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    Chapter 12

    Lubrication &Journal bearings

    (7(7 -- 8 Lectures)8 Lectures)

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    TOPICS

    1. Definitions and Objectives 2. Types of Lubrication3. Dynamic Viscosity

    4. Bearing Characteristic Number5. Stable & Unstable Lubrication6. Hydrodynamic Lubrication

    7. Design Considerations QUIZ48. Heat Balance-Self-Contained Bearings9. Clearance

    10. Pressure-Fed Bearings11. Loads and Materials12 Boundary lubrication

    13. Types of Journal Bearings

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    Definitions and objectives

    The role of a bearing is to provide relative positioning and rotational freedom while transmittinga load between a shaft and a housing.

    There are two general types of bearings:1. Rolling-contact bearings (anti-friction bearings, rolling

    bearings). In the rolling-contact bearings the load istransmitted by rolling rather than by sliding.

    2. Journal Bearings (plain bearings, bushings, sleeve bearings). In journal bearings, the load is transmitted bysliding and the problem of this class of bearings isessentially a lubrication problem .

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    Definitions and objectives

    Journal Bearings : cylindrical or semi-cylindrical bushing made of a suitable material .

    The Journal is the part of shaft or pin in bearing

    Among applications :1. High speed, high temperature, high varying loads:

    Automotive engines: connecting rod, crankshaft, Metal alloys Turbo machinery: Metal alloys

    2. Light loads, low speeds with little or no lubrication: Nylon, Teflon, rubber

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    Types of Lubrication

    1. Hydrodynamic Lubrication(HDL)(a) Full, thick Fluid film lubrication - surfaces

    separated by bulk lubricant film; Filmconditions required for lubrication.

    2. Boundary (Thin Film)Lubrication(b) partial lubrication ( mixed) - both bulklubricant and boundary film play a role; (c)

    boundary lubrication - performance dependsessentially on boundary film

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    3. HydrostaticLow speed, light load

    4. Elastohydrodynamic

    For rolling contact(gears, rolling bearings)

    5. Solid FilmExtreme Temperatures

    (Graphite or Molybdenum disulfide))

    Types of Lubrication

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    Viscosity(HDL)Shear Stress

    dydu

    AF

    ==

    is absolute or dynamic viscosity(lbf.s/in 2 or reyn . In ips system and

    Pa.s in SI system)

    du/dy is the rate of shear or velocitygradient

    If rate of shear is constant: du/dy = U/hWith h= c (clearance)

    c=

    Fig. 12.1

    cU

    hU

    AF

    ===

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    Viscosity vs. temperature

    In general, Viscosity decreases with temperature increase.The increase in temperature comes from friction

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    Petroffs Law

    =

    ===

    ==

    ==

    ==

    = cr

    P N

    f s f

    f

    s

    s

    T T

    rlW

    Pr lPr f fWr T

    clN r

    lr T

    rl Ar AT

    crN

    cU

    22

    2;)2(

    4)(2

    2;)(

    2

    322

    Bearing Characteristic Number (Sommerfeld Number )

    S cr f

    c

    r

    P

    N S

    22

    2

    =

    =

    Petroff used a concentric shaft to define a group of dimensionless parametersThat allow the prediction of an acceptable coefficient of friction .

    r/c = clearance ratio

    Shear torque in lubricant

    Friction torque

    S bl d bl l b i i

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    0.08-0.14For steel onBronze

    a

    bc

    12

    1

    2 f = 0.001-0.005Similar to precision BB

    Stable and unstable lubricationThe McKee Brothers Plot

    (a) Full, thick Fluid filmlubrication - surfacesseparated by bulk lubricantfilm; Film conditions requiredfor lubrication.

    (b) partial lubrication ( mixed) - both bulk lubricant and boundary film play a role;

    (c) boundary lubrication -

    performance dependsessentially on boundary film

    Boundary lubrication should be expected for slow speeds:

    U

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    Hydrodynamic Lubrication (HDL)

    For lubricated bearingthe minimum film

    thickness h 0 occurs tothe left of load line because the shaft is

    pushed by the pressure build up on the right.The shaft is playing therole of a pump.

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    Hydrodynamic Lubrication (HDL)Nomenclature

    Fig. 12.6

    1. e: eccentricity

    2. h 0 minimum film thickness3. = e/c = eccentricity

    ratio

    4. bearing angular length

    H d d i L b i ti (HDL) Th

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    Tower investigated bath-type lubrication in 157

    partial bearing. He was ableto determine the pressuredistribution in oil film inaxial and radial directions.

    Reynolds used Towersfindings to propose arelationship betweenfriction, pressure andvelocity. His work is given

    under mathematical form inthe following.

    Hydrodynamic Lubrication (HDL)-TheoryB. Tower

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    Hydrodynamic Lubrication (HDL): theoryO. Reynolds

    Assuming pressure varies in x-direction only (no leakage)

    Assuming Velocity varies in x & y directions

    )1(

    0

    ydxdp

    dxdzdx y

    dxdz pdydzdydzdxdxdp pFx

    =

    =+++=

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    Hydrodynamic Lubrication (HDL): theory

    Assuming Newtonian viscous fluid + u = u(x,y)

    Assuming Constant viscosity and substituting Eq. (1) into (2):

    Integrating (3) twice (holding x constant):

    Assuming no slip at boundaries :

    )2( yu

    =

    )3(12

    2

    2

    2

    dxdp

    yuor

    yu

    dxdp

    =

    =

    )4(1 2122

    C yC ydxdpu ++=

    )5(@

    00@0

    1

    2

    === 2

    ===dphU

    C h yU u

    C yu

    dxh

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    The velocity distribution in film is:

    Flow rate/unit width:

    Incompressible flow:

    The above is the Reynolds Eq . For one-dimensional flow.

    Considering Leakage (2-D):

    Hydrodynamic Lubrication (HDL): theory

    ( ) )6(21 2 yhU hy yu dxdp +=

    )8(0 adxQd

    =

    )1112(633

    =+

    dx

    dhU z

    ph

    z x

    ph

    x

    )7(122

    3

    0 dxdphUh

    udyh

    Q ==

    )1012(63

    =

    dx

    dhU

    dx

    dph

    dx

    d

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    Hydrodynamic Lubrication (HDL):Theory

    There are no general analytical solutions tothe 2-D Reynolds Equation.

    The Summerfeld Solution to Eq. 12-11

    )1212(2

    = P N cr f cr

    S

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    Design ConsiderationsTwo groups of variables in the design of sliding bearings (eq:12.12)

    A- The independent variables :1. The viscosity ,2. The load per unit of projected bearing area, P (unit Load)

    3. The speed N= N J (see equation 12-13)4. The bearing dimensions r, c, and l ( important l/d )B- The dependent Variables or performance factors :

    1. The coefficient of friction f 2. The temperature rise T3. The volume flow rate of oil Q

    4. The minimum film thickness ho

    The first (A) are somewhat under designer control and the second (B) are not. Certainlimitations should be set for variables B and A varied to satisfy them

    )1212(2

    =P N

    cr f

    cr

    General Design Criteria for Journal Bearings

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    General Design Criteria for Journal Bearings( See Lab Manual for details )

    1. The value of the important parameter l/d is taken between 0.25 and 1.5 . Values up to 2 and 3 were usedin earlier designs. Nowadays, the value of l/d is

    confined between 0.25 and 0.75 . Short bearings are preferred when shaft deflections and misalignments areexpected.

    2. The nominal value of clearance ratio r/c can be takenapproximately as:

    1000 for precision bearings when 25< d

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    General Design Criteria for Journal Bearings

    ( See Lab Manual for details )

    3. The minimum film thickness h0 can be estimated fromTrumplers design criteria :

    or

    4. The outlet temperature of the oil should be kept below250 F (121 C). A value around 70 C (160 F) is usuallyspecified as the average operating temperature.

    5. Starting unit load P st=W st /ld is kept below 300 psi6. Design factor on starting load should be at least 2.

    )(0004.0005.0)(00004.00002.0

    0

    0

    mmd h

    ind h

    + +)(00025.00 ind h =

    Relationship bet een ariables

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    Relationship between variables

    Viscosity ChartsIn IPS units

    Relationship between variables

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    Relationship between variables

    Viscosity ChartsIn SI Units

    Relationship between variables

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    Relationship between variables

    Viscosity Charts

    Relationship between variables

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    Relationship between variables

    Minimum Film Thickness &Eccentricity ratio Chart

    Opt ima l de s ignZ one

    Relationship between variables

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    Relationship between variables

    Minimum Film Thickness Angular position vs. S

    Relationship between variables

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    Relationship between variablesCoefficient of friction variable vs. S

    Relationship between variables

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    Relationship between variablesFlow variable vs. S

    Relationship between variables

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    p

    Maximum pressure ratio vs. S

    Relationship between variables

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    pTerminating Position of film pressure & maximum film pressure vs. S

    Relationship between variables

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    pLubricant Temperature rise T

    )(211

    2a

    QsQT QC T sQQC T QC p ps ploss H

    =+=

    Taking T 1 as reference temperature:

    )(Pr 42 bc fr

    J lNc

    J TN

    loss H ==The heat loss due to friction

    ( ) ( )[ ] )(

    //5.01/

    4c

    rcNlQQsQc fr

    P

    C J T p

    =

    Equating (a) to (b)

    ( ) ( )[ ] )1512(//5.01/70.9

    =

    rcNlQQsQc fr

    P psiF

    T With = 0.0311 lbm/in 3 &

    C p = 0.42 Btu/lbm. F for petroleum lubricantsand J=9336 lbf.in/Btu

    Relationship between variables

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    pLubricant Temperature rise vs. S

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    Sample problems on HDLThe analysis problems are of two general categories:1) When the viscosity is specified as in example 12-

    1 through 12-4 of 7 th ed. The solution is straight

    forward.

    2) The problem becomes more complex when only the

    lubricant inlet temperature is specified. To solvethis type of problem an iterative procedure has to

    be followed. An example of the procedure is

    given in the following.

    Sample problems on HDL

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    p pProblem 12:3: Given T av=T operating =150 F

    Solution : to find any of the performance factors we need to havethe bearing characteristic number : S .

    1.65

    l bl

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    Sample problems on HDL

    Problem 12:3: Continued

    Problem # 12-12 (Modified)

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    ( )A 2-1/2 x2-1/2-in sleeve bearing uses grade 20 lubricant. The axial-

    groove sump has an inlet temperature of 110 F . The shaft journalhas a diameter of 2.500 in and the radial clearance is 0.002 in. lf

    journal speed is 1120 rev/min and the radial load is 1200 Ib f .Estimate

    (a) The magnitude and location of the minimum oil-film thickness.(b) The eccentricity.(c) The coefficient of friction.(d) The power loss rate.(e) Both the total and side oil-flow rates.(f) The maximum oil-film pressure and its angular location.(g) The terminating position of the oil film.(h) The average temperature of the side flow.(i) The oil temperature at the terminating position of the oil film.

    Given : d = 2 5 in b = 2 504 in c = 0 002 in W = 1200 lbf SAE = 20Problem # 12-12

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    Given : d = 2.5 in, b = 2.504 in, c min = 0.002 in, W = 1200 lbf, SAE = 20,T 1 = 110F,N = 1120 rev/min, and l = 2.5 in.

    Required (see list)

    Solution : to find any of these performance factorswe need to have the bearing characteristicnumber : S .

    To find average viscosity ( From Fig. 12-11; 12) we need to have

    the average operating film temperature T f (Eq. 12-14) :Procedure: (good for IPS and SI system)1. For a first trial assume T = (General) 20 80 F ( 10-50C )

    For our case take T = 40 F2. T f =130 F

    ( ) avavavavP N

    cr

    S

    42 108.3192

    67.18625

    5.25.21200

    67.182

    002.25.12

    ==

    ==

    21T

    f T T +=

    Problem # 12-12

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    3. Find av = 3.8 reyn (From Fig. 12-11; 12) using T f = 130F

    4. Calculate S = 3.8x104x3.8x10

    -6= 0.144

    5. Calculate TF or TC using 12-18 or Fig 12-23; 24 withS=0.144 and l/d =1

    6. Recalculate T fcal = 110+25.7/2 122.85 F7. Compare T fcal to T fassum if |difference| less than 6 F or 3 C

    Recalculate, For our case Tfassum -Tfcal = 130-122.85= 7.15 >6 Fneed to re-iterate:

    1 assume T =30 F2 T f = 125F 5 TF 27 F3 av 4.3 reyn 6 T fcal = 110+27/2 123.5F4 S 0.163 7 T fassum -T fcal = 125-

    123.5=1.5

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    av = 4.3 reyn (From Fig. 12-11 for oF; 12 for oC) using T f= 125F yielding S=0.163

    a) Using Fig 12- 16 with S=0.163 and l/d =1

    h0/c = 0.49 h

    0= 0.0098 in

    Using Fig 12- 17 = 56 b) e= c- h0 =.002-.00098 = 0.001in. or using Fig. 12-

    16 =e/c = 0.5 e = 0.001 in .c) f :Fig 12- 18 (r/c)f= 4f = 4/625=0.0064

    d) Power loss: H=(2 TN)/(778x12)= (2 fWrN)/778x12=H = 0.121 Btu/s =436 Btu/hr H = 126 j/s=453 KJ/hr

    Problem # 12-12

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    e) Using Fig 12- 19 with S=0.163 and l/d =1 Q/rcNl = 4.15 Q = 4.15x1.25x0.002x18.67x2.5=0.48

    in3/sUsing Fig 12- 20 Q s /Q=0.61 Q s = 0.29 in 3/s

    f) Using Fig 12- 21 P/P max = 0.44 P max = 192/0.44=436psig

    g) Using Fig 12- 22 Pmax

    = 18 & p0

    = 82 h) See part (a) Tav = 125F

    i) T2= 110+30=140 F

    NOTE: In cases where l/d curve is not available the interpolationequation (12- 16)

    may be used when necessary.

    Sample problem on Design of HDL Journal

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    Sample problem on Design of HDL JournalBearings ( to be solved during help session )

    Design a journal bearing to carry a radial load of1500 lb while the shaft rotates at 850 rpm. Theshaft stress analysis determines that the minimumacceptable diameter at the journal is 2.10 in.

    The shaft is part of a machine requiring good precision.

    Power loss in the bearing should not exceed 1% ofthe 15 hp driving power.

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    Procedures for design of oil lubricated journal

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    bearings

    Step2 : The value of the important parameter l/d istaken between 0.25 and 1.5 . Values up to 3 wereused in earlier designs. Nowadays the value of l/d isconfined between 0.25 and 0.75 . Short bearings are

    preferred when shaft deflections and misalignmentsare expected.

    Step3 : The minimum film thickness h0 can beestimated from one of these equations:

    )(0004.0005.0

    )(00004.00002.0

    0

    0

    mmd h

    ind h

    +

    +)(00025.00 ind h =

    Procedures for design of oil lubricated journal

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    bearings

    Step4 : The nominal value of clearance ratio r/c (r = bearing radius and c = clearance) can be takenapproximately as:1000 for precision bearings when 25< d

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    bearings

    Step5 : Now the bearing characteristic number ( S =Sommerfeld number) can be determined from thechart of Fig. 12.164 .

    Step6 : Next, the viscosity of the oil is determinedusing:

    Where:

    P (unit load) = W/ld, with W being the applied load. N = speed in revolutions per second.

    N P

    r cS

    2

    =

    Procedures for design of oil lubricated journal

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    bearings Step7 : The outlet temperature of the oil should be kept

    between 200 F (93 C ) and 250 F (121 C). A value of 70 C(160 F) is usually specified as the average operatingtemperature [2, 9, 18-20]. The chart of Fig 12-11 or 12-12[3,4]) can be entered to select an oil grade. If the selectedlubricant has a viscosity higher than the value computed instep 6, recalculate S and find the new h0.

    Step8: Now, find the friction coefficient from Fig. 12-17 . Thefriction coefficient should be kept as low as possible consistentwith h0 (i.e. in the optimum zone between the minimumfriction line and the maximum load line in Fig. 12.14 [3,4]. Asa general rule friction coefficients below 0.01 are acceptable(see Table 28-1 of the Standard Handbook of Machine Design[5]).

    Procedures for design of oil lubricated journalb

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    bearings

    Step9: Power loss due to friction can be calculatedfrom:

    Its value can be compared to the input power to take adecision concerning f and h0.

    Step10: Select a suitable bearing material from Table 12-5[3,4] or from Tables 28-2 to 28-4 of the Handbook [5]. Unit

    load, maximum operating temperature and conditions should be used as criteria for material selection.

    Step11: Write a summary of your design results .

    )(1050

    hp fWrN

    H =

    Self-Contained Bearings

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    Pillow-blocks or pedestal bearings are used for:

    Fans,BlowersPumps and small motors

    Examples of Pillow-blocks withPolymer Bearings

    Ring oiled bearing

    Self-Contained BearingsTwo general types of lubrication: 1) Oil-Ring and 2) Oil Bath

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    Since the warm lubricant stays within the bearing housing ; it shouldbe designed such that the heat generated by friction is dissipated.

    As seen above the heat generated (in Btu/s ) by friction can be estimated:

    )(Pr 42 bc

    fr

    J

    lNc

    J

    TN gen

    H ==

    Where J= 9336 in.lbf/Btu

    The heat to be dissipated & surface temperature of housing (=T bearing ) are respectively:

    )19;1712(1

    )19;1712()(

    1bb

    T T T

    aaT T A

    f b

    f CR

    loss H

    ++=

    +=

    h

    )(1050

    hpin fWrN gen

    H =

    See Eq. 12-18 for CR =

    Combined overall coef. Of rad-conv.=2, 2.7,5.9 Btu/(hft 2 F)

    and Table 12-2 for

    Or in ( hp )

    T f is the average film temperature which is unknown and found bytrial and error to satisfy Hgen =H loss as in the following example.See also (Eq. 12-20) for T f

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    Example on self-contained bearings

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    Ring oiled bearing

    Example on self contained bearings

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    Example on self-contained bearings

    ClearanceAmong the independent variables under designers control, clearance is the

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    Among the independent variables under designer s control, clearance is themost difficult to hold accurate during manufacture and It may also increase

    during service because of wear .When selecting a clearance for a JB a number of performance variablesand expected in service wear should be taken into account.

    Bearing Noisy+h0 decreases

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    Clearance

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    Temperature limits for mineral oils

    Oils with antioxidants + O 2 supply unlimited

    O 2 insignificant

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    Pressure-Fed BearingsUnit load

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    Unit load

    w

    ( )

    =

    ==

    2'

    2312'4'2

    2/

    wll

    rlW

    rlW P

    Velocity Profile

    ( ) )2112(4'822

    = ycl p

    u s

    Pressure-Fed Bearings

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    Example of pressure-fedGrooved bearings

    Centrally located full annular groove

    Circumferential groove axial pressuredistribution

    Pressure-Fed BearingsPressure-Fed lubricantNatural circulation of oil

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    Use charts with l/d

    )6(21 2

    yhU

    hy yu dxdp

    =

    '8

    )2112(4'82

    max

    22

    lc pu

    ycl p

    u

    s

    s

    =

    =

    ( ) )2212(5.11'3

    23

    +=

    l

    rc psQ

    s

    ( )2312'4'2

    2/ ==rl

    W rl

    W PrlW

    P 2=

    Q s from Fig. 12-20

    Velocity

    Side-Flow

    Unit load

    Use charts with l/d

    ( )

    ( )( )( )

    )2512(5.11

    /)10(978

    )2412(5.11

    /0123.0

    42

    26

    42

    2

    +

    =

    +

    =

    r pW S c fr T

    r p

    W S c fr T

    s

    C

    s

    F

    Temperature rise

    T from Fig. 12- 24

    Example on Pressure-Fed Bearings

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    Problem 12-16 (modified)

    An eight-cylinder diesel engine has a frontmain bearing with diameter 3.5 in. and length2 in. The bearing has a central annular oilgroove 0.250 in. wide. It is pressure-lubricated

    with SAE 30 oil at an inlet temperature of180F and at a supply pressure of 50 psi.Corresponding to a radial clearance of 0.0025

    in, a speed of 2800 rev/min, and a radial loadof 4600 lb, find the temperature rise and theminimum oil-film thickness.

    Given : d = 3 .5 in, l = 2 .0 in, P s = 50 psi, w = 0.25 in; c min= 0 0025 in W = 4600 lbf SAE 30 T = 180F; N = 2800

    Problem # 12-16 (modified)

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    = 0 .0025 in, W = 4600 lbf, SAE 30, T 1 = 180 F; N = 2800

    rpm Required: TF, h 0 , P max , Pmax & p0

    Solution: Use Eq. 12-24 to compute TF

    psirl

    W P

    cr

    inwl

    l

    751875.075.14

    4600'4

    7000025.0

    75.1

    875.02

    '

    =

    ==

    ==

    ==

    )( )

    )2412(5.11

    /0123.042

    2

    +

    =r pW S c fr T

    s

    F

    ( ) avavP

    N

    cr avS

    410045.375160

    28002700

    2 ===

    Problem # 12-16

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    1. For a first trial assume T = 30 F2. T f = 180+30/2 = 195 F3. Find av = 1.4 reyn (From Fig. 12-12) using T f = 195F4. Calculate S = 0.04265. Use S = 0.0426 and l/d = to find = 0.93 from Fig. 12-16 & (r/c)f

    = 2.2 from Fig. 12-18

    6. Calculate TF

    6. T fcal = 180+22.64/2 191.3 F7. Compare T fcal to T fassum if |difference| >6 F Recalculate,

    For our case Tfassum -Tfcal = 195-191.3= 3.7

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    Using Fig 12- 16 with S=0.0426 and l/d =1/4h0/c = 0.07 h0 = 0.000175 in

    Trumpler Trumpler ss Criteria satisfied?Criteria satisfied?1)1) hh

    0 0 0.0002+0.00004(3.5)=0.00034 in0.0002+0.00004(3.5)=0.00034 in not satisfied?not satisfied?

    2)2) T T max max = T = T ss ++ T= 180+22.64=202.64T= 180+22.64=202.64 FF

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    A- Loads : Typical values of unit load P

    JOURNAL BEARING LOADS & MATERIALS

    B- Materials : To minimize wear of journal bearings, Metallic

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    j g ,

    Materials (Table 12-6 for Hydrodynamic Lubrication and 12-7for Boundary Lubrication) are selected for:1. Mechanical Properties

    Conformability : to compensate for small shaft misalignmentsand deflections (i.e. Low E and yield: Lead base Babbit=90%Pb + 10% Cu)

    Embeddability : to allow foreign particles to becomeembedded into the bearing which prevents scratching of shaftand sleeve (Tin base and Lead base Babbit )

    High Fatigue Strength : to support the compressive cyclicloading (Trimetal, Silver, Steel base, Solid Brass)

    JOURNAL BEARING MATERIALS2. Thermal Properties

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    High Thermal Conductivity : to remove heat rapidly from thebearing (Ag, Cu, Pb ). Thermal Coefficient of Expansion not too different from that

    of casing and shaft.3. Metallurgical Properties

    Compatibility : to avoid fusing under heat and contactdissimilar materials (Mainly not same melting point ) for shaftand bearing are more compatible than similar materials.

    4. Chemical Properties Corrosion Resistant : to resist corrosion by lubricant

    improvement additives (Sn, Al, Ag...).

    Non-Metallic Materials (Table 12-6) such as Wood, Rubber, CarbonGraphite, Derlin, Teflon, Nylon Most have low thermalconductivity.

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    Boundary Lubricationthin-film, Olite, Oiles, bushed pin

    In certain applications boundary lubrication should be

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    In certain applications boundary lubrication should bedesigned for ( see your lab manual and earlier notes andexample for the procedure of boundary lubrication design ).

    Boundary lubrication should be expected for slow speeds ( start

    ups and shut downs) : U

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    Mix animal or vegetable oils with lubricantUse porous metallic materials (Table 12-7)Use non-metallic materials (Table 12-8)Use indented bearings

    K in Table 12-8 and f 1 and f 2 in tables 12-10 & 12-11

    ( )2712)(21 == PV K f f t wratewear

    JOURNAL BEARING MATERIALS-Boundarylube

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    JOURNAL BEARING MATERIALS-Boundary lubrication

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    Sample problem on Design of Boundary-LubricatedJournal Bearings

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    g

    Design a boundary lubricated plain-surface bearing to carry a radial load of 2.5 kN from ashaft rotating at 1150 rpm. The nominal minimumdiameter of journal is 75 mm.

    Given: Boundary lubricated JB. W=2.5 kN; n= 1150 rpm ;d = 75 mm

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    Solution : 0.25< l/d

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    (Plain Bearings, sleeves)

    Radial

    Thrust Journal Bearing

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    Thrust

    Journal Bearings

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    Types of bearings

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    Plain Bearings

    Journal Bearings

    Self-lubricated Journal Bearings

    Bushes Polymer Bearings

    Types of Bearings

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    Radial Journal Bearings for PinionShaft in Gear Box for GE Turbine

    ESCOSA-DAMMAM

    Types of Bearings

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    Housing for Gear Boxshowing Radial JournalBearing Supports

    Types of Bearings

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    Radial Journal Bearings for PinionShaft in Gear Box for GE Turbine

    Types of Radial Journal Bearings

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    Types of Radial Journal Bearings

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    Types of Radial Journal Bearings

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    Typical Groove Patterns

    Thrust Journal Bearing

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    Thrust Journal Bearing

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    Thrust Bearing for GETurbine Shaft