Theoretical Evaluation of The e Ects of Crank Oset On The Reduction of Engine Friction
Theoretical Evaluation of The e Ects of Crank Oset On The Reduction of Engine Friction
          Abstract: This study discusses the eects of crankshaft osets to the piston thrust side on engine
          friction. An analytical model to interpret some key friction parts of an engine, such as crankshaft
          bearings, pistons and piston rings, is considered, and the eects of a crankshaft oset on the moving
          parts is calculated using numerical analysis. Analytical results show that the crankshaft oset has
          some inuence mainly on the side force upon the piston and eects variation in the piston sliding
          speed. The crankshaft oset can reduce signicantly friction loss of the piston skirt, whereas friction
          loss in other parts is negligible. The optimum oset to minimize skirt friction loss depends on the
          operating conditions. Upon calculation and measurement it is determined that reduction in friction
          loss occurs mainly at low engine speed and low engine load. When the speed and load increase,
          benet is conned to the lowest osets, and at higher osets the friction increases. Analytical and
          experimental results indicate that crank oset is eective in reducing engine friction and improving
          fuel economy in the low and medium engine speed region.
Keywords: crankshaft, oset, friction, side force, piston skirt, fuel economy
m                    equivalent mass of the crank journal                                       high-eciency and low fuel consumption engine. Many
     j
                     and pin                                                                    researchers are interested not only in improving engine
m                    wrist pin mass                                                             performance but also in reducing emissions as a result of
    pin
m                    piston skirt mass                                                          better fuel consumption eciency using gasoline direct
    pis
M                    total moment about the wrist pin                                           injection (GDI ), variable valve timing ( VVT ), variable
M                    asperity contact moment                                                    valve lift ( VVL) and other technologies. Reducing friction
     c
M                    total friction moment                                                      loss, which causes about 5 per cent of total power loss in
     f
M                    friction moment due to asperity contact                                    the engine, is another area receiving much attention with
     fc
M                    friction moment due to hydrodynamics                                       a view to improving fuel consumption [1–3]. Reducing
     fh
M                    hydrodynamic moment                                                        friction loss would improve considerably mechanical
     h
M                    inertia moment of the piston skirt                                         eciency. It is reported that a 10 per cent reduction in
     pis
M                    rotating mass of the crankshaft                                            engine friction would improve fuel economy by 1–1.5 per
     r
p                    hydrodynamic pressure                                                      cent at full load [4].
p                    back pressure in the ring groove                                              All friction losses in the engine are generated in the
  b
p                    ring tension                                                               valvetrain, the piston assembly, the crankshaft and other
  TE
P                    asperity contact pressure                                                  moving parts. Among these, the friction loss in the piston
   c
r                    crank radius                                                               assembly is up to 40–65 per cent [5], of which the loss in
  c
R                    nominal radius of the piston skirt                                         the piston skirt is about 40–50 per cent. Recently, a crank
t                    time                                                                       oset technology was proposed to reduce friction loss in
U                    sliding speed                                                              the piston assembly [6 ]. Only a few studies, however, have
W                    external force in the bearing                                              focused on the crank oset, and the friction reduction has
                     = F2 +F 2                                                                  not been thoroughly studied and established thus far.
                            bx    by
Ÿ                   piston skirt acceleration                                                  Shinichi et al. [7] reported that, when a crank oset is
                                                                                                applied, fuel economy is improved by 3 per cent at low
a                    piston skirt bearing angle                                                 engine speed and low engine load, and there is an optimum
b                    connecting rod angle                                                       point to maximize the oset eect. Nakayama et al. [6 ]
b                    asperity radius of curvature
    r                                                                                           conrm the oset eect by a oating liner and explain that
e                    eccentricity in the bearing                                                this eect is due to the piston side force and sliding speed.
e                    eccentricity of the piston bottom
   b                                                                                            They conclude, however, that it is very hard to apply this
e                    eccentricity of the piston top
   t                                                                                            technique to mass production of engines.
eb                   radial velocity of the piston bottom
   b                                                                                               This study sets up a useful model to analyse lubrication
eb                   radial velocity of the piston top
   t                                                                                            and the friction characteristics of the engine bearing, the
g                    oil viscosity                                                              piston ring and the piston to examine the eect of crank
h                    crank angle                                                                oset on reduction in friction. The results of this study will
m                    asperity density                                                           be helpful in developing a crank oset engine.
m                    boundary friction coecient
    f
s                    composite r.m.s. roughness = s2 +s2
                                                       1  2
t                    hydrodynamic component of the shear
                     stress                                                                     2     THEORETICAL MODEL
w                    attitude angle of the bearing
w ,w ,w              shear stress factor                                                        2.1 Equations of motion
  f fp fs
w                    shear ow factor
  s                                                                                             Figure 1 shows a schematic diagram of the crank oset
w ,w                 pressure ow factor
  x y                                                                                           engine. In such an engine the crankshaft centre is dis-
Q, h̃                bearing angular coordinate
v                    rotational speed                                                           placed to the piston thrust side from the cylinder bore.
                                                                                                The amount of oset chosen is within a range ensuring
                                                                                                that the rotation of the crankshaft is not disturbed by
                                                                                                the cylinder block. With application of the oset, it is
1        INTRODUCTION
                                                                                                necessary to adjust the connecting rod length and the
                                                                                                crank radius to t the combustion chamber volume and
In recent years, as the regulations concerned with emis-                                        compression ratio.
sions, such as CO regulation in Europe and US Federal                                             The piston sliding speed and the acceleration with an
                  2
regulations in North America, have become more severe                                           oset are dened as follows
and market demand for low fuel consumption vehicles has
increased, the ecient consumption of fuel has become                                               Yb =r sin h +r vM cos h (l2M2)Õ 1/2         (1)
                                                                                                         c         c
one of the most important factors for the automotive
                                                                                                    Ÿ =r v2 cos h +(r vM cos h )2(l2M2)Õ3/2
industry. Among eorts to improve the fuel economy in                                                    c            c
vehicles, much research has been carried out to develop a                                               +{(r v cos h )2r v2M sin h }(l2M2)Õ0.5 (2)
                                                                                                              c          c
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Proc. Instn Mech. Engrs Vol. 217 Part D: J. Automobile Engineering                                                                         D01503 © IMechE 2003
                              THEORETICAL EVALUATION OF THE EFFECTS OF CRANK OFFSET                                                                                 893
where
   M =r sin h +C C                                   (3)
         c          p    o
The change in piston acceleration with the oset aects
the piston inertial force and the load on the piston pin
and the crankpin. These changes in load and speed aect
the dynamics and lubrication characteristics of the
engine moving parts. Figure 2 shows analytical models
for obtaining the equation of motion for each moving
part of the engine.
   In addition to the primary axial motion of the piston,
there is also a secondary lateral and rotational motion
within the bore. The lateral motion proceeds transversely
in the bore and the rotational motion is around the wrist
pin axis.
   The governing equation for the dynamic motion of
the piston from Fig. 2a can be obtained as follows [8–10]
                                                                                                Fig. 2       Dynamic modelling of engine moving parts
  C        A B             A B
                                                                          D
               a           b                      a        b
      m     1   +m     1                  m       +m
        pin    L    pis    L                  pin L    pis L
                                                                                        lm and asperity contact pressure by the surface
                          A B
         I                 b                    b I                                     roughness.
           pis +m (ab) 1              m (a b)  pis
          L      pis       L             pis    L  L                                       As shown in Fig. 2b, the journal movement in the
                                                                                        engine bearing can be expressed as non-linear equilib-
         GH
          ë                                                                            rium equations for the radial and circumferential
    ×          t
          ë                                                                            directions as follows [11].
               b
                                                                                          m C [ë ewb 2]=F +W cos w
          C                                                D
           F (F +F +F +F ) tan w                                                           j R             r
                                                                                                                                               (5)
          =      f   gas    pisy   piny           (4)
              M +M +F C F C                                                              m C [eẅ +2ewb ]=Ff W sin w                         (6)
                      f   gas p     pisy g                                                  j R
In equation (4), reaction forces, F, F , M and M can                                    In equations ( 5) and (6), the reaction forces of the oil
                                       f        f
be calculated using hydrodynamic pressure by the oil                                    lm, F and Ff , can be derived by integrating the oil lm
                                                                                              r
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D01503 © IMechE 2003                                                                                  Proc. Instn Mech. Engrs Vol. 217 Part D: J. Automobile Engineering
894                           MYUNG-RAE CHO, DAE-YOON OH, TAE-SEON MOON AND DONG-CHUL HAN
pressure. Here, W is the load working upon the con-                                             The reaction forces in equations (4) to (7) can be
necting rod and the main bearing. The load on the                                               calculated from the oil lm pressure and the contact
connecting rod can be obtained from the combustion                                              pressure as follows:
pressure and the inertial force of the reciprocating mass
                                                                                                piston skirt
of the connecting rod. To calculate the load on the main
bearing, however, some statically indeterminate method                                              F =F +F ,                     M =M +M                                  (11)
                                                                                                        h  c                          h   c
is needed in which the crankshaft is supported by several
bearings, but such calculation is very dicult. To sim-
plify the model, a statically determinate method is used
                                                                                                    F =R
                                                                                                     h             PP   p cos(h̃ a ) dh̃ dy                               (12)
                                                                                                                   PP
   In the piston ring pack, the pressure of the oil lm
                                                                                                    M =R                 p(ay) cos (h̃ a ) dh̃ dy                        (13)
and the asperity contact pressure are in balance with the                                            h
ring tension and the ring back pressure. Thus, the load                                                             A
                                                                                                                   PP
equilibrium equation of the piston ring becomes [13, 14]
                                                                                                    F =R                P cos(h̃ a ) dh̃ dy                               (14)
        A         B
            dh                                                                                       c                   c
   F    h ,    =F +F 2ðRb ( p +p )=0                                           (7)
     pr m dt     oil c    p TE   b                                                                                 A
With such an equilibrium equation for each moving
part, the reaction force by the oil lm and the surface
                                                                                                    M =R
                                                                                                     c             PP    P (ay) cos(h̃ a ) dh̃ dy
                                                                                                                          c
                                                                                                                                                                           (15)
                                                                                                               A
The governing equation for lubrication analysis used in
this study is an average Reynolds equation as follows
[15, 16 ]
                                                                                                    Ff =
                                                                                                              PP    p sin Q dQ dz                                          (17)
       A            B A B
   d w h3 dp   d w h3 dp
      x      +    y                                                                             piston ring
   dx g dx     dy g dy
                                                                                                                        P
                                                                                                                            bp
                 dh¯            dh¯                                                                 F =2ðR                       p dx                                      (18)
                    A   B
                          dw
                     t +6s s +12 t                                                                   oil
           =6|U|                                                                (8)                                       0
                 dy       dy    dt
                                                                                                                       P
                                                                                                                         bp
In order to apply this equation to each engine part, it is                                          F =2ðR        P dx                               (19)
                                                                                                     c             c
assumed that the engine bearing works in the fully                                                            0
hydrodynamic lubrication area and the piston ring and                                           Lastly, the total friction force in each moving system is
skirt work in the mixed lubrication area. Therefore, the                                        dened as the sum of viscous friction and boundary fric-
ow factor for surface roughness in equation (8) is                                             tion, the shearing force and the friction force and the
ignored in engine bearing analysis. Because the ring                                            friction moment. Only viscous friction is considered for
width of the piston ring pack compared with the ring                                            the engine bearing
                                                                                                                                h¯ qP
length of the circumference is very short, only the press-
                                                                                                          mU
ure gradient along the ring circumference is considered                                            t = ¯ [w +w ]+w                  h               (20)
as one-dimensional analysis. Oil starvation of the ring                                             h      h    f     fs     fp 2 qy
                                                                                                             PP                           PP
pack is not considered in this study.
   In equation (8), to calculate oil lm pressure, use is                                           F=              t dA+m                  P dA                           (21)
                                                                                                     f               h     f                 c   c
made of the conventional Reynolds boundary condition.
                                                                                                              PP                            PP
Oil lm pressure is calculated using a nite dierence
method and then iterative calculation.                                                              M=                 t ã dA +m                P ã dA                   (22)
                                                                                                     f                  h         f               c      c
   However, to calculate the contact pressure with sur-
face roughness, use is made of Greenwood and Tripp’s                                            Table 1 shows specications and input variables of the
[17] asperity contact theory as follows                                                         test engine used for numerical analysis.
           8 ã2
                                     S
                                         s
   P (H )=      ð ( mb s)2E                F (H )                               (9)
    c       15        r                  b 2.5                                                  2.3 Numerical analysis
                      P
            1  2                                                                                Oil lm thickness and the friction of each moving part
   F (H )=       (s H )n eÕse/2 ds                                           (10)
    n      ã2ð                                                                                  are calculated as follows:
               H
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Proc. Instn Mech. Engrs Vol. 217 Part D: J. Automobile Engineering                                                                                           D01503 © IMechE 2003
                             THEORETICAL EVALUATION OF THE EFFECTS OF CRANK OFFSET                                                                                895
Fig. 4    Eect of crank oset on the mean side force at full                                   Fig. 5      Eect of crank oset on the mean friction torque in
          engine load                                                                                       engine bearings at full engine load
REFERENCES