IMECE2003-41457: Multi Criteria Design Optimization of Backhoe Loader Front Mechanism
IMECE2003-41457: Multi Criteria Design Optimization of Backhoe Loader Front Mechanism
IMECE2003-41457
Lever
Pull rod Breaking force
L1 ξ 8( 2 )
3
L2
7
Figure 2. Position of attachment and shovel cylinder in the two ϕ2
different situations where parallel motion is desired.
Figure 4. Variables associated with the kinematic analysis.
In the first case the procedure of analysis is as follows: y-coordinate in a local coordinate system pointing from point 5
Firstly the global coordinates, r of points 3 .. 6 are found as: to point 10 is chosen. The position of point 8 is computed
along exactly the same lines, only here the circles in question
have points 3 and 9 as center and the radii L3 and s(83 ) .
r i = A ⋅ s(i 1 ) i = 3..6 (1)
1
The position analysis is concluded with some straight
forward computation of the orientation of the lever, the
In equation (1) the standard formulation using the position of point 7 and the orientation and length of the
transformation matrix, A of the main boom together with the hydraulic actuators.
1
coordinates of the points of interest in the local coordinate
system of the main boom, s(i 1 ) are used. Next, the positions of ( )
ϕ3 = ∠ r8 − r3 − β + π r 7 = r 3 + A ⋅ s7( 3 )
3
(6)
points 10 and 9 are computed utilizing that a sub fourbar (
θ MC = ∠ r 4 − r 1 ) LMC = r 4 − r 1 (7)
linkage may be identified consisting of the attachment as the
driven link, the main boom as the frame and the small pull rod θ SC = ∠(r 7 − r 2 ) LSC = r 7 − r 2 (8)
and the vertical arm as the connecting rods. The position
analysis is basically a computation of the intersection points of
Hence, the entire kinematic analysis may be carried out
two circles, see figure 5, with center at point 10 and point 5
based on explicit expressions greatly reducing the
and radii L4 and L5 , respectively. The analysis also includes
computational time.
a unique routine that chooses the intersection point that The second type of kinematic analysis also employs
corresponds to the actual assembly configuration. equation (1). Next, point 7 is computed as the intersection
point between two circles centered at point 2 and point 3 and
cosθ − sin θ ∆ x with radii LSC and L2 , respectively. Next, point 8 may be
r9 = r5 + ⋅ (2)
sinθ cosθ ∆ y determined:
ng
O (Y ) = w1 ⋅ f 1 + w2 ⋅ f 2 + ∑Φ (12)
i =1 i
y'
5
min 60
Figure 7. Extreme position 2. In all of the four extreme positions kinematic analysis of type 1
has been used. Next, the current design is evaluated in two
Extreme position 3, see figure 8: The main boom is in its motion intervals where kinematic analysis of type 2 is
lower position, ϕ 1 = ϕ 1,min and the shovel is plane, α = 0° . In employed.
Motion interval 1: The front loader mechanism is initially
this position point 5 must lie at least 30 mm above point 6 in a position corresponding to extreme position 3. With the
(IC8) to provide a margin against point 5 colliding with the shovel cylinder locked the main boom is moved to its upper
ground. Also, the breaking force is evaluated in this position. position. The first objective function is evaluated as:
The breaking force is penalized if it is either 2 kN below or
above the desired value, (IC9).
(α i − α 1 )2
m
Extreme position 4, see figure 9: The main boom is in its f1 = ∑ (15)
i =1
lower position, ϕ 1 = ϕ 1,min and the shovel is tilted upwards,
α = 45° . In this position the maximum length of the shovel In equation (15) m = 20 is the number of evaluated positions
cylinder is computed, LSC ,max . The necessary dead length of that should be viewed as a compromise between computational
the shovel cylinder in order to utilize the entire stroke is: cost and precision.
Motion interval 2: The front loader mechanism is initially
d' = 2 ⋅ LSC ,min − LSC ,max (14) in a position corresponding to extreme position 4. With the
shovel cylinder locked the main boom is moved to its upper
position.
8 RESULTS
y' Applying the optimization formulation described
x' '
9 previously yields the design listed in table 1. As initial design
y' ' 3 in the optimization the best design developed "manually" by
0 10
7 Hydrema ApS was used. The non-zero contributions to the
2
minimized penalty function are listed in table 2.
4
5
6
1 Table 1. Design variables of optimized design. All dimensions
Figure 10. Different distances used to evaluate inequality in mm.
constraints associated with the motion intervals. x2 = 38.57 y2 = −170.71 ξ 3( 1 ) = 1000.53
The value x' should remain positive to give margin against η3( 1 ) = 184.75 ξ 5( 1 ) = 2432.65 η5( 1 ) = −50.76
collision between lever and steering house. The value y' L2 = 259.18 ξ 8( 3 ) = −565.24 η8( 3 ) = −125.18
should stay above 330 mm to allow room for a sufficient
bending stiffness of the main boom (IC13). L3 = 1489.17 L4 = 507.7 L5 = 371.28
Point 5 should lie at least 100 mm to the left of the line
connecting points 6 and 9 (IC14) and at least 110 mm below Table 2. Non-zero contributions to the penalty function.
the small pull rod (IC15). Points 7 and 3 should both lie at IC 5 = 9.21 IC6 = 10.62 IC 9 = 0.56
least 110 mm to the left of the vertical arm (IC16 and IC17). IC11 = 0.03 f1 = 411.70 f 2 = 237.46
The values x' ' and y' ' should remain less than 1250 mm and
more than -50 mm, respectively (IC18 and IC19). Inequality In figure 11 the shovel rotation are shown for the optimized
constraints (IC14..19) ensures margins against collision design corresponding to the two motion intervals.
between different members of the front loader mechanism.
Obviously, the vast number of side constraints and 50 α [deg]
corresponding threshold values have been decided in close
coorporation with Hydrema ApS. The weighing was carried 40
out as follows: All constraint violations related to dimensions Motion interval 2
was computed in mm 2
directly without any weighing. 30
Violation of the breaking force constraint was computed in
20
N 2 and weighed with a factor of 1 ⋅ 10 −5 . Violation of the
angle in IC5 was computed in deg 2 and weighed with a factor 10 Motion interval 1
of 3.0. The objective functions was directly computed in ϕ 1 [deg]
0
deg 2 without any weighing. The final optimization
-40 -30 -20 -10 0 10 20 30 40 50
formulation is the result of an iterative proces were weighing
-10
factors and side constraints continuously have been varied or
added/removed until the design returned by the procedure was Figure 11. Variation of shovel rotation as function of the
deemed acceptable. rotation of the main lift.
[4] Soni, A. H., Dado, M. H. F., and Weng, Y., "An Automated
Procedure for Intelligent Mechanism Selection and
Dimensional Synthesis", Journal of Mechanisms,
Transmissions and Automation in Design, Vol. 110, pp. 131-
137, 1988.