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Calculating bearing stiffness based on preload

2.4 Selecting internal clearance and preload

2.4.1 Calculating bearing stiffness based on preload

Within this study the preload of the bearings is selected based purely on required stiffness of the bearings. The other aspects of the preload selection are neglected to keep focus on the rotor dynamics. Bearing stiffnesses are calculated using Rotor-Bearing Dynamics (RoBeDyn) toolbox for MATLAB -software. RoBeDyn toolbox is developed in LUT university and is used to simulate rotor and bearing dynamics. Package includes function to calculate bearing stiffnesses and thus is useful in this study. The bearing stiffness function is based on Hertzian contact theory and results are calculated using Newton-Raphson iteration. The stiffness calculation method is described in detail in following paragraphs.

In Figure 6 main dimensions of a ball bearing are presented. Where 𝑑 is ball diameter, π‘Ÿπ‘œπ‘’π‘‘ is the outer groove radius, π‘Ÿπ‘–π‘› is the inner groove radius, 𝑐𝑑 is the diametral clearance, π·β„Ž is

the bearing housing diameter, π‘‘π‘š is the pitch diameter, 𝑑𝑠 is the bore diameter, 𝐷𝑖 is the inner raceway diameter and π·π‘œ is the outer raceway diameter. (Kurvinen, et al., 2015, p. 13)

Figure 6. Main dimensions of a ball bearing (Kurvinen, et al., 2015, p. 13)

As described in article by E. Kurvinen et al. the elliptical contact conjunction is used to calculate contact stiffness between rolling elements and bearing raceway. Figure 7 the geometry of elliptical contact conjunction is shown with the normal force that acts on the solids. It is noteworthy that radius of contact conjunction is defined negative when surface is concave. (Kurvinen, et al., 2015, p. 11)

Figure 7. Elliptical contact conjunctions (Kurvinen, et al., 2015, p. 11)

Contact deformation are defined with aid of curvature sum, 𝑅 , and curvature difference, 𝑅𝑑, as shown in equations 13 & 14.

1

In case of angular contact bearing, the contact angle must be considered. Figure 8 shows a cross section of angular contact bearing. In Figure 9 the cross section is taken in plane that is colinear with the contact angle line. In Figure 8 πœ™ is the contact angle of the bearing, π‘Ÿπ‘π‘¦π‘–π‘› is the groove radius of bearing inner ring, π‘Ÿπ‘π‘¦π‘œπ‘’π‘‘ is the groove radius of bearing outer ring, π‘Ÿπ‘ is the radius of the bearing ball, and 𝑑𝑗 is the distance along contact line between the outer and inner raceways. In Figure 9 π‘Ÿπ‘π‘₯π‘œπ‘’π‘‘ is the radius of outer raceway and π‘Ÿπ‘π‘₯𝑖𝑛 is the radius of inner raceway.

Figure 8. Cross section of angular contact ball bearing geometry.

Figure 9. Contact plane cross section of angular contact ball bearing π‘Ÿπ‘π‘¦π‘œπ‘’π‘‘

π‘Ÿπ‘π‘¦π‘–π‘›

πœ™

π‘Ÿπ‘

𝑑𝑗

π‘Ÿπ‘π‘₯𝑖𝑛 π‘Ÿπ‘π‘₯π‘œπ‘’π‘‘

When contact angle is considered, the radiuses of the inner race are calculated as shown equation 17-19 (Kurvinen, et al., 2015, p. 12)

π‘Ÿπ‘Žπ‘₯𝑖𝑛 = π‘Ÿπ‘Žπ‘¦π‘–π‘› =𝑑

For outer raceway the corresponding equations are 20-22 (Kurvinen, et al., 2015, p. 12)

π‘Ÿπ‘Žπ‘₯π‘œπ‘’π‘‘ = π‘Ÿπ‘Žπ‘¦π‘œπ‘’π‘‘ = 𝑑

When stiffness of angular contact ball bearing is calculated equations 17-22 must be used in formulas 13 & 14 to retrieve curvature sum, 𝑅 , and curvature difference, 𝑅𝑑, that in turn, will be used in later calculations.

When a load is applied to the solids, contact point is expanded to an ellipse. The ellipticity parameter, π‘˜π‘’, is described as shown below, in equation 23 (Sopanen & Mikkola, 2003, p.

7).

In turn the ellipticity parameter is defined as shown in equation 24 (Sopanen & Mikkola,

Where elliptical integrals πœ‰ & 𝜁 are as follows

πœ‰ = ∫ [1 βˆ’ (1 βˆ’ 1 simplify calculation following approximated values can be used (Kurvinen, et al., 2015, p.

12) (Sopanen & Mikkola, 2003, p. 8)

π‘˜Μ…π‘’ = 1,0339 (𝑅𝑦

Where

𝐸′ is the effective modulus of elasticity πΈπ‘Ž is the modulus of elasticity for material a 𝐸𝑏 is the modulus of elasticity for material b π‘£π‘Ž is the Poisson’s ratio for material a 𝑣𝑏 is the Poisson’s ratio for material b

Using equations 27-30 shown above, the contact stiffness coefficient 𝐾𝑐 can be calculated with equation 31

𝐾𝑐 = πœ‹π‘˜Μ…π‘’πΈβ€²βˆš π‘…πœ‰Μ…

4,5πœΜ…3 (31)

Total stiffness of a single bearing ball can be calculated when contacts with inner and outer race are combined with equation 32 as shown below

πΎπ‘π‘‘π‘œπ‘‘ = 1

𝐾𝑐𝑖𝑛 is the contact stiffness between bearing ball and inner raceway πΎπ‘π‘œπ‘’π‘‘ is the contact stiffness between bearing ball and outer raceway

The ball bearing forces and moments can be calculated using the relative displacements of the raceways. The displacements of each bearing balls can be evaluated in radial direction using equation 33 and in axial direction with equation 34 (Kurvinen, et al., 2015).

π‘’π‘—π‘Ÿ= 𝑒π‘₯π‘π‘œπ‘ π›½π‘—+ 𝑒𝑦𝑠𝑖𝑛𝛽𝑗 (33)

𝑒𝑗𝑑 = π‘’π‘§βˆ’ (βˆ’π›Ύπ‘₯𝑠𝑖𝑛𝛽𝑗+ π›Ύπ‘¦π‘π‘œπ‘ π›½π‘—)(𝑅𝑖𝑛+ π‘Ÿπ‘–π‘›) (34)

Where

𝑒π‘₯ is relative displacement in x direction 𝑒𝑦 is relative displacement in y direction 𝑒𝑧 is relative displacement in z direction 𝛽𝑗 is the attitude angle of ball bearing j

𝛾π‘₯ is the relative misalignment of the inner and outer raceway about x axis 𝛾𝑦 is the relative misalignment of the inner and outer raceway about y axis

The displacements of raceways and bearing balls are visualised in Figure 10.

Figure 10. Axial and transverse cross-section in the A-A plane of illustrative structure of a ball bearing (Kurvinen, et al., 2015, p. 14)

The contact angle of a single bearing ball, πœ™π‘—, is expressed as shown in equation 35

πœ™π‘— = tanβˆ’1( 𝑒𝑗𝑑

𝑅𝑖𝑛+ π‘Ÿπ‘–π‘›+ π‘’π‘—π‘Ÿβˆ’ π‘…π‘œπ‘’π‘‘+ π‘Ÿπ‘œπ‘’π‘‘) (35) Where,

𝑅𝑖𝑛 is the radius of the inner raceway π‘…π‘œπ‘’π‘‘ is the radius of the outer raceway π‘Ÿπ‘–π‘› is the radius of the inner raceway groove π‘Ÿπ‘œπ‘’π‘‘ is the radius of the outer raceway groove

the distance between raceways along the contact line of the bearing 𝑑𝑗 is expressed by equation 36. (Kurvinen, et al., 2015, p. 16)

𝑑𝑗 = π‘Ÿπ‘œπ‘’π‘‘+ π‘Ÿπ‘–π‘›βˆ’π‘…π‘–π‘›+ π‘Ÿπ‘–π‘›+ π‘’π‘—π‘Ÿβˆ’ π‘…π‘œπ‘’π‘‘+ π‘Ÿπ‘œπ‘’π‘‘

π‘π‘œπ‘ πœ™π‘— (36)

The total elastic deformation of a single bearing ball, π›Ώπ‘—π‘‘π‘œπ‘‘, is calculated with equation 37 (Kurvinen, et al., 2015, p. 16)

π›Ώπ‘—π‘‘π‘œπ‘‘ = 2π‘Ÿπ΅βˆ’ 𝑑𝑗 (37)

Where π‘Ÿπ΅ is the radius of the bearing ball.

Then the forces acting on a single bearing ball, 𝐹𝑗, can be calculated using equation 38 (Kurvinen, et al., 2015, p. 16).

𝐹𝑗 = πΎπ‘π‘‘π‘œπ‘‘(π›Ώπ‘—π‘‘π‘œπ‘‘)

3

2 (38)

The forces of each individual bearing ball can be combined to form bearing forces of the whole ball bearing using equations 39 – 43 (Kurvinen, et al., 2015, p. 16). Sum of forces and

moments should include only components where bearing balls are under compression (Sopanen & Mikkola, 2003, p. 12).

𝐹𝑋 = βˆ’ βˆ‘ πΉπ‘—π‘π‘œπ‘ πœ™π‘—π‘π‘œπ‘ π›½π‘— 𝑧 is the number of bearing balls

In the RoBeDyn toolbox for MATLAB the bearing displacements are calculated using Newton Raphson iteration with equation 44.

𝒆(𝑛+1)= 𝒆(𝑛)βˆ’ (𝑲𝑇(𝑛))βˆ’1𝑸(𝑛) (44)

Where

𝒆(𝑛+1) is matrix containing the displacements of the bearing on iteration step 1+n 𝒆(𝑛) is matrix containing the displacements of the bearing on iteration step n 𝑲𝑇(𝑛) is the tangent stiffness matrix vector on iteration step n

𝑸(𝑛) is matrix containing the forces acting on bearing on iteration step n

bearing forces 𝑸(𝑛) include bearing and external forces as described in equation 45

𝑸(𝑛) = 𝑸𝑏(𝑛)βˆ’ 𝑸𝑒π‘₯𝑑(𝑛) (45)

Where

𝑸𝑏(𝑛) is the matrix of bearing forces 𝑸𝑒π‘₯𝑑(𝑛) is the matrix of external forces

External forces include bearing preload forces and thus amount of preload is factor when calculating bearing stiffness.

The stiffness matrix for each iteration step, 𝑲𝑇(𝑛), is presented in equation 46

𝑲(𝑛)𝑇 =πœ•π‘Έ(𝑛)

πœ•π’†(𝑛) (46)

Newton Raphson iteration is continued until convergence criterion, shown in equation 47, is met

|𝑸| < πΎπ‘π‘œπ‘›π‘£βˆ™ |𝑸𝒆𝒙𝒕| (47)

Where

πΎπ‘π‘œπ‘›π‘£ is the convergence criterion factor

Bearing stiffness matrix π’Œπ‘ is the tangent stiffness matrix from last converged iteration step.

From E. KrΓ€mer’s book we can retrieve an estimation for damping factor in rolling element bearings. The damping matrix of the bearing is estimated as shown in equation 48. (KrΓ€mer, 1993)

𝒄𝒃 = (0,25 … 2,5) βˆ™ 10βˆ’5π’Œπ’π’Šπ’ (48)

where

𝒄𝒃 is the damping matrix of the bearing

π’Œπ‘™π‘–π‘› is the linearized stiffness of the bearings in N/mm

A constant is chosen within the limits shown in equation 48. For calculating damping matrices, the equation 49 is used.

𝒄𝒃 = 2,5 βˆ™ 10βˆ’5π’Œπ’ƒ (49)

Similar calculation method specifically for angular contact bearings has been introduced by Noel, et al. in their study (2013). In their study this method has proven good results with not considerable increase in calculation effort. (Noel, et al., 2013) Since RoBeDyn -toolbox was available to use, the effort of implementing analytical method was considered to be out of scope of this study.

The procedure of bearing stiffness calculation using RoBeDyn MATLAB toolbox is presented in flowchart in Figure 11.

Figure 11. Flowchart bearing stiffness calculation using RoBeDyn-toolbox