil Formulations

Cage-Land Abrasive Wear

Adhesive Wear Test Method

Oil-Off Test Protocol

 

top

 

 

 

 

 

top

 

 

 

 

 

 

top

 

 

 

 

 

 

top

 

 

 

 

 

 

top

 

 

 

 

 

 

  Introduction
  Test Rig and Test Materials
  Test Procedure
  Typical Oil-Off Test Results
  Effect of Material or Oil Lubricating Quality

Oil Off Testing
  Introduction
  An Oil-off test protocol evaluates bearing materials and lubricants for durability and operational life under marginal lubrication conditions that may be experienced in service. The commonly used aircraft bearing steel M50 is used as a baseline for evaluation purposes. Oil-off tests generally support other tribology tests for material and lubricant performance. Other test protocols include attributes for adhesive wear, abrasive wear and load-carrying (scuffing) capacity.
Test Rig and Test Materials
 

Oil-off tests can be conducted with the Wedeven Associates, Inc. WAM8 or WAM9 test machines, as shown in Figure 1. The test specimens consist of a ½ inch ball specimen (or alternate ball sizes), which rides against a flat disc specimen. The disc specimen represents bearing ring materials.

Final finishing of the disc specimen is conducted by Wedeven Associates, Inc. Surface preparation consists of fine grinding, followed by abrasive lapping to a surface finish of 2 µ-inch, Ra. The lapping operation is done with specimen rotation about its centerline to create a circumferential lay in the direction of rolling motion. The finishing method consists of several lapping stages to obtain a consistent surface texture. Care is taken to avoid microscopic bends and folds ("leafing") in the surface texture. The final finish is similar to a finely honed bearing raceway.

Test Procedure
 

An oil-off test protocol was established with the following test conditions:

Ball M50, ½ inch dia., Grade 5 (or alternate size or Grade)
Disc M50, finished to 2 min Ra (baseline material and finish)
Contact stress 2.49 GPa (360 ksi)
Entraining velocity 10.16 m/sec (400 in/sec)
Contact slip 5%
Temperature (disc) 200 °C (392 °F)
Lube supply drip feed until oil-off at 600 seconds

The test is initiated after the disc specimen temperature stabilizes at 200 °C. The first 60 seconds of the test is operated at or near pure rolling. The remainder of the test is run at 5% slip. A computer-controlled peristaltic pump is shut off after 600 seconds. To avoid release of residual oil on the ball and disc surfaces, tests are conducted with the ball thermocouple, oil shielding material and parts of the heating equipment removed from the test area immediately following oil shut off. Oil-off tests can be conducted with various criteria for test termination. These include: (1) oil-off operation until a rapid rise in traction coefficient to an arbitrary value; (2) oil-off operation until a rise in traction coefficient to 0.15 and (3) oil-off operation for 220 seconds, which is beyond the time typically required to reach a maximum traction coefficient (~0.4) and the onset of a high wear rate.

Except where noted, the test oil is Mobil Jet II. Mobil Jet II is classified as a standard (STD) oil under MIL-PRF-23699 specification. From our testing of qualified jet engine oil products, Mobil Jet II has excellent lubricating ability compared to most oil brands on the qualified products list for MIL-PRF-23699.

Typical Oil-Off Test Results
 

To establish the role of oil lubricating characteristics during oil-off conditions, two tests were run with oil TEL-0004, which has known difficulties in certain applications. TEL-0004 is a qualified Grade 4 product under MIL-PRF-7808K specification. The U.S. Air Force supplied the test oil with the designation TEL-0004. Oil-off tests were also conducted with high load-carrying DOD-L-85734 oil, which is used in aircraft gearboxes and demanding engine applications.

Typical oil-off traction behavior for M50/M50 materials and the three oil types are shown in Figure 2. With continuous oil supply and a test temperature of 200 °C, the traction coefficient for a full EHD oil film is on the order of 0.025. A typical traction coefficient for jet engine oil at ambient temperature (~23 °C) is on the order of 0.07.

The rise in traction coefficient after oil-off is associated with local adhesion and transfer of material from the ridges of the finishing marks on the disc specimen. The local material transfer, smearing and oxidation create material pileup and a loss of surface integrity. At this stage the surfaces encounter high local friction events due to material pileup and high friction oxides. The amount of wear is not significant. While the surface disturbance appears to be minor, the situation is in a run-away condition heading for gross surface failure and a traction coefficient on the order of 0.4.

The maximum traction coefficient of 0.4 is attributed to massive adhesion and material transfer between the surfaces. The rise in traction coefficient is associated with the spread of adhesive events across the operating track on the specimens. A momentary departure from an increase in traction is believed to be the result of lower tangential shear caused by the onset of wear.

These tests show that oil starvation leads to local adhesion and pileup of material on the surfaces with a corresponding rise in traction coefficient. Once this process starts (and without subsequent oil replenishment) adhesion and oxidation of transferred material becomes a run-away process. The run-away process seems to be well on its way by the time the traction coefficient has increased from 0.025 to 0.15 -- a six-fold increase in traction coefficient.


Effect of Material or Oil Lubricating Quality
 

The above results show that the initiation of run-away traction is due to adhesion and oxide growth at local sites. Resistance against adhesion depends upon the material pair, along with protection against removal of surface films that prevent atomic bonding between the surfaces. If this is the case, the important attributes of the material for oil-off performance are associated with the material's response to chemistry or "tribo-chemistry".

The oil-off test results with the three test oils in Figure 2 are summarized below with respect to the average time to at traction coefficient of 0.15.

Test Oil
Average time to traction coefficient of 0.15
TEL-0004(4 cSt) MIL-PRF-7808K
10.5 seconds (2 tests)
Mobil Jet II (5 cSt) MIL-PRF-23699
42.0 seconds (3 tests)
DOD-L-85734
81.0 seconds (1 test)

Oil additive chemistry and other factors affecting the lubricating ability of the oil are significant contributors to oil-off capability. An eight-fold difference between the time-to-failure is evident between a low quality oil for lubrication compared to a high quality oil. The traction data in Figure 2 shows that the onset of failure for TEL-0004 is a sudden event. The additive chemistry in the DOD-L-85734 oil results in a gradual rise in traction coefficient. The gradual rise in traction coefficient is associated with a controlled tribological process, which results in less severe local damage to the surfaces. There are noticeably fewer areas of material transfer or islands of oxidized material on the surfaces with the DOD-L-85734 oil.

These results strongly suggest that a high quality oil for lubrication can provide greater tolerance against surface damage during oil-off operation with better probability for recovery after a high traction event due to momentary oil-out conditions. It is recognized that with perhaps a few exceptions, high performing oils for lubricating ability are almost always low quality oils for thermal stability and coking. The significant feature that these tests bring out is that testing for bearing or material performance for oil-off capability can be significantly affected by oil type.

The oil-off test protocol can also be used to evaluate bearing materials, surface finishing processes (roughness and texture) and effects of surface defects. The test protocol can be expanded to include material and oil attributes and their potential for recovery following a high traction and material transfer event. The recovery is accomplished by repair of the surfaces through a wear process. However, incomplete surface repair and accumulated damage below the surface are likely to reduce fatigue life. In any case, recovery, even with a sacrificial wear process, has the potential to achieve survivability in the near term. To explore this further, inspection and documentation of oil-off bearing test hardware (or field hardware) is recommended. It is possible that a high quality lubricating oil may allow higher bearing torque rise and heat generation in an oil-off event than a low quality oil.