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( ) ( )
++++= sfihfoff ErrE
rrErrE
rrpr 22
22
22
22
r
Through interference fit torque can be transmitted, which can be estimated
( ) ( ) sifshfoh ErrEErrE,
with a simple friction analysis at the interface. ( ) = coefficient of ( )
( )LdpFApNF
fff
ff
=== coefficient of friction( )
LdpTTorque
p
f
fff
2
2
= Abrasion Adhesion
211/19/2011 1
C.A.Coulomb 17811)Clearly distinguished between static & kinetic friction
2)Contact at discrete points.) p
3)Friction due to interlocking of rough surfaces
4)No adhesion5)f func(v)
11/19/2011 2
5)f func(v)
PLOUGHING Eff tPLOUGHING Effect
Assume n conical asperities of hard metal in contact with flat soft metal, vertically project area of contact: y p j
( )2*5.0 rnA =
HrnW )*5.0( 2= HnrhF )(=
cot2= Slope of real surfaces are always less than 10 (i.e. > 80), therefore <
0 1 11/19/2011 3
0.1.
ADHESION Theory
Two surfaces are pressed together under load W.
They deformed until area of contact (A) is sufficient to support y ( ) ppload W. A = W/H.
To move the surface sideway, must overcome shear strength of y, gjunctions with force F F = A s 4
Hs=11/19/2011
Aim: To reduce shear strength of interface
LUBRICATION Process by which the
friction in a moving contact is reduced. Six distinct form of l b i i lubrication are: Hydrodynamic Hydrostatic Elastohydrodynamic Mixed Boundary S lid fil
11/19/2011 5
Solid film
11/19/2011 6
FLUID FILM >5FLUID FILM BEARINGS
>5
Machine elements designed to produce smooth (low friction) motion between solid surfaces in relative motion and to generate a load support for mechanical and to generate a load support for mechanical components. Fluid between surfaces may be a gas, liquid or solid. Word film implies that fluid thickness (clearance) separating
the surfaces is several orders of magnitude smaller than other dimensions of bearing (width & length).
Successful design requires film thickness to be larger than the micro asperities on the surfaces, operation without contact of surfaces.
Operation principles of liquid film bearings are hydrodynamic, hydrostatic or combination.
11/19/2011 7
Hydrodynamic Hydrostatic
4/6/8 pockets
A i l diAxial coordinate Axial coordinateAxial coordinate
11/19/2011 8
Hydrodynamic HydrostaticRelative motion between two External source of pressurized Relative motion between two mechanical surfaces is utilized to generate pressure and levitate one surface relative to other
External source of pressurized fluid is required to levitate the one surface and separate it from other surface Costlyone surface relative to other
surface. Self-actingfrom other surface.. Costly
Load support is a strong function f l b
Load support is a weak function of lubricant viscosity. of lubricant viscosity.HDL provides an infinite bearing life
Infinite life if supporting ancillary equipments function welllife equipments function well
Able to damp the external vibrations.
Able to control the effect of external vibration.. Active control
Significant difference in static & kinetic friction coefficients
Almost same value of coefficient of frictions.
High relative speed generates much higher load capacity &
Very good control on the shaft position.g p y
destabilize the shaft-system.p
11/19/2011 9
Petroffs Petroff s Equation
Friction = Shear Stress * Area
( i i * /h)*
C is radial clearance
RLARNV 2 ; 2 ==F = (Viscosity* V/h)*Area
CRLRNF
F
2*2* force,Friction =
RLPCRLRN
iont of frictCoefficien
2/2*2*
WF,
=
=
Bearing
Stribeck
CR
PN
RLP 22
2
=Bearing characteristic number
11/19/2011 10Conclusion: Coefficient of friction is a function of speed, load and viscosity
Lubricant Viscosity
VI relates viscosity change at 37.8 0c and 98.90c.
Pennsylvanian oil~VI=100 gulf coast oil ~ VI=0 100*HL
U-LVI =gulf coast oil VI 0 H-L
1111/19/2011
Dynamic viscosity, 1cP = 1mPa.s
Kinematic viscosity, 1cS = cP/0.85 (g/cm3)
Variation with Temperaturep
More viscous oil is more susceptible to change in viscosity with temp.
Walthers equation: Form the basis of ASTM viscosity temperature chart
Tlt t)60l (l Vogels equation: Most accurate; very useful in engineering calculations
Tc logconstant)6.0log(log =+engineering calculations
ty.in viscosiincrease with increasesbtemp.ofunitshasb iscosity.inherent v givesk )/( += tbke
12
yp
11/19/2011
Temperature Rise Friction, due to shear of lubricant film,
generates heat (FV)) in lubricant oil and i th t t f l b i t increases the temperature of lubricant.
Assuming that total generated heat is i d b th il fl i th h b icarried by the oil flowing through bearing
( )( )22=
LRNRflowoilbyconvectedHeatgeneratedHeat
( )( ) ( )( ) 232
222
=
LNR
tCmNRC
LRNRP
( )/8603= mkg( )
( ) 2322
=
=
LNRtor
LCmC
NRtorP
( )1000
/1760
==
RCkgJCP
o
( ) 222
2
= LCLCRNCtor
P
1000=C
Nt 252=( )( )
228
=CR
CNtor
P Nt 2.52=
11/19/2011 13
Nt 2.52= Assume rotational speed = 900 rpm p p783=t In hydrodynamic lubrication, increase in viscosity increases load capacity but also increases friction. We require Reynolds equation.
SAE grade
Viscosity in mPa s 400c
Viscosity in mPa s 1000c
friction. We require Reynolds equation.
( )atat e
= grade mPa.s 40 c mPa.s 100 c
10W 32.6 5.5720W 62 3 8 81
25.525848 7809
4.36606 898220W 62.3 8.81
SAE 30 100 11.9SAE 40 140 14 7
48.780978.3000
109 6200
6.89829.3177
11 5101SAE 40 140 14.75W-20 38 6.9210W 30 66 4 10 2
109.620029.754051 9912
11.51015.41847 986610W-30 66.4 10.2
10W-40 77.1 14.410W 50 117 20 5
51.991260.369391 6110
7.986611.275216 051510W-50 117 20.591.6110 16.0515
11/19/2011 14
Reynolds Equation A basic pressure distribution equation for Fluid
Film Lub. In 1886, Reynolds derived for estimation of
pressure distribution in the narrow, converging gap between two surfaces gap between two surfaces.
Reynolds equation helps to predict hydrodynamic, squeeze, and hydrostatic film mechanisms.
33equation Reynolds'
( ) ( ) ( )
++
++=
+
02121
33
26 VVhWWz
hUUxz
Phzx
Phx h
11/19/2011 15
U1
y
No pressure development within the parallel surfaces.
U2=0 x
p p p
U1 U1 U1
11/19/2011 16
Pressure driven flow
11/19/2011 17
Small element ofFluid with sides
dzdxdzdydxppdzdxdydzpdy:balanceForce + += ++dx, dy, and dz
dzdxdzdydxx
pdzdxdyy
dzpdy .... :balanceForce + += ++u=flowNewtonianFory=flowNewtonian For
=
yu
yxP 11/19/2011 18
yyx
u P
=
yu
yxP
1yu :nintegratioOn Cy
xP +=
yyx
21
2
2CyCy
xPu ++=
x2;Uu 0,y :conditionsboundary Using ==
21
1
2
)( ,
hPUUUuhy
==
2
121
22 2)( ,
yPyhy
ChxP
hUUCU
=
=
( ) 2212 UhyUU
xPyhyu ++
= Check !!!
11/19/2011 19
:unit widthper direction -in x rate Flow
.0
dyuqh
x = ( )
212 213 hUU
xPhqx ++= Check !!!
direction-zin rate flowSimilarly
dh
( ).
30
hWWPhq
dywqz
++=
= ( )
212 21WW
zqz ++=
equationcontinuitymassusingderivedisequationReynolds
0)(
equationcontinuity massusingderivedisequation Reynolds
0 =++
qVVq zhx11/19/2011 20
zx
equation Reynolds'
( ) ( ) ( )
++
++=
+
02121
33
26 VVhWWz
hUUxz
Phzx
Phx h xxx
Stretching action
iU1 iiU1iiiU1
xx11/19/2011 21
equation Reynolds'
( ) ( ) ( )
++
++=
+
02121
33
26 VVhWWz
hUUxz
Phzx
Phx h xxx
Wedge action (inclined surfaces
2h1h
z11/19/2011 22
equation Reynolds'
( ) ( ) ( )
++
++=
+
02121
33
26 VVhWWz
hUUxz
Phzx
Phx h xxx
Squeeze action q(bearing surfaces move
di l
0h
tt
1h
tt
2h
perpendicular to each other)
0tt = 1tt = 2tt =
Can ca
High lofor shdurat
210
210
ttthhh
>
arryoadshortion210
ttt
equation Reynolds'
( ) ( ) ( )
++
++=
+
02121
33
26 VVhWWz
hUUxz
Phzx
Phx h xxx
( )
+=
h
xUU
zP
zh 21
3 61:Ition Simplifica
xz
( )
+=
h
xUU
xPh
x 213
6:IItion Simplifica xxx 11/19/2011 24
H d St ti B i (HSB)Hydro-Static Bearings (HSB) Completely removal of wear and reduction of Completely removal of wear and reduction of coefficient of friction to 1/500. Surfaces can be separated by full fluid film even at Surfaces can be separated by full fluid film even at zero speed. No problem with micro roughness and waviness. No problem with micro roughness and waviness.
Zero friction at zero speed.Useful feature for large size telescopes and radars.Useful feature for large size telescopes and radars.
High stiffness Oil film thickness varies as cube root of load.
Wh t b i i b d H d t ti h i
3/1Wh Why not every bearing is based on Hydrostatic mechanism
High pressure supply Reliability & life of high pressure oil lines are always in doubt.11/19/2011 25
Elementary 1-D Analysis
Assume a shaft of radius Ro is located oco-axially with a circular recess of radius Ri.
Assume all the oil in recess is at the supply pressure Ps.
11/19/2011 26
R f t
Elemental flow rate: rddrdphq .
12
3
=Ref to slide 20
If flow is axisymmetrical, and radial flow rate
dr12y ,
is constant, then flow rate:
23 dphQ
If film thickness is constant then on
2..12 rdrpQ =
If film thickness is constant, then on integration:
)(log 6 1
3
CrQph +=
11/19/2011 27
6
Using two boundary conditions to find unknown values of C1 and Q
is Rr
RR
rR
pp = 00
0
Rregion in the log
log
Load carrying capacity:iRlog
( )drrdpRpW oi
R
Ris +=
20
2 .
Substituting expression of p and rearranging iR 0
iR12 ( )
=o
o
i
os
RR
RRpWlog.2
1 .
22
=
1
21
11log.2
1
r
rCW
11/19/2011 28
iR 1r
20
22load vs ratio
16
18
20
C1 = 10
10
12
14
l
o
a
d
6
8
10
.1 .2 .3 .4 .5 .6 .7 .8 .94
ratio
( )drrdpRpW oRR
is += 20
2 .iR 0
)/1l (1
6
30 phQ s= 1
2CQ =)/1log(6 1rQ )/1log( 12 rCQ11/19/2011 29
flow vs ratio1
2CQ =
180
200
220
240 )/1log( 12 r
Q
120
140
160
180
w
60
80
100
120
f
l
o
w
0
20
40 C2 = 10
.1 .2 .3 .4 .5 .6 .7 .8 .9
ratio
Generally we require high load capacity but low flow rate Generally we require high load capacity but low flow rate.
11/19/2011 30
Power loss: consists of pumping power and friction losses.
+=PQP
PPP fht =0h
UAF
244
0 1
.
=
=RRP
PQP
i
sh =02
0
)(
R
rAh
rF
00
12
=Rh
Pf
443 == 0 3
0
2
2iR
ff drrhPrFP
24
00
402
0
30 1
2)/log(61
+=
RR
hRP
RRhP is
it
000 )g( i Generally we require high load capacity, low flow rate and low power loss
11/19/2011 31
power loss.
Example: W = 1000 N, =5 rpm, R0=100 mm, Ri=50 mm, =0.01 Pa.s. Optimize minimum film thickness for minimum power loss
244
0230 11
+= RRPhP i
0001
2)/log(6
+=Rh
PRR
P si
t
( )
= oi
os RR
R
RpW1
.2
2
20
2301 h
ChCPt +=( )
i
oos
RR
plog.2
0h
d/523605*2
( ) Pa 824,585.01 )2log(.21.0*1000rad/s5236.060
5*2
22 ====
ss PP
sC
C
/N.m10*404.0
)N/(s.m 10*614.226
2
2111
==
11/19/2011 32
( ) sC /N.m10404.02micronh losspowero 8.26min =
Short Static Short Static Hydrodynamic Bearing
( )
+=
h
xUU
zP
zh 21
3 61 xzz dhUP
32
2 6 =dxhz 32
6 dhUdp 0zat 0dp/dzcondition pressuremax using 6 3 === zdxdh
hU
dzdp
L/2 zat 0p using 4
3 223 ==
= Lz
dxdh
hUp
11/19/2011 33
4 dxh
Film thickness, h, depends on geometry of tribo-pair. ForFilm thickness, h, depends on geometry of tribo pair. For example, in journal bearing h = Cr + e cos
eLdhU 3equation followingin h of expression Using
2 rC
edRdxLzdxdh
hUp ==
= ;;
43 2
3
( ) 4sin
cos13 22
32
+=Lz
RCUp
r
11/19/2011 34
Load capacity of short journal bearing bearing
centres of line of direction in component Load
( )222
2
3
0 1
22
cos)...(2
2
= = rC
LUWdzRdpWL
L
2 3
centres of line lar toperpendicu component Load
LUL W( ) 23
2
2220 14
sin)...(
= =
rrr C
LUWdzRdpWL
2/1
( )2/1
22222
322 1116
14
+
=+=
rr C
LUWWW ( )14 rC
21tantan == Wr 4tantan == W11/19/2011 35
Locking of Journal Locking of Journal Position
valueMaxW ===
01
valueMaxW =
02
0
===
W
20
10
Lesser the attitude angle, better the stability of bearing.
80
90eccentricity ratio vs. attitude angle
60
70
e
40
50
t
u
d
e
a
n
g
l
e
10
20
30
A
t
t
i
0 .1 .2 .3 .4 .5 .6 .7 .8 .9 10
10
11/19/2011 37
Eccentricity ratio
Friction force in Journal BearingFriction force in Journal Bearing
Petroff equation (explained on slide 10)--- inaccurate
dAFhdxdp
hU ;
2
=+= h = Cr + e cos
dzRdhUF
L
L.0
2/
2/ 0
+=
2/1
21
2
=
C
ULRF ( )2/1
22222
31116
14
+
=
rC
LUW1 rC
If 0, F Petroff solution( )14 rC
11/19/2011 38
Raimondi & Boyd Method
hPhPh loadingstaticfor equation Reynolds'
33
xhU
zPh
zxPh
x =
+
6
R 2 N
dft tiCR Snumber Sommerfeld s
NpN
=
secondfor rotation sN
Dimensionless numberDimensionless number
11/19/2011 39
L/D S (R/C)f Q/(RCLNs ) Qs / Q p/pmax1 .631 .2 74 12.8 3.596 .28 .529
.264 .4 63 5.79 3.99 .497 .484
.121 .6 50.6 3.22 4.33 .68 .415
.045 .8 36.2 1.7 4.62 .842 .313
.019 .9 26.5 1.05 4.74 .919 .247
0.5 2.03 .2 75 40.9 3.72 .318 .506
.779 .4 61.5 17 4.29 .552 .441
.319 .6 48 8.1 4.85 .73 .365
.092 .8 33.3 3.26 5.41 .874 .267
.031 .9 23.7 1.6 5.69 .939 .206
0.25 7.57 .2 75.2 153 3.76 .33 .489
2.83 .4 60.9 61.1 4.37 .567 .415
1.07 .6 46.8 26.7 4.99 .746 .334
11/19/2011 40
.261 .8 31 8.8 5.6 .884 .24
.074 .9 21.9 3.5 5.91 .945 .18
Question: Estimate friction coefficient Question: Estimate friction coefficient and minimum film thickness of a full cylindrical hydrodynamic bearings cylindrical hydrodynamic bearings required for shaft of 50 mm diarotating at 1500 rpm Assume applied rotating at 1500 rpm. Assume applied load is 5 kN, bearing length is 50 mm radial clearance is 25 microns mm, radial clearance is 25 microns, and lubricant viscosity is 25 mPa.s (at
bi t t t ) ambient temperature). mkg /860 3= ( )t( )CkgJC mkgP o/1760
/860
= ( )at
at e=
11/19/2011 41
Clutches & Brakes Difference between coupling, clutch &
brake. Maximize friction (uniform) Smooth, gradual connection/disconnection, g Minimize Wear (if mechanical)
Design targets: Design targets: Required friction torque. Actuating Mechanism Actuating Mechanism
Heat dissipation. Desired life
11/19/2011 42
Desired life.
Various Types of ypClutches & Brakes
PP
PP
P
Mating frictional surfaces transmitting torqueP
P
transmitting torque Actuating mechanisms Centrifugal P
P
Centrifugal Magnetic Hydraulic
11/19/2011 43
Hydraulic Pneumatic
ClutchesCone clutch is installation. However, disk clutch a number f d t l t hof advantages over cone clutch.
Large frictional area in relatively small area.
More effective heat More effective heat dissipation.
Simple construction.
11/19/2011 44
Simple construction.
Aim: Obtain expression of axial force F necessary to produce a certain torque with pressure distribution.
Uniform pressureUniform pressure
or
d2=ir
drrpF 2
( )222 ior rrpdrrpF o == ri
( )2ro ( )33322 ior rrpfdrrprfT i == 11/19/2011
Friction based brakesFriction mat. f Pmax
(MPa)Tmax(C)( ) ( C)
Dry OilMolded 0.25-0.45 0.06-0.09 1-2 230Molded
Woven 0.25-0.45 0.08-0.1 0.35-0.69 230
Sintered 0.15-0.45 0.05-0.08 1-2 300
Cast iron/Hard_steel
0.15-0.25 0.03-0.06 0.69-0.72 260
Wet or dry brakes
11/19/2011 46
Laws of Wear Wear Volume proportional
to sliding distance (L) True for wide range of
conditions Wear Volume proportional
to the load (N) D ti i Dramatic increase
beyond critical load Wear Volume inversely Wear Volume inversely
proportional to hardness of softer material
HNLkV
31= Transition from mild wear to severe
depends on relative speeddepends on relative speed, atmosphere, and temperature.
11/19/2011
Two methods to estimate pressure distribution are:
Uniform wear
Uniform pressurep
( )UtpAkNLkVvolumeWear 11or
( )
UpUkVHH
VvolumeWear ==33
,
1 =ir
drrpF 2 rprp
pUwHp
Atwratewear
===
meanratearConstat we3
, 1
ooii rprp =meanratear Constat we
= or
drrpF 2 r=ir
oo drrpF 2 = oi
r
roo drrrpfT 2
i
11/19/2011
Comparison( ) iioiwearuniform rrrrpfT at pressuremax assuming22max = ( )332fT ( )33max 32 iopressureuniform rrpfT = ( )2 33 rrT ( )( )32 22 == rrr rrTTRatio ioi iowearuniformpressureuniform( )( )1132 2
3 =RRRatio
1 451.5
1.551.6
Torque ratio vs dimension ratio
( )13 R1 2
1.251.3
1.351.4
1.45
T
o
r
q
u
e
r
a
t
i
o
11/19/2011 491.2 1.3 1.4 1.5 1.6 1.7 1.8 1.9 2
1.11.15
1.2
R
Friction mat
f Pmax(MPa)
Value of ri to maximize Tmat. (MPa)
Dry Oil
M ld d 0 25 0 06 1 2( )22max ioiwearuniform rrrpfT = Molded 0.25-0.45 0.06-0.09 1-2Woven 0.25- 0.08- 0.35-
0=rdTd
Woven0.45 0.1 0.69
Sintered 0.15-0 45
0.05-0 08
1-2ird
or
0.45 0.08
Cast iron/Hard steel
0.15-0.25
0.03-0.06
0.69-0.72( )NrrrpfT ioi 22max =
3o
ir =Most of automotive clutches operate
Hard_steel
ost o auto ot e c utc es ope atewet. The oil serves as an effective coolant during clutch engagement. To compensate reduced coefficient
11/19/2011 50
To compensate reduced coefficient of friction, multiple disks are used.
= or
drrpF 2Disk Brake
ir
oo drrpF 2
F F= or
drdrpF 2
F F=ir
ii drdrpF 1
ddrrrpfTor
ii = 2
ddrrrpfTir
ii 1
= or
oo drrrpfT 211/19/2011 51
ir
oopf
Ex: Two annular pads, ri=98mm, ro=140 mm, subtend an angle of 100, have a coefficient of friction of 0.35, and are
t t d b i f h d li li d 36 i actuated by a pair of hydraulic cylinders 36 mm in diameter. Torque requirement is 1500 N.m. Determine max contact pressure, actuating force and hydraulic pressure. contact pressure, actuating force and hydraulic pressure.
CASE I: Uniform wear
ddrrrpfTor
ii = 2 NdrdrpF or
ii 180072
==
pf
irii
1
09801401500 22
pir
ii
1
pi 2098.014.0
180*100*098.0*35.0
21500
=
Papi 2506649=PF 17690959
11/19/2011 52( ) Paphydraulic 17690959018.0 2 ==