For over two decades these life factors based on oil filtration
(Refs. 31–32) have been used in conjunction with ANSI/
ABMA standards (Refs. 6–7) and bearing computer codes
(Ref. 34) to predict rolling-element bearing life. However, in
1999 filter ratings underwent a revision and improvement
(Ref. 35). They are now based on ISO 16889 (Ref. 36), replacing
the older and now disavowed ISO 4572:1981 (Ref. 33).
A primary difference between these filter ratings is how
particle size is specified and measured. The older filter test
method used particle counters calibrated per ISO 4402:1991
(Ref. 37), with a variable material comprising irregularly
shaped particles — AC Fine Test Dust (AC FTD). The new filter
test method employs particle counters calibration per ISO
11171:1999 (Ref. 38), based on spherical particles traceable to
a National Institute of Standards and Technology (NIST) reference
material (SRM 2806, 1997) (Ref. 39), providing more
accurate and verifiable results (Refs. 35 and 40). In addition,
the new filter rating method uses a somewhat different test
dust (ISO Medium Test Dust, ISO MTD) (Ref. 41), replacing
the no-longer-available dust previously used, AC FTD.
The Needelman-Zaretsky life factors published in the early
1990s (Refs. 31–32) do not correspond to this revised and improved
system of filter ratings. This paper focuses on the improved
methods for measuring filter performance (improved
filter ratings), and recalibrated bearing life factors incorporating
these new ratings. The improved system of filter rating
provides more accurate measurement of industrial filter performance,
including performance improvements achieved
by advancements in the design, materials, and manufacture
of filters over the past 20 years.
In 2007 the ISO Standard 281, “Rolling Bearings — Dynamic
Load Ratings and Rating Life” (Ref. 42), was radically
changed. It is based on the inclusion of a “fatigue limit” in
the bearing life calculations and the addition of a “contamination
factor for circulating oil lubrication with online filters.”
This “contamination factor” is based on the analytical
work of Ioannides et al (Ref. 17) and on a “cleanliness code
according to ISO 4406” (Refs. 43–44). ISO 4406:1987 (Ref. 43)
is the cleanliness code based on particle counters calibrated
to the now obsolete ISO 4402 calibration (Ref. 37) that used
irregularly shaped AC FTD. ISO 4406:1999 (Ref. 44) uses the
approved ISO 11171 calibration method (Ref. 38) based on
the NIST spherical-particle reference material. ISO 281:2007
(Ref. 42) incorporates the new ISO 4406:1999 cleanliness
code (Ref. 44) but does not specify filter ratings to the levels
of contamination.
Based on the above discussion it became the objective
of the work reported herein to 1) review methods and data
for determining the effects of lubrication oil particle quantity
and size for calculating the bearing L10; 2) experimentally
calibrate older filter ratings that used AC FTD to new filter
ratings using the NIST traceable particle counting calibration
and ISO MTD; 3) re-calibrate the Needelman-Zaretsky equations
for determining the effect of oil filtration on rolling-element
bearing life to new filter ratings per ISO 16889 (Ref. 36);
4) determine filter ratings and related life
factors based on new cleanliness codes per
ISO 4406:1999 (Ref. 44) for ISO 281:2007
(Ref. 42); and 5) compare recalibrated filter
life adjustment factors to cleanliness ratings
presented in ISO 281:2007.
Failure Morphology
It is generally accepted that if a rolling-element
bearing is properly designed, manufactured,
installed, lubricated, and maintained,
“classical” rolling-element fatigue
is the failure phenomenon that limits bearing
life (Ref. 45). Rolling-element fatigue
is extremely variable but also statistically
predictable — depending on the steel type,
steel processing, heat treatment, bearing
manufacturing/type, and operating conditions.
This type of fatigue is a cycle-dependent
phenomenon resulting from repeated
stress under rolling-contact conditions and
is considered high-cycle fatigue; Sadeghi et
al provide an excellent review of this failure
mode (Ref. 46).
Rolling-element fatigue can be simply
categorized as either surface- or subsurface-
initiated (Fig. 1). The subsurface-initiated
fatigue failure is referred to as “classical”
rolling-element fatigue. The fatigue
failure manifests initially as a pit or spall
that is generally limited in depth to the zone
of the resolved maximum shearing stresses
and in diameter to the width of the contact
area (Fig. 1) (Ref. 45). Figure 1(a) illustrates the sequential
progression of a subsurface-initiated crack from a non-metallic
inclusion such as a hard oxide inclusion that acts as a
stress raiser. With repeated stress cycles the crack propagates
to form a crack network that reaches the surface, resulting in
a spall shown sequentially in the bearing race track. At this
point the bearing is no longer fit for its intended purpose and
should be removed from service. Bearing rating life L10, as
defined by the standards ANSI 9–1990 (Ref. 6), ANSI 11–1990
(Ref. 7), and ISO 281:2007 (Ref. 42), is based on subsurface
origin (classical)rolling-element fatigue (Ref. 45).
Figure 1 Subsurface- and surface-initiated rolling-element fatigue failures. For subsurface-initiated
failure, spall begins in subsurface region of maximum resolved shearing stresses. For
surface-initiated failure, spall begins at surface defect or discontinuity that acts as a stress
raiser. (a) Subsurface- initiated spall from hard oxide inclusion; and (b) surface-initiated
spall from debris indentation.
- Click image to enlarge
When the bearing is operated under conditions that deviate
from the rating or reference condition, the fatigue origin
can be of “surface” origin as illustrated in Figure 1(b).
In this instance the spall can initiate from a defect or stress
raiser on and/or near the surface of the bearing raceways
and/or rolling-elements (Refs. 45, 47–48). In the instance of
surface-initiated fatigue spall from hard-particle contamination,
the load zone of the race and/or rolling-element is indented
by the contaminant (Fig. 2). The indent acts as a stress
raiser from which the crack initiates and then propagates to
form a crack network into the subsurface region of resolved
maximum shearing stresses (Fig. 1(b)). A spall similar in appearance
to that of the surface-initiated spall is formed. The
characteristic difference between the surface- and subsurface-initiated spalls is that surface-initiated spalls result in
“arrowhead-type” geometry at the leading edge or point of
origin on the rolling-element or raceway surface (Fig. 1(b)).
Figure 2 Stress raiser from indentation of debris particle entering Hertzian contact zone between
rolling-element and raceway.
- Click image to enlarge
The number, size, and material properties of particles entering
the Hertzian contact of the rolling-element and raceway
impact bearing life. The nature of the particles in the oil
is a function of several processes:
- Manufacturing processes (swarf, chips, and grit)
- Internal generation, including wear debris and chemical
attack on surfaces
- Ingression from the environment (sand and dust)
- Maintenance activities (making/breaking fittings and new
oil)
- Lubricant breakdown products (sludges, precipitates, and
coke)
Typical particle size distributions from a variety of mechanical
systems are shown in Figure 3 (Refs. 31 and 32). The
greater number of smaller particles in each of the lubrication
systems is due in part to wear mechanisms that generate
smaller particles and, in part, to removal processes that
tend to remove more large particles than small ones (Ref. 31).
Steele (Ref. 49) reported a wide range of particulate levels in
unused turbine oils.
Figure 3 Comparing effect of oil filtration on particle contamination for
mechanical systems according to particle size calibration, per ISO
4402 (Needelman and Zaretsky (Ref. 31); Zaretsky (Ref. 32)).
- Click image to enlarge
Work reported by Tonicello et al (Ref. 47)
showed that for pairs of disks in rolling
contact where one pair comprises silicon
nitride (Si3N4) against AISI M–50 bearing
steel, and the second pair comprises AISI
M–50 against AISI M–50, and the oil particle
contamination is AISI M–50 wear debris,
the dent indentation on the raceway
of the respective AISI M–50 disk was three
times deeper with the Si3N4 disk than
with the AISI M–50 steel disk on a AISI
M–50 steel disk (Fig. 4). Greater stress concentration
in the Hertzian contact results
from deeper dents. It can be reasonably
concluded that ceramic balls or rollers can
lead to deeper dents in a mating steel raceway
(Ref. 47).
Figure 4 Dent profiles made on AISI M-50 steel disks by AISI M-50 particles. Mating disk (counterface)
is Si3N4 or AISI M-50 steel. Figure from Tonicello, et al (Ref. 47) (Courtesy of Maney
Publishing.)
- Click image to enlarge
Morales-Espejel and Gabelli (Ref. 50)
discuss “the different hypotheses available
to explain the interaction of sliding (and rolling) with the indentation
marks in both gears and rolling bearings” under
EHD lubrication. They present theory and analysis that are
qualitatively verified by experiment. The micropitting phenomenon
occurring around indentation marks is described
by them with the same physical model of Morales-Espejel
and Brizmer (Ref. 51) that takes into account the progression
of surface fatigue induced by locally reduced lubrication conditions.
Filter Rating Procedure
The basic procedure for rating filters is shown in the flow diagram
of Figure 5. During the multi-pass test, slurry of silica
particles is continuously fed into a recirculating system.
Figure 5 Basic multi-pass test procedure for filter rating using silica-based test
dust and in-line particle counting.
- Click image to enlarge
Particles flow into the filter, where some are captured, and
others return to the reservoir where they continue to recirculate. Throughout the test, particles upstream and downstream
of the filter are quantified with electronic, automatic
particle counters. The filter factor, or filter rating, for particle
size x is defined as the ratio of upstream to downstream
counts recorded during the test, denoted βx and termed the
“beta ratio”:
where NUx and NDx are the average number of particles
upstream and downstream of the filter, respectively,
whose particle size is greater than x μm.
Originally, automatic particle counters were calibrated
using AC FTD, per ISO 4402:1991 (Ref. 37). This material
comprises small, irregularly shaped particles of silica sand.
Although widely used, AC FTD lacked traceability, had
batch-to-batch variations, and reported size distributions of
dubious accuracy especially below 10 μm. In order to make
testing more reproducible, calibration methods were developed
traceable to an NIST standard reference material, NIST
SRM 2806 (Ref. 39). However, the new calibration method
(per ISO 11171:1999) (Ref. 38) reports the size of particles (in
micrometers) as the diameter of an equivalent sphere, rather
than the longest dimension as in the original method. These
alterations, in effect, changed the “micron ruler.” As shown in
Table I (Ref. 38), the particle sizes originally below 10 μm are
reported larger, and sizes above 10 μm are reported smaller.
For example, a silica particle reported to be 3 μm in size by a particle counter calibrated to the old standard is now reported
as 5.1 μm in size using the new calibration standard.
- Click image to enlarge
Figure 9 Comparison between βx (c) = 1,000 filter ratings based on ISO
16889:2008 and βx = 200 filter ratings based on obsolete ISO
4572:1981.
- Click image to enlarge
Along with calibrating automatic particle counters, AC
FTD was also used as the test contaminant in the previous
version of the multi-pass test. When it became unavailable
in the 1990s, an alternative test material with similar chemical
composition and size distributions was adopted — ISO
MTD. Although using a slightly different test contaminant
influences test results, the changes are less significant than
those produced by the new particle size calibration described
above. The βx values obtained via the revised multi-pass test
(ISO 16889:2008) (Ref. 36), using ISO MTD and particle counters
calibrated to the NIST standard, are now reported as βx(c)
values, where x is the micron size, per Equation 1, and c emphasizes
the new calibration method.
Twenty years ago, leading filter manufacturers rated filters
at the particle size x where βx = 200 (Eq. 1). For example, a filter
rated at β5 = 200 has one out of every 200 particles equal to or
greater than 5 μm pass through the filter during testing. However,
most engineers and end-users prefer to think of filter
ratings as the size where essentially no particles pass through
the filter. In an attempt to reach this ideal, many manufacturers
now also rate filters at the particle size x where βx = 1,000.
At this higher rating, only one particle in 1,000 passes through
the filter during testing. Using the new ISO standard, modern filter ratings are βx(c) = 200 and βx(c) = 1,000. Typical removal efficiency
results are shown in Figure 6.
Figure 6 Representative results from multi-pass filter testing per
ISO 16889:2008.
- Click image to enlarge
The removal efficiency Ex of any particle size x can be related
to the β factor as follows:
For any filter there is a large particle size above which essentially
nothing passes, βx ≥ 104 and Ex → 100%. In contrast,
there is also a small particle size for which βx ≥ 1 and Ex → 0%,
so that nearly all particles this size and smaller freely pass
through the filter and accumulate to copious amounts in recirculating
systems. For intermediate sizes, a fraction of the
particles are captured and the rest pass downstream. As an
example, a filter with β10(c) = 1,000 removes 99.9% of all particles
≥10 μm in size during a multi-pass test.
In summary, the changes to the ISO filter rating standard
were as follows:
- Particle counter calibration
- Changed from AC FTD to NIST calibration
- Increased accuracy and reproducibility
- Changed the “micron ruler”
- Test contaminant
- Changed from AC FTD to ISO MTD
- Increased accuracy and reproducibility
- Highest filter rating changed from βx = 200 to βx(c) = 1,000
- Closer to concept of “absolute rating”
Examples:
- For β5(c) = 200, 1 out of every 200 particles or 5 out of every
1,000 particles greater than 5 μm passes through filter
during test.
- For β5(c) = 1,000, 1 out of every 1,000 particles greater than 5 μm passes through filter during test.
Results and Discussion
In 1991, based on the experimental research of Bhachu et al
(Refs. 12–13) and Loewenthal et al (Refs. 9–11), Needelman
and Zaretsky (Ref. 31) presented a set of empirically derived
equations for bearing fatigue life (adjustment) factors (LF)
as a function of oil filter ratings (FR). These equations were
normalized (LF = 1) to a 10 μm filter rating at normal cleanliness
(as it was then defined, where βx = 200 per ISO 4572:1981
(Ref. 33). The life factor equations were incorporated into
the reference book, STLE Life Factors for Rolling Bearings
(Ref. 32).
The Needelman and Zaretsky oil filtration life factors
(Ref. 31) have been used in conjunction with ANSI/ABMA
standards (Refs. 6–7) and with bearing computer codes
(Ref. 34). Experimental studies made by other investigators
verify the relationship between rolling-element bearing life
and the size, number, and types of particle contamination
(Refs. 1–2; 4–5; 8, 14–20; 47–48). The ISO 281:2007 (Ref. 42)
incorporates a rolling-element bearing life factor based on
lubricant cleanliness and EHD film thickness based on the
work of Ioannides et al (Ref. 17) but does not relate the lubricant
cleanliness to the filter ratings.
Filter ratings have been revised and improved (Ref. 35).
They are now based on an upgraded filter rating method per
ISO 16889:2008 (Ref. 36), employing particle counts calibrated
to an NIST standard (Refs. 36 and 39). The work reported
here was undertaken to calibrate the “old” and obsolete filter
ratings to the “new” filter ratings, and to recalibrate the previously
published bearing life factors based on the old filter ratings
to life factors based on the new filter ratings. The revised
rolling-element bearing life factors were then compared to
the life factors in the ISO 281:2007 Standard (Ref. 42) that are
based solely on lubricant cleanliness levels.
Recalibration of Filter Ratings
Old βx = 200 filter ratings (AC FTD calibration) were converted
to new βx(c) = 200 filter ratings using Table I and plotted
in Figure 7. Although this transformation does not take into
account the change in test contaminant to ISO MTD, alterations
in counter calibration dominate over the change in test
contaminant. The equation relating old βx = 200 filter ratings
(FROLD200) with new βx(c) = 200 filter ratings (FRNEW200) is:
Figure 7 Comparison of new filter ratings — based on ISO 16889:2008 using
spherical particle calibration per ISO 11171:1999 — with obsolete
filter ratings based on ISO 4572:1981 using AC FDT calibration, per ISO
4402:1991.
- Click image to enlarge
Multi-pass filter tests were then performed according to
the new ISO 16889:2008 (Ref. 36) method using 25 different
filters over a wide range of filter efficiencies from five different
manufacturers. This allowed plotting βx(c) = 1,000 filter ratings
with βx(c) = 200 ratings. The relationship is plotted in Figure
8, and approximated by the equations:
Figure 8 Comparison of βx (c) = 1,000 filter ratings with βx (c) = 200 filter ratings;
filters tested, per ISO 16889:2008.
- Click image to enlarge
By cross-plotting the data of Figure 7 with that of Figure 8,
a relation between old and obsolete βx = 200 filter rating and
new filter rating βx(c) = 1,000 is obtained (Fig. 9), as described
by the equations:
Figure 9 Comparison between βx (c) = 1,000 filter ratings based on ISO
16889:2008 and βx = 200 filter ratings based on obsolete ISO
4572:1981.
- Click image to enlarge
Rolling Bearing Fatigue Life Factors
There were two independent investigations to specifically determine
the effect of oil filtration on rolling-element bearing
life. These were the studies of Loewenthal et al. (Refs. 9–11)
and Bhachu et al (Refs. 12–13).
Roller bearings.Bhachu et al (Refs. 12–13) used a gear
test machine to generate wear debris. The gear wear debris,
verified by ferrography to be representative of that found in
helicopter gearboxes, was used as the contaminant. Rollingelement
fatigue tests were conducted with 25 μm bore roller
bearings having a 2,957 N radial load. For each test series,
gear oil flow was passed through one of four possible filters
of different ratings from 2.5–40 μm or through an electromagnetic
separator and continuously supplied to a parallel rollerbearing
fatigue tester. EHD film thickness and Λ values during
testing are shown in Table 2.
Significantly, tests run with 40 μm filtration for only 30 min
before switching to 3 μm filtration showed substantially the
same lives as if all running had been with a 40 μm filter. Apparently
the early damage could not be healed, at least in
these small roller bearings. The test results are also shown in
Table 2. These results show that life increased with improved
filtration.
The original filter ratings were based on the old filter rating
method, ISO 4572:1981 (Ref. 33), with βx = 200. From these
roller bearing life data (Table 2), it was assumed (Ref. 31) that
the filter life factor takes the following form:
C1 is an empirically determined constant and C2 is an
empirically determined exponent. The experimentally determined
L10 lives from Table 2 for filter ratings βx 200 = 3 and
25 μm are 8 and 2.5 million inner-race revolutions. Solving for
C1 and C2 and normalizing LF = 1 when FR = 10 μm at βx = 200
(normal cleanliness), the following empirical relation was
obtained:
Substituting the new filter ratings into Equation 9, from
Equations 4 and 8, respectively, allows calculating bearing
life factors for new filter ratings. For βx(c) = 200:
For Equation 10, where FRβx(c)200 ≤ 4, LF ≈ 2.8.
For βx(c) = 1,000:
For Equation 11, where FRβx(c)1000 ≤ 5, LF ≈ 3.5.
Using Equation 9, the L10 lives for roller bearings were predicted
by normalizing Equation 9 to the experimentally obtained
L10 life, using the 3 μm-rated (βx = 200) filter. These results
are presented in Table 2 for comparison purposes.
The post-test inner-raceway measurements for 40 μm
(βx = 200) filtration showed greater out-of-roundness than in
the untested bearing. Less out-of-roundness was observed
with finer filtration down to the 8 μm (βx = 200) rating. Virtually
no out-of-roundness was observed when the 3 μm (βx = 200)
filter was used. Below the 3 μm (βx = 200) level the measurement
was similar to that of the un-used bearing. Bhachu et
al (Refs. 12–13) suggested that particles smaller than 3 μm
(βx = 200) were too small to have any effect on roundness and
merely passed through the contacts of the rollers and raceways.
There is a strong suggestion from the data of Table 2 that the
lack of contamination contributes to improvement in bearing
raceway surface finish during operation. There appears to be
a correlation between the lubricant film parameter Λ after
testing and rolling-element fatigue life as evidenced by the data.
a) Radial load, 2,975 N; original surface composite roughness (rms) 0.33 μm. From Bhachu, et al. (12) and Sayles and Macphearson (13).
b) Number of fatigue failures out of number of bearings tested.
c) Life prediction normalized to 3-μm filter, βx = 200.
d) Test run with 40-μm filter for 30 min before switching to 3-μm filter.
- Click image to enlarge
Ball bearings.Loewenthal et al (Refs. 9–11) performed a
series of tests to measure the quantitative effects of filtration
on rolling-element fatigue life. Four levels of filtration were investigated
using full-flow (βx = 200) filters rated at 3, 30, 49, and
105 μm. The 3 μm (βx = 200) filter used for these tests had been
developed to replace the original 40 μm (βx = 200) filter for a helicopter
gas turbine lubrication system. During service these
new filter elements were not only found to provide a much
cleaner lubricant — with less component wear — but contrary
to prior belief, to also greatly extend the time between filter
and oil changes — as discussed by Loewenthal et al.
The test bearings were 65 μm deep-groove ball bearings
run at 15,000 rpm under a radial load of 4,580 N, which produced
a maximum Hertz stress of 2,410 MPa. The lubricant
contaminant rate was 0.125-g/hr-per-bearing. The test environment
was designed to simulate an aircraft lubrication
system containing multiple bearings, pumps, and other components
commonly found in such systems. Test temperature
was 347 K. The test lubricant was a MIL–L–23699-type, which
produced a Λ value of 3.3, based on race and ball pre-test surface
finish measurements. The test contaminant was similar
to the particulate matter found in the lubricant filters of 50
IT8D commercial engines (Jones and Loewenthal (Ref. 52)).
Because this engine has a number of carbon-graphite bearing
sump seals, replication of oil contaminants in engines with
“windback-type” labyrinth seals demanded the use of a contaminant
made of 88 percent carbon-graphite dust, 11 percent
Arizona test dust, and 1 percent stainless steel particles.
The results of these tests are summarized in Table 3. As
with the work of Bhachu et al (Refs. 12–13), improved filtration
increased bearing life. However, for the contaminated
tests there appears to be no statistical difference in life obtained
between the 3- and 30 μm filters. Because of the severe
wear obtained, the contaminated 105 μm filter test series was
suspended after 448 hours on each bearing. No fatigue failures
were encountered due to the gross wear of the bearing
races. Based upon the test results between the 3- and 49 μm
filters, the following life relation is suggested from the data for
βx = 200 filter rating for ball bearings:
Using Equation 12, the L10 lives of ball bearings were predicted
by normalizing Equation 12 to the experimentally obtained
L10 life using the 3 μm (βx = 200) rated filter. These results
are presented in Table 3 for comparison purposes.
Substituting the filter rating for FR (βx = 200) from Equations
4 and 8, respectively, into Equation 12, filter life factors
can be calculated for the new filer ratings where:
1. For βx(c) = 200 filter rating:
for Equation 13, where FR βx(c)200 ≤ 4, LF ≈ 1.6.
For Equation 14, where FRβ x(c) 1,000 ≤ 5, LF ≈ 1.8.
Table 4 provides results from Equations 6, 9, and 12 for
various filter ratings. The resultant life adjustment factors
can be used to adjust the calculated bearing L10 or catalog life
to account for filtration level in the lubricant system. These
LF values are normalized to filter ratings (FR) of 10 μm at
βx(c) = 200 and 13 μm at βx(c) = 1,000 (normal cleanliness) and
are independent of the Λ and/or K values, loading conditions,
and bearing size. Based upon the data of Loewenthal et al
(Refs. 9–11), it is not recommended to use a life adjustment
factor less than 0.5 — even when no filter is used. Further,
Equations 9 and 12 may reflect the differences in the effect of
particle damage between roller and ball bearings.
Technology for improved oil filtration is commercially
available. By minimizing the number of harmful particles
entering a rolling-element bearing, oil filtration can substantially
extend bearing life. In addition to machine-generated
wear debris and ambient mineral dusts, all-too-frequent high
contamination levels in new oil also requires good filtration.
No reported testing has been performed comparing grease
lubrication, which entraps wear debris, with oil lubrication for the same bearings, with or without oil filtration. It is suggested
that for long-term application a LF = 0.5 for grease lubrication
be considered the same as oil lubrication for bearings
without filtration where no periodic re-greasing of the
bearing occurs. Where the bearing is continuously or periodically
re-greased, a LF = 1 should be considered.
a) Radial load, 4,580 N; speed, 15,000 rpm; temperature, 347 K; test lubricant, MIL-L-23699 type; film parameter A, 3.3. From Loewenthal, et al. (9)–(11).
b) Number of fatigue failures out of number of bearings tested.
c) Probability (expressed as a percentage) that bearing fatigue life in a given test series will be inferior to the life obtained with ultraclean lubrication. A 90% or
greater confidence number is considered statistically significant.
d) Life prediction normalized to 3-μm filter, βx = 200 and L10 = 1,099 h.
e) Test series was suspended after 448 test hours on each of the test bearings due to excessive bearing wear. No fatigue failures were encountered.
f) Life prediction normalized to 3-μm filter, βx = 200 and L10 = 505 h.
- Click image to enlarge
Comparison of Filter Life Factors (FLFs) to ISO Standard
281:2007
In 2000 the International Organization for Standardization
(ISO) modified the standard ISO 281:1990 — “Rolling Bearings:
Dynamic Load Ratings and Rating Life” — to include a
fatigue limit (Ref. 53). The endurance or fatigue limit as applied
to rolling-element bearings is based on the theoretical
work presented in 1985 by Ioannides and Harris (Ref. 54). It
is a theoretical load or shearing stress (based on a Hertzian
contact stress) below which no fatigue failure is assumed to
occur, and therefore where fatigue life is infinite. ISO 281:2007
replaced ISO 281:1990, as modified in 2000. The 2007 standard
adopted the 1999 approach to bearing life calculations
presented by Ioannides, Bergling, and Gabelli (Ref. 55), and
includes the effects of lubricant contamination on bearing
life.
The ISO 281:2007 Standard (Ref. 42) incorporates a new service
life formula that integrates all life adjustment factors LF in
what is now called aISO. The life factor aISO includes four interdependent
factors: 1) lubrication regime, К; 2) lubricant contamination
or oil cleanliness, eC; 3) applied dynamic equivalent
load (applied load) to the bearing, P; and 4) fatigue load or
stress endurance limit of the bearing material, Cu.
From the ISO 281:2007 Standard (Ref. 42) p. 24 —
“…when the lubricant is contaminated with solid particles,
permanent indentations in the raceway(s) (and rollingelements)
can be generated when these particles are overrolled.
At these indentations local stress risers are generated
which will lead to a reduced life of the rolling bearing. This
life reduction due to contamination in the lubricant film is
taken into account by the contamination (life) factor eC.”
In the ISO 281:2007 Standard (Ref. 42), the contamination
factor eC is given in a table based upon levels of contamination
that are not tied to specific filter ratings.
The standard states that the contamination life factor is dependent
on the following:
- Type, size hardness and quantity of the (contaminant)
particles
- EHD lubricant film thickness (viscosity ratio, К)
- Bearing size (bearing pitch diameter, Dp)
The lubrication regime is defined by EHD theory; in the
standard it is defined by the parameter К, the ratio of the
actual viscosity of the lubricant in the bearing at operating
temperature to a reference viscosity. The reference viscosity
is that which would produce a lubricant film thickness equal
to the composite surface roughness of the rolling-element
and the raceway, or Λ = 1. If К < 1, the contact is in a boundary
lubrication regime where the surface asperities of the rollingelement
and the raceway are in contact. It is preferable to
operate the bearing in a lubrication regime where К ≥ 1. As К
increases, bearing life increases. The К value in the standard
is based on what is termed in EHD theory as the “lubricant
factor,” or Λ. The Λ is equal to the EHD film thickness h divided
by the composite surface finish σ of the rolling-elements
in contact with the raceway:
where
and σ1 and σ2 are the root mean square (rms) surface roughness
of contacting bodies. Unfortunately, in the ISO 281:2007
Standard (Ref. 42), К is based on an undefined lubricant and
lubricant properties, and an undisclosed composite surface
finish, σ. However, from the standard where Λ can be calculated:
An approximate correlation can be established between filter
ratings and the contamination levels. For example, BFPA/
P5:1999 (Ref. 56) correlates ISO contamination levels with
βx = 75 and βx = 200 filter ratings. Using a similar approach,
we correlated filter ratings at βx(c) = 1,000 per ISO 16889:2008
(Ref. 36) to the contamination levels listed in ISO 281:2007
(Ref. 42). These contamination levels and filter ratings, together
with the life factor eC, are shown in Table 5. Also listed
are the Needelman-Zaretsky filter life factors at βx(c) = 1,000, from Equations 11 and 14 for comparison purposes.
- Click image to enlarge
The contamination life factors eC from ISO 281:2007 (Ref. 42)
are differentiated by both filter rating and bearing pitch diameter.
The Needelman-Zaretsky life factor equations do not
differentiate based on bearing size but do distinguish between
ball and roller bearing types (Ref. 31).
Although we consider the effect of Λ on rolling-element
fatigue life independent of and separate from the filter life
factors, the Needelman-Zaretsky life factors (Ref. 31) are normalized
at Λ ≈ 1.1 and LF = 1.
The contamination life factor eC from Table 5 can be used to
adjust the calculated bearing L10 or catalogue life to account
for filtration level in the lubricant system; these results are
shown in Table 6. The values of eC for Dp < 100 mm were used.
For the data of Bhachu et al (Refs. 12–13), К = 2.8. For the data
Loewenthal et al (Refs. 9–11), К = 4.7. For each respective set
of data the EHD film thickness was assumed by us to remain
unchanged. Hence the effect of Λ and/or К was not factored
into the predicted lives shown in Table 6.
a) Normalized to 7-μm filter rating where βx(c) = 1,000 for high cleanliness level of contamination.
b) See Table 3. Test series was suspended after 448 test hours on each of the test bearings because of excessive wear. No fatigue failures were
encountered.
- Click image to enlarge
The results from the Bhachu et al (Refs. 12–13), and
Loewenthal et al (Refs. 9 and 11), suggest the following: 1)
for filtration levels between 4 and 34 μm at βx(c) = 1,000, representing
“extreme cleanliness” to “typical contamination,”
the ISO 281:2007 Standard (Ref. 42) provides a reasonable
qualitative estimate of the effect of particle damage on rolling
bearing life; and 2) at conditions of severe contamination and
above where the filter ratings are ≥ 35 μm at βx(c) = 1,000, the
ISO 281:2007 Standard (Ref. 32) correlates with the Bhachu et
al results. In contrast, the ISO 281 is conservative compared
to the Loewenthal et al test results. This may be attributed to
the use in the Loewenthal et al tests of a contaminant based
on carbon-graphite particles that may act as a solid lubricant while the ISO 281 life ratings are primarily concerned with
common hard steel contamination that can be found in industrial
gearboxes and used by Bhachu et al in their tests.
Gabelli, Morales-Espejel, and Ioannides (Ref. 20) provide
a discussion of the theoretical basis for the calculation of
the contamination factor eC that correlates with the curves
of contaminant life factors vs. К values presented in the ISO
281:2007 Standard (Ref. 42) and the contaminant life factors
presented in Table 5 that are from the standard. According to
Gabelli, Morales-Espejel, and Ioannides (Ref. 20), the following
variables should apply in determining a contamination
factor eC: (Ref. 1) mean bearing (pitch) diameter; (Ref. 2) level
of contamination (filter size); and (Ref. 3) lubrication rating
of the bearing (К value). Gabelli, Morales-Espejel, and Ioannides
reduce the variables by the elimination of the fatigue
limit. Their theoretical results were similar to those in Annex
A of the ISO 281:2007 Standard (Ref. 42).
There is an issue as to whether the EHD film thickness or Λ (К
value) mitigates the negative effect of lubricant contamination
on rolling-element fatigue life. That is, is the effect of contamination
on bearing life less severe with increasing film thickness?
In order to benchmark their analysis, Gabelli, Morales-
Espejel, and Ioannides (Ref. 20) presented endurance data of
172 bearing population samples obtained over several years
comprising 14 types and sizes of rolling-element bearings. It
was reported by them that “Each bearing sample is normally
formed of a group of 30 bearings; several thousand bearings
were endurance tested for this set of experimental results.”
The Gabelli, Morales-Espejel, and Ioannides data for Λ
values varying from 0.4 – 2.9 (К = 0.3 – 4) comprises three contamination
levels. They classified their contamination conditions
as follows:
- The first contamination condition was classified as
their “standard cleanliness tests.” The filtration level at
βx(c) = 1,000 was ≤ 7 μm and their range for eC varied from
0.8 – 1, or equivalent to “high cleanliness” in Table 5.
- The second contamination condition was classified as
“slight contamination,” or equivalent to βx(c) = 1,000 filter
range of 15–24 μm in Table 5. They reported that under the
given test conditions the expected contamination (life)
factors eC can range from 0.3–0.5; their actual life data
showed eC values that ranged from 0.1–0.5.
- The third contamination condition was classified as
“typical to severe contamination.” From Table 5 this
would comprise βx(c) = 1,000 filter range of 25 μm or
greater — although no filters appear to have been used in
this test series. Their actual life data showed eC values that
ranged from 0.01–0.3.
The Gabelli, Morales-Espejel, and Ioannides experimental
data, if statistically significant, shows a relation between the
contaminant life factors eC2 and К — as presented in Annex A of
the ISO 281:2007 Standard (Ref. 42).
In 1985 Lorosch (Ref. 14) reported that “The influence of
contaminants is great with small bearings, and decreases
with increasing bearing size. Consequently large bearings
have a larger capacity than calculated.” In other words, for
a particular contamination level or oil cleanliness the effect
of lubricant contamination is less severe for larger-pitch diameter
bearings than for smaller-pitch diameter bearings.
The effect of bearing size on the contamination factor eC is
incorporated in Annex A and Table 13 (Table 5 of this paper)
of ISO 281:2007 Standard (Ref. 42). For pitch diameters ranging
from 25–2,000 mm the contamination (life) factors eC increased
with increasing pitch diameter or bearing size. That
is, the larger the bearing the less effect of contamination on
the life of the bearing.
The pitch diameters for the bearing tests reported by
Gabelli, Morales-Espejel, and Ioannides (Ref. 20) were between
25–200 mm. Their data did not show a statistical relation
between the contamination levels and bearing size. They
explained, “The range of bearing sizes limited the range for
comparison with bearing size.” However, the sizes and types
of bearings were reasonably representative of those used in
most rotating machinery applications.
A comparison of the data in Table 2 for the roller bearings
from Bhachu et al (Refs. 12–13) — and the data for ball bearings
in Table 3 from Loewenthal et al (Refs. 9–11) — suggests
that the roller bearing lives are more sensitive to changes in
contamination level than those of the ball bearing. This is reflected
in the Needelman-Zaretsky contamination life factors
in Table 5.
Summary of Results
In 1991 Needelman and Zaretsky (Ref. 31) presented a set of
empirically derived equations for bearing fatigue life (adjustment)
factors (LF) as a function of oil filter ratings (FR). These
equations for life factors were incorporated into the reference
book, STLE Life Factors for Rolling Bearings (Ref. 32). These
equations were normalized (LF = 1) to a 10 μm filter rating at
βx = 200 (normal cleanliness) as it was then defined and Λ of
1.1. Over the past 20 years these life factors based on oil filtration
have been used in conjunction with ANSI/ABMA (American
Bearing Manufacturers Association) standards and
bearing computer codes to predict rolling bearing life. Also,
additional experimental studies have been made by other
investigators into the relationship between rolling bearing
life and the size, number, and types of particle contamination.
During this time period filter ratings have also been
revised and improved and are now based on particle counts
calibrated to a NIST standard reference material in the ISO
11171:1999 Standard (Ref. 38). It was the objective of the work
reported herein to 1) review methods and data for determining
the effects of lubrication oil particle size for calculating
the bearing L10 or catalog life; 2) experimentally correlate
older and/or obsolete filter ratings and the new ISO filter ratings;
3) re-calibrate the Needelman-Zaretsky equations for
determining effect of oil filtration on rolling-element bearing
life to the new filter ratings; 4) relate the new filter ratings to
contamination levels listed in the ISO 281:2007 Standard; and
5) compare recalibrated filter life adjustment factors to those
cleanliness ratings presented in ISO 281:2007 (Ref. 42).
The following results were obtained:
- Using two transformations, obsolete filter ratings can
be converted to new ISO filter ratings and vice versa.
Approximate equations relating the old βx = 200 FR values
with the new βx(c) = 200 and βx(c) = 1,000 FR values are:
For new βx(c) = 200 filter rating;
FRβx(c) 200 = 0.722 (FRβx 200) + 2.97
For new βx(c) = 1,000 filter rating;
FRβx(c) 1,000 = 0.848 (FRβx 200) + 4.14
- Two separate sets of life factors (LF) based on lubricant
cleanliness for roller bearings and ball bearings,
respectively, were derived based on the new βx(c) = 200
and βx(c) = 1,000 ISO filter ratings. These LF values are
normalized to FR values of 10 μm at βx(c) = 200 and 13 μm
at βx(c) = 1,000 and are independent of Λ and/or К, loading
conditions, and bearing size. These are:
LF ≈ 3.5 [1.39 (FRβx(c) 200) – 4.11]–0.55
For roller bearings and new βx(c) = 1,000 filter rating;
LF ≈ 3.5 [1.18 (FRβx(c) 1,000) – 4.88]–0.55
For ball bearings and new βx(c) = 200 filter rating;
LF ≈ 1.8 [1.39 (FRβx(c) 200) – 4.11]–0.25
For ball bearings and new βx(c) = 1,000 filter rating;
LF ≈ 1.8 [1.18 (FR βx(c) 1,000) – 4.88]–0.25
- ISO 281:2007 Standard provides a reasonable qualitative
estimate of the effect of particle damage on rollingelement
bearing fatigue life for filtration ratings ranging
from ≤ 4 μm at βx(c) = 1,000 (extreme cleanliness) up to
β34(c) = 1,000 (typical contamination). At conditions of
severe contamination and above, where the filter ratings
are ≥35 μm at βx(c) = 1,000, the ISO 281:2007 Standard
correlated with test results obtained with common hard
steel contamination that can be found in industrial
gearboxes.
Acknowledgments. The authors would like to thank the
Donaldson Company for supplying the multi-pass test data
used to create Figures 6 and 8 and Equations 5 and 6.
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About Author
William (Bill) Needelman received his B.Sc. from McGill
University and M.S. from Princeton in Physical Chemistry.
His work career began at the Pall corporation (26
years) — his last six years there as Principal Scientist. After
eight years at the Donaldson Corporation as Chief Science
Advisor, Needelman began his own company — Filtration
Science Solutions, Inc. His business was devoted to the
R&D, design, build, modeling, laboratory testing, field
testing, and evaluation of filters for a countless variety of
aerospace and industrial applications. Bill’s work has appeared in some 47
publications, including international standards and handbook chapters. He
was also the lead author for AWEA-Recommended Practices for Wind Turbine
Gearbox Filtration. In addition, he is an Adjunct Professor of Chemistry at SUNYSuffolk
and at the U.S. Merchant Marine Academy.
Erwin V. Zaretsky, PE is an engineering consultant to
industry and government, a noted speaker and teacher,
and author of more than 200 technical papers and
two books. He retired as Chief Engineer/Materials and
Structures at the NASA Glenn Research Center where he
retains an emeritus position as Distinguished Research
Associate. A 1957 graduate of the Illinois Institute of
Technology in Chicago — and with a 1963 doctorate
from Cleveland State University — Zaretsky is a former
head of the NASA Bearing, Gearing and Transmission Section, where he
was responsible for most of the NASA mechanical component research for
air-breathing engines and helicopter transmissions. With over half a century
of experience in mechanical engineering related to rotating machinery and
tribology, Zaretsky has performed pioneering research in rolling-element
fatigue, lubrication and probabilistic life prediction; his work resulted in the
first successful 3 million DN bearing. Zaretsky is an Adjunct Professor at Case
Western Reserve University. In 1992 he edited and co-authored the STLE
(Society of Tribologists and Lubrication Engineers) book — STLE Life Factors
for Rolling Bearings — as he had done previously, in 1997 — Tribology for
Aerospace Applications. Zaretsky is the recipient of numerous NASA awards
for his contributions to the Space Program, among which are the NASA Medal
for Exceptional Engineering Achievement, the NESC Director’s Award and the
Astronaut’s Silver Snoopy Award. In both 1999 and 2013 the STLE presented
Zaretsky with the Wilber E. Deutsch Memorial Award, which honors the most
outstanding paper written on the practical aspects of lubrication. In 2012
the STLE presented Zaretsky with their International Award — STLE’s highest
technical honor for his lifetime of contributions to the field of tribology
research. He has also received four IR-00 awards. Zaretsky is a Life Fellow of
both the ASME and STLE.