Ball Bearings

1.0 Introduction

Ball bearings are used widely in instruments and machines in order to minimize friction and power loss. While the concept of the ball bearing dates back at least Leonardo da Vinci, their design and manufacture has become remarkably sophisticated. In the following we shall review their basic characteristics.

2.0 Types of Ball Bearings

Commercially available ball bearings, which are usually made from hardened steel, involve many forms of construction. These have been summarized by A.O. DeHart ("Which Bearings and Why", ASME Paper 59-MD-12, 1959), from which source the following material (including Figures 1 & 2) is hereby reprinted*


"A typical deep-groove ball bearing designed for high-speed operation is shown in Figure 1. In this bearing, the separator serves to keep the balls from rubbing against one another as is piloted on the inner race OD. Alternatively, the separator may be piloted by the rolling elements or by the outer race ID. Where rotative speeds are low, the separator often is omitted. The rolling elements may take many forms — cylinders, balls, tapered rollers, barrels, or very slim rollers known as needles — and the whole bearing name is generally taken from this form.

Ball Bearings

There are several types of ball bearings that fit specific needs. The deep-groove ball bearing, Figure 2(a), is the most versatile. Radial loads and thrust-load capacities may be approximately equal in this bearing. When it has the proper separator, it is very good for high-speed operation. At low speeds, no bearing separator is required; at intermediate speeds, a ball control separator of steel-ribbon construction is adequate; while the ultimate high-speed performance is obtained with a race controlled (or piloted), fully machined separator.

Since balls are assembled into the bearing by eccentric displacement of the races the number of balls in this type of bearing is limited. More balls can be introduced into the bearing if a notch is machined into one of the races, Figure 2(b). Radial load capacity is higher in this bearing than in the standard deep-groove construction, but high-speed performance and thrust-load capacity is impaired. When large thrust loads in one direction are coupled with radial loads, angular contact ball bearings, Figure 2(c), are usually superior. Most high-speed and precision spindles use axially preloaded pairs of these bearings. Preload is controlled by the length of the spacers, which determine axial location of the races, or by mounting the bearings against one another in a "back-to-back" or "face-to-face" fashion. The double-row, angular-contact bearing, Figure 2(d), is a simpler arrangement from the standpoint of the user. The preload is built into the bearing at the factory.

In contrast th the previously discussed bearings, in which alignment is a very critical item, the self-aligning ball bearing, Figure 2(e) by virtue of the spherically ground outer race can tolerate considerable misalignment of shaft and housing. On the other hand, load-carrying capacity is reduced due to the high contact stresses that result from the large difference in curvature between the balls and the outer race.

The thrust ball bearing, Figure 2(f), is adaptable to large thrust loads that have almost no radial component. Very large sizes of this bearing are used in gun turrets and large earth moving machinery"

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Table 1. Bearing Selection Factors*

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3.0 Bearing Selection

Bearing selection represents a compromise among many factors including the nature of the application, performance requirements and cost. A useful bearing-selection chart, which summarizes the principal considerations involved, has been given by A.O. DeHart and is reproduced in Table 1.

For more details, which are beyond the scope of this presentation, the reader is referred to technical literature.

4.0 Bearing Loads

The first step in sizing a suitable ball bearing for a given application is the determination of the loads which support. In this section we list some of the most frequently occurring mechanical configurations and the bearing loads imposed by them.




The maximum bearing load on either pulley shaft occurs when the belt is transmitting the maximum horsepower (i.e., the belt would slip if the horsepower were increased above this level). Under this condition the maximum bearing load is given by:



Note: In the case of chain drives the bearing load is often approximated by the pull on the tight side of the chain, the slack side being assumed tensionless.


The bearing load on the camshaft bearings due to load, P, can be determined according to Cases (a) or (b), if the camshaft is supported by two bearings.

(ii) Disc cam with translating roller follower

The bearing load on the camshaft bearings due to the load, P, can be determined according to Cases (a) and (b), if the camshaft is supported by two bearings. Note that the force P in the above two cases is equivalent to a radial force, P, together with a torque about the cam axis.

(f) Spur Gears (External)



(g) Helical Gears

We consider here only the case of helical gears on parallel shafts.

Note that:
(i) The helices on mating gears are of opposite hand;
(ii) The direction of the thrust load is determined by the condition (see Figure 12) that the vector sum of the radial force and the thrust load is normal to the helix. This implies that reversal of rotation causes reversal of thrust.
The thrust load in the case of helical gears implies that the bearings be capable of carrying both the radial load and the thrust load.

The calculation of the radial bearing load in the case of shafts with two bearings can be obtained from Cases (a) and (b).

Again we note that since action and reaction are equal and opposite, the three orthogonal force components F, F_R and F_T act on gears (and shafts), but in opposite directions.


Note that the direction of F (in all gear drives) depends on the direction of rotation of the driving gear. The thrust loads F_TG and F_TP are components of the tooth separating force, which must be taken up by both pinion and gear bearings. The directions acting on the gear and the pinion are opposite. Total bearing force on each gear is the vector sum of three forces: tangential, gear thrust and pinion thrust. These forces are shown in Figure 14.


With the aid of these figures the radial bearing loads for shafts with two bearings can be obtained from Cases (a) and (b). The presence of thrust loads again necessitates axial takeup capabilities in bearings.


Note that the direction of F depends on the direction of rotation of the worm. The three force components, F, F_R and F_TW must be taken up by both worm and gear bearings. The directions acting on the worm gear and worm are opposite. Total bearing force on each member is the vector sum of these three forces. With the worm as driver and the gear rotating as shown in Figure 15, the direction of these forces on each member are shown in Figures 16a and b.


With the aid of these figures the radial bearing loads for shafts with two bearings can be obtained from Cases (a) and (b). Once again both thrust and radial forces need to be taken up by the bearings.

(j) Compound Spur-Gear Train

As an example of the bearing-reaction calculations for an entire gear train we consider the spur-gear train shown in Figure 17.

The gear train shown in Figure 17 transmits 1/20 horsepower. Shaft S-1 is the driver. If shaft S-2 rotates at 100 rpm CW as shown, what are the bearing reaction forces on Shaft S-2?

The free body diagram of S-2 is shown in Figure 18a, and component forces are shown in Figure 18b. From the horsepower the tramsitted forces are obtained as follows:

These transmitted forces are generated from contact tooth forces given by Equation 2:

Where the double subscripts designate transmission of forces between members. For example, F₁₂ means the force of gear 1 on gear 2.

The above contact tooth forces plus the bearing reaction forces hold the shaft in equilibrium as pictured in Figure 18a. Resolving all forces into X and Y components, as shown in Figure 19, the equilibrium equations can be applied.

Because of the particular shaft orientation given for this problem the X and Y components of contact force F₁₂ are the tangential and normal components, but this is not true of F₄₃ which is inclined 50° to the X axis.


Thus, there are 4 unknowns and two equations. However, if the moment equilibrium equations are written, the unknowns can be reduced.

Taking moments about Bearing A, first about the X-axis and then about the Y-axis (using the convention Positive moments are CCW):

Note that the sign of is negative. This means its direction is actually opposite of that assumed in equilibrium Equation 26. Thus, in Figure 19 component should be drawn in reversed direction to that shown. Conversely, component has a positive sign, so its' direction assumed for the equilibrium and Figure 19 is correct.

To determine the X reaction components moments are taken about the Y-axis at bearing A:

The resultant bearing reaction forces and orientations are pictured in Figure 20.

5.0 Sizing Ball Bearings

(a) Basic Definitions

In the course of many years of experience with ball bearings and extensive testing, it has been found that the prediction of the load capacity of a ball bearing is a statistical event related to the fatique life of the bearing. This makes the sizing of ball bearings more difficult than that of many other machine elements.

A basic phenomenon in ball bearings is that ball bearing life has been found to be inversely proportional to the cube of the bearing load. This means that when the load is doubled the life expectancy of the bearing is reduced by a factor of eight. This phenomenon has been studied extensively and has led to the adoption of an industry-wide national standard for rating ball bearings pioneered by the AFBMA (Anti-Friction Bearing Manufacturers Association, 1235 Jefferson Davis Highway, Arlington, Virginia, 22202). The following represents a summary of the load rating of ball bearings less than one inch in diameter, according to ANSI-AFBME Standard 9, 1978: "Load Rating and Fatique Life for Ball Bearings" - reprinted with the permission of the American National Standards Institute Inc., 1430 Broadway, New York, N.Y., 10018:

"Life Criterion. Even if ball bearings are properly mounted, adequately lubricated, protected from foreign matter, and are not subjected to extreme operating conditions, they can ultimately fatigue. Under ideal conditions, the repeated stresses developed in the contact areas between the balls and the raceways eventually can result in fatigue of the material which manifests itself as spalling of the load carrying surfaces. In most applications the fatigue life is the maximum useful life of a bearing. This fatigue is the criterion of life used as the basis for the first part of this standard."

The material in the standard which follows assumes bearings having non-truncated contact area, hardened good quality steel as the bearing material, adequate lubrication, proper ring support and alignment, nominal internal clearances, and adequate groove radii. In addition certain high-speed effects such as ball centrifugal force and gyroscopic moments are not considered. We now continue with the standard.

"Life. The "life" of an individual ball bearing is the number of revolutions (or hours ar some given constant speed) which the bearing runs before the first evidence of fatigue develops in the material of either ring (or washer) or of any of the rolling elements."

"Rating life. The "RATING LIFE", L₁₀, of a group of apparently identical ball bearings is the life in millions of revolutions that 90% of the group will complete or exceed. For a single bearing, L₁₀ also refers to the life associated 90% reliability. As presently determined, the life which 50% of the group of ball bearings will complete or exceed ("median life", L₅₀) is usually not greater than five times the RATING LIFE."

"Basic Load Rating. The "basic load rating", C, for a radial or angular contact ball bearing is that calculated, constant, radial load which a group of apparently identical bearings with stationary outer ring can theoretically endure for a RATING LIFE of one million revolutions of the inner ring. For a thrust ball bearing it is that calculated, constant, centric, thrust load which a group of apparently identical bearings can theoretically endure for a RATING LIFE of one million revolutions of one of the bearing washers. The basic load rating is reference value only, the base value of one million revolutions RATING LIFE having been chosen for ease of calculation. Since applied loading as great as the basic load rating tends to cause local plastic deformation of the rolling surfaces, it is not anticipated that such heavy loading would normally be applied."

(b) Determination of Basic Load Rating.

Based on the preceding definitions the standard lists the equations required for the determination of the basic load rating:

"Calculation of Basic Load Rating. The magnitude of the basic load rating, C, for radial and angular contact ball bearings with balls not larger than 25.4 mm (1 inch) in diameter is:

(c) Illustration

Consider an ABEC 3 single row, radial ball bearing having 10 balls of 1/16" diameter, 0.330" inner race diameter and 0.452" outer race diameter in a single shield configuration.

This means that for a load of P =143 lbs. the rating life of this ball bearing will be one million revolutions and 90% of a group of such ball bearings will be expected to complete or exceed this value.

Suppose now it is desired to determine the "L₁₀" life of this bearing when operating at 200 RPM and a load of 50 lbs, the life being evaluated in hours of operation.

Let the life in hours be denoted by l₁₀ and let N denote the RPM of the bearing. We then have


Substituting N = 200, P = 50 and C = 143 into Equation (29), we obtain l₁₀ = 1949 hours.

NOTE: L₁₀ is bearing life in millions of revolutions l₁₀ is bearing life in hours.

A chart showing required life at constant operating speed has been given by N. Chironis ("Today's Ball Bearings", Product Engineering, December 12, 1960, pp. 63-77, chart on p. 68). This chart is hereby reproduced with the permission of McGraw-Hill Book Company, New York, N.Y.

(d) Combined Axial and Radial Loads

Such cases can be evaluated according to the methods previously outlined by combining the axial and radial loads into an equivalent radial load. This is defined in ANSI/AFBMA Standard 9, 1978 as follows:

"Calculation of Equivalent Radial Load. The magnitude of the equivalent radial load P, for radial and angular contact bearings, under combined constant radial and constant thrust loads, is:

P = XF_r + YF_a

Values of X and Y are given in Table 4.

The rating and sizing of ball bearings involve many considerations, many of which are beyond the scope of this introductory presentation. For further information the reader is reffered to the technical literature.

(6.0) Tolerances and Clearances

For satisfactory operation of ball bearing, suitable shaft and housing tolerances are extremely important. Standard tolerance ranges have been established by the industry and Tables 5 and 6 show recommended deviations of shaft diameters and housing bores from nominal.

For normal conditions the recommendations of many manufacturers for rotating shafts and stationary housings, as given by Wilcock and Booser*, recommend fits in the approximate range K5 and J6 for shaft fits, and J6 and H7 for housing fits.

A fuller discussion of tolerances and their relation to bearing applications, installation and design is a complex subject beyond the scope of this presentation. This would include considerations involving temperature effects, high-speed operation, shock loading, lubrication, environmental conditions etc. For a discussion of such topics the reader is referred to the technical literature.

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* "Bearing Design and Application" by D.F. Wilcock and E.R. Booser, McGraw Hill, New York, N.Y., 1st Ed., 1957. p.69

D cos α dm	Single Row Radial Contact; Single & Double Row Angular Contact, Groove Type(1)		Double Row Radial Contact Groove Type		Self-Aligning
	Metric (2)	Inch (3)	Metric (2)	Inch (3)	Metric (2)	Inch (3)
0.05	46.7	3550	44.2	3360	17.3	1310
0.06	49.1	3730	46.5	3530	18.6	1420
0.07	51.1	3880	48.4	3680	19.9	1510
0.08	52.8	4020	50.0	3810	21.1	1600
0.09	54.3	4130	51.4	3900	22.3	1690
0.10	55.5	4220	52.6	4000	23.4	1770
0.12	57.5	4370	54.5	4140	25.6	1940
0.14	58.8	4470	55.7	4230	27.7	2100
0.16	59.6	4530	56.5	4290	29.7	2260
0.18	59.9	4550	56.8	4310	31.7	2410
0.20	59.9	4550	56.8	4310	33.5	2550
0.22	59.6	4530	56.5	4290	35.2	2680
0.24	59.0	4480	55.9	4250	36.8	2790
0.26	58.2	4420	55.1	4190	38.2	2910
0.28	57.1	4340	54.1	4110	39.4	3000
0.30	56.0	4250	53.0	4030	40.3	3060
0.32	54.6	4160	51.8	3950	40.9	3110
0.34	53.2	4050	50.4	3840	41.2	3130
0.36	51.7	3930	48.9	3730	41.3	3140
0.38	50.0	3800	47.4	3610	41.0	3110
0.40	48.4	3670	45.8	3480	40.4	3070

1. 
   a. When calculating the basic load rating for a unit consisting of two similar, single row, radial contact ball bearings, in a duplex mounting, the pair is considered as one, double row, radial contact ball bearing.
   
   b. When calculating the basic load rating for a unit consisting of two, similar, single row, angular contact ball bearings in a duplex mounting, "Face-to-Face" or "Back-to-Back", the pair is considered as one, double row, angular contact ball bearing.
   
   c. When calculating the basic load rating for a unit consisting of two or more similar, single angular contact ball bearings mounted "in Tandem", properly manufactured and mounted for equal load distribution, the rating of the combination is the number of bearings to the 0.7 power times the rating of a single row ball bearing. If the unit may be treated as a number of individually interchangeable single row bearings, this footnote 1c does not apply.
   
   
2. Use to obtain C in newtons when D is given in mm.
   
   
3. Use to obtain C in pounds when D is given in inches.

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* Reprinted by permission of the American National Standards Institute, 1430 Broadway, New York, N.Y. 10018 (from ANSI-AFBMA Std 9-1978)

Required Life At Constant Operating Speed (data from SKF Industries)
Type of Machine	Life in Hours of Operation
Instruments and apparatus which are only infrequently used Ex.: demonstration apparatus, devices for operation of sliding doors	500
Aircraft engines	500 - 2000
Machines for service of short duration or intermittent operation, where service interruptions are of minor importance Ex.: hand tools, lifting tackle in machinery shops, hand-driven machines in general, farm machinery, assembly cranes, charging machines, foundry cranes, household machines	4000 - 8000
Machines for intermittent service where dependable operation is of great importance Ex.: auxiliary machines in power stations, conveying-equipment in production lines, elevators, general-cargo cranes, machine tools less frequently used	8000 - 12,000
Machines for 8-hour service which are not always fully utilized Ex.: machines in general in the mechanical industries, cranes for continuous service, blowers, jackshafts	20,000 - 30,000
Machines for continuous operation (24-hour service) Ex.: separators, compressors, pumps, main-line shafting, roller beds and conveyor rollers, mine hoists, stationary electric motors	40,000 - 60,000
Machines for 24-hour service where dependability is of great importance Ex.: pulp and paper machines, public power stations, mine pumps, public pumping stations, machines for continuous service aboard ship	100,000 - 200,000

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* Reproduced from "Today's Ball Bearings" by N. Chironis, Product Engineering, December 12, 1960, pp. 68 with the permission of McGraw-Hill Book Co. Inc., New York, N.Y.

Bearing Type				Single-Row Bearings		Double Row Bearings
Radial Contact Groove Ball Bearings	Fa / Co	Fa / IZD2		Fa / Fr > e		Fa / Fr ≤ e		Fa / Fr > e		e
		Units Newtons, mm	Units lbs. in.	X	Y	X	Y	X	Y
	0.014 0.028 0.056 0.084 0.11 0.17 0.28 0.42 0.56	0.172 0.345 0.689 1.03 1.38 2.07 3.45 5.17 6.89	25 50 100 150 200 300 500 750 1000	0.56	2.30 1.99 1.71 1.56 1.45 1.31 1.15 1.04 1.00	1	0	0.56	2.30 1.99 1.71 1.55 1.45 1.31 1.15 1.04 1.00	0.19 0.22 0.26 0.28 0.30 0.34 0.38 0.42 0.44
Angular Contact Groove Ball Bearings with Contact Angle 5°	iFa / Co	Fa / ZD2		For this type use the X,Y and e values applicable to single row radial contact bearings		1	2.78 2.40 2.07 1.87 1.75 1.58 1.39 1.26 1.21	0.78	3.74 3.23 2.78 2.52 2.36 2.13 1.87 1.69 1.63	0.23 0.26 0.30 0.34 0.36 0.40 0.45 0.50 0.52
		Units Newtons, mm	Units lbs. in.
	0.014 0.028 0.056 0.084 0.11 0.17 0.28 0.42 0.56	0.172 0.345 0.689 1.03 1.38 2.07 3.45 5.17 6.89	25 50 100 150 200 300 500 750 1000
10°	0.014 0.029 0.057 0.086 0.11 0.17 0.29 0.43 0.57	0.172 0.345 0.689 1.03 1.38 2.07 3.45 5.17 6.89	25 50 100 150 200 300 500 750 1000	0.46	1.88 1.71 1.52 1.41 1.34 1.23 1.10 1.01 1.00	1	2.18 1.98 1.76 1.63 1.55 1.42 1.27 1.17 1.16	0.75	3.06 2.78 2.47 2.20 2.18 2.00 1.79 1.64 1.63	0.29 0.32 0.36 0.38 0.40 0.44 0.49 0.54 0.54
15°	0.015 0.029 0.058 0.087 0.12 0.17 0.29 0.44 0.58	0.172 0.345 0.689 1.03 1.38 2.07 3.45 5.17 6.89	25 50 100 150 200 300 500 750 1000	0.44	1.47 1.40 1.30 1.23 1.19 1.12 1.02 1.00 1.00	1	1.65 1.57 1.46 1.38 1.34 1.26 1.14 1.12 1.12	0.72	2.39 2.28 2.11 2.00 1.93 1.82 1.66 1.63 1.63	0.38 0.40 0.43 0.46 0.47 0.50 0.55 0.56 0.56
20° 25° 30° 35° 40°				0.43 0.41 0.39 0.37 0.35	1.00 0.87 0.76 0.66 0.57	1	1.09 0.92 0.78 0.66 0.55	0.70 0.67 0.63 0.60 0.57	1.63 1.41 1.24 1.07 0.98	0.57 0.68 0.80 0.95 1.14
Self-aligning Ball Bearings				0.40	0.4 cot ∞	1	0.42 cot ∞	0.65	0.65 cot ∞	1.5 tan α

1. Two similar, single row, angular contact ball bearings mounted "Face-to-Face" or "Back-to-Back" are considered as one, double row, angular contact bearing.
2. Values of X,Y and e for a load or contact angle other than shown in Table 2 are obtained by linear interpolation.
3. Values of X,Y and e shown in Table2 do not apply to filling slot bearings for applications in which ball-raceway contact areas project substantially into the filling slot under load.
4. For single row bearings when F_a / F_r ≤ e, use X = 1, Y = 0.

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* Reprinted by permission of the American National Standards Institute, 1430 Broadway, New York, N.Y., 10018 (force ANSI-AFBMA Std. 9-1978).

Fit inner ring to shaft

Push fit

Push fit to wringing fit

Wringing fit

Drive fit

Light force fit

Force fit

Heavy force fit

Nominal diameter mm

g6

h6

h5

j5

j6

k5

k6

m5

m6

n6

p6

Over

Incl.

3

6

-0.0002 -0.0005

0 -0.0003

0 -0.0002

+0.0002 -0.0000

6

10

-0.0002 -0.0006

0 -0.0004

0 -0.0002

+0.0002 - 0.0001

+0.0003 -0.0001

10

18

-0.0002 -0.0007

0 -0.0004

0 -0.0003

+0.0002 -0.0001

+0.0003 -0.0001

+0.0004 +0.0000

+0.0005 +0.0000

18

30

-0.0003 -0.0008

0 -0.0005

0 -0.0004

+0.0002 - 0.0002

+0.0004 -0.0002

+0.0004 +0.0001

+0.0006 +0.0001

+0.0007 +0.0003

+0.0008 +0.0003

+0.0011 +0.0006

30

50

-0.0004 -0.0010

0 -0.0006

0 -0.0004

+0.0002 -0.0002

+0.0004 -0.0002

+0.0005 +0.0001

+0.0007 +0.0001

+0.0008 +0.0004

+0.0010 +0.0004

+0.0013 +0.0007

+0.0017 +0.0010

50

80

-0.0004 -0.0011

0 -0.0007

0 -0.0005

+0.0002 -0.0003

+0.0005 -0.0003

+0.0006 +0.0001

+0.0008 +0.0001

+0.0009 +0.0004

+0.0012 +0.0004

+0.0015 +0.0008

+0.0020 +0.0013

80

120

-0.0005 -0.0013

0 -0.0009

0 -0.0006

+0.0002 -0.0004

+0.0005 -0.0004

+0.0007 +0.0001

+0.0010 +0.0001

+0.0011 +0.0005

+0.0014 +0.0005

+0.0018 +0.0009

+0.0023 +0.0015

120

180

-0.0006 -0.0015

0 -0.0010

0 -0.0007

+0.0003 -0.0004

+0.0006 -0.0004

+0.0008 -0.0001

+0.0011 +0.0001

+0.0013 +0.0006

+0.0016 +0.0006

+0.0020 +0.0011

+0.0027 +0.0017

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* After SKF
** Reprinted by permission of McGraw-Hill Book Co. Inc., New York, N.Y. from "Bearing Design and Application" by D.F. Wilcock and E.R. Booser, 1st Ed., 1957, pp. 64-65

Fit housing – Outer ring		Close– Running fit	Slide fit		Push fit		Wringing fit		Drive fit		Heavy drive fit		Light force fit
Nominal diameter mm		G7	H8	H7	J7	J6	K6	K7	M6	M7	N6	N7	P6	P7
Over	Incl.
10	18	+0.0002 +0.0009	0 +0.0011	0 +0.0007	-0.0003 +0.0004	-0.0002 +0.0002	-0.0004 +0.0001	-0.0005 +0.0002	-0.0006 -0.0002	-0.0007 0	-0.0008 -0.0004	-0.0009 -0.0002	-0.0010 -0.0006	-0.0011 -0.0004
18	30	+0.0003 +0.0011	0 +0.0013	0 +0.0008	-0.0004 +0.0005	-0.0002 +0.0003	-0.0004 +0.0001	-0.0006 +0.0002	-0.0007 -0.0002	-0.0008 0	-0.0009 -0.0004	-0.0011 -0.0003	-0.0012 -0.0007	-0.0014 -0.0006
30	50	+0.0004 +0.0013	0 +0.0015	0 +0.0010	-0.0004 +0.0006	-0.0002 +0.0004	-0.0005 +0.0001	-0.0007 +0.0003	-0.0008 -0.0002	-0.0010 0	-0.0011 -0.0005	-0.0013 -0.0003	-0.0015 -0.0008	-0.0017 -0.0007
50	80	+0.0004 +0.0016	0 +0.0018	0 +0.0012	-0.0005 +0.0007	-0.0002 +0.0005	-0.0006 +0.0002	-0.0008 +0.0004	-0.0099 -0.0002	-0.0012 0	-0.0013 -0.0006	-0.0015 -0.0004	-0.0018 -0.0010	-0.0020 -0.0008
80	120	+0.0005 +0.0019	0 +0.0021	0 +0.0014	-0.0005 +0.0009	-0.0002 +0.0006	-0.0007 +0.0002	-0.0010 +0.0004	-0.0011 -0.0002	-0.0014 0	-0.0015 -0.0006	-0.0018 -0.0004	-0.0020 -0.0012	-0.0023 -0.0009
120	180	+0.0006 +0.0021	0 +0.0025	0 +0.0016	-0.0006 +0.0010	-0.0003 +0.0007	-0.0008 +0.0002	-0.0011 +0.0005	-0.0013 -0.0003	-0.0016 0	-0.0018 -0.0008	-0.0020 -0.0005	-0.0024 -0.0014	-0.0027 -0.0011
180	250	+0.0006 +0.0024	0 +0.0028	0 +0.0018	-0.0006 +0.0012	+0.0003 -0.0009	-0.0009 +0.0002	-0.0013 +0.0005	-0.0015 -0.0003	-0.0018 0	-0.0020 -0.0009	-0.0024 -0.0006	-0.0028 -0.0016	-0.0031 -0.0013
250	315	+0.0007 +0.0027	0 +0.0032	0 +0.0020	-0.0006 +0.0014	-0.0003 +0.0010	-0.0011 +0.0002	-0.0014 +0.0006	-0.0016 -0.0004	-0.0020 0	-0.0022 -0.0010	-0.0026 -0.0006	-0.0031 -0.0019	-0.0035 -0.0014
315	400	+0.0007 +0.0030	0 +0.0035	0 +0.0022	-0.0007 +0.0015	-0.0003 +0.0011	-0.0011 +0.0003	-0.0016 +0.0007	-0.0018 -0.0004	-0.0022 0	-0.0024 -0.0010	-0.0029 -0.0006	-0.0034 -0.0020	-0.0039 -0.0016
400	500	+0.0008 +0.0033	0 +0.0038	0 +0.0025	-0.0008 +0.0017	-0.0003 +0.0013	-0.0013 +0.0003	-0.0018 +0.0007	-0.0020 -0.0004	-0.0025 0	-0.0026 -0.0011	-0.0031 -0.0007	-0.0037 -0.0022	-0.0043 -0.0018
500	630	+0.0009 +0.0035	0 +0.0041	0 +0.0027	-0.0009 +0.0018	-0.0003 +0.0014	-0.0014 +0.0003	-0.0019 +0.0008	-0.0022 -0.0005	-0.0027 0	-0.0029 -0.0012	-0.0034 -0.0007	-0.0041 -0.0024	-0.0046 -0.0020

---

* After SKF
** Reprinted by permission of McGraw-Hill Book Co. Inc., New York, N.Y. from "Bearing Design and Application" by D.F. Wilcock and E.R. Booser, 1st Ed., 1957, pp. 64-65