Monday, 18 June 2012

Different Losses in Bend


 Bend Loss:  A form of increased Attenuation in a Fiber that results from bending a fiber around a restrictive curvature (a macro bend) or from minute distortions in the fiber (micro bends). 2. A form of increased attenuation caused by allowing high order Modes to radiate from the walls of a fiber optic cable. There are 2 common types of bend losses. The first type results when the fiber optic Cable is curved through a restrictive radius or curvature. The second type is generally referred to as micro bends. It is caused by small distortions of the Fiber Optic Cable imposed by externally induced perturbations as, for Example, slip shod cabling techniques.
Types of Bends:
Conduit installations are normally referred to as runs of conduit. A run of conduit is the conduit, fittings, straps, conductors, and bends needed from one opening to the next (for example, from the panel board to the first outlet box or from the first outlet box to the second outlet box). In a run of conduit, there cannot be more than the equivalent of four 90° bends, for a total of 360°. The purpose of allowing only so many bends in a run of conduit is to help in pulling conductors into the conduit. Experience has taught that if more than 360° of bends are used, it is very difficult to pull conductors through the bends Figure 1

Figure: 1 360° bendConduit bodies are available in the following configurations: elbow back (LB), elbow right (LR), and elbow left (LL) and a T. The configuration of each is determined based on the location of the removable cover Figure 2



                                               
Figure: 2 Conduit bodies
By using a conduit body in a run, you provide an opening for pulling the conductors without having to mount a box. At the same time, you can make a turnaround or go over an obstacle and maintain a neat conduit installation. The turn or 90° turn made by the conduit body does not count as one of the four allowable bends in a run. As a matter of fact the conduit body is identified as an outlet box. One of the most common bends you will make in the field is the right-angle bend, more commonly called a 90° bend or just a 90. It can be used for going around an inside corner, into the top or bottom of a box from a horizontal run, or over an object. Anyone can make a 90° bend in a stick of conduit and then cut it off to make it fit the situation, but this practice wastes time and material. The secret is to find out where the bend is needed, mark the conduit accordingly, and make the bend in the right place. This practice saves time and material. Before you can determine where to place your bender on the conduit, there are some things you must know. First, there are two lengths on the conduit that must be considered, from one end of the conduit to the 90° bend and then from the 90° bend to the other end of the conduit. The shorter of these two lengths is called the stub end and the longer is the running end. Second, the radius of the bend takes up a part of the stub. This part of the stub is called take-up and is shown in Figure 3 the amount of take-up depends on the type and size of the conduit you are bending Table -1



 
Figure: 3 Conduit bending terms






Table-1 Conduit take-up
Amount of Take-Up for 90° Bends Using an EMT Bender
Size and Type of Conduit
Take-Up
1/2-inch EMT
5 inches
3/4-inch EMT or 1/2-inch rigid steel*
6 inches
1-inch EMT or 3/4-inch rigid steel*
8 inches
1 1/4-inch EMT or 1-inch rigid steel*
11 inches
In the following example, you are going to make a 90° bend using 1/2-inch EMT conduit and the EMT bender. You are going to run the conduit from the top of a panel to the ceiling and then horizontally along the ceiling. Measure from the top of the panel to the ceiling. This will give you the stub length of 18 inches. Measure 18 inches from the end of the conduit and make a mark (Figure 4).
Look at Table 1 to find out what the take-up is for 1/2-inch EMT conduit. The take-up is 5 inches. Measure back 5inches from the first mark toward the end of the conduit and make a second mark as shown in Figure - 4





Figure -4 placing the bender to make a 90° bend
Hold the bender in one hand with the lip on the floor pointed toward the stub end. Use the other hand to place the conduit in the bender. Align the bender arrow with the take-up mark. Put one foot on the footrest and hold the handle with both hands. To make the bend, apply pressure on the footrest as you pull on the handle until the handle is parallel with the floor. It is OK to go slightly beyond 90° with the bend, in fact it is preferred, because it is easy to bring it back to 90°.
You should now have a 90° bend with an 18-inch stub Figure 4. To see whether the bend will fit properly, place it next to something that has a right angle (for example, in the corner where the floor and wall meet).








Figure 3-6. 90° bend with an 18-inch stub
If the bend is more than 90°, you can stand on the running end and push out on the stub end, a little at a time, until it is 90°. If the stub is too short or if the conduit is too long to push back, place the handle of the bender over the end of the stub and, with one foot on the conduit on the floor, spring the stub back (right-angle bends should always be made with the conduit and the bender on the floor).
In this example, you are going to make a 90° bend in the conduit and run it along the wall. The first thing you must do is establish a reference point using the following steps:
Step 1: Measure the distance from the outside edge of the knockout to the wall at box a (Figure -5).
Step 2: Transfer that measurement above box A and across from box B. Mark a reference line (Figure -5).
Step 3: Measure the distance from the outside edge of the knockout to the ceiling at box B (Figure -5)
Step 4: Transfer that measurement across from box B and above box A. Mark a reference line. Where the two lines cross is the reference point (Figure -5).
 Step-5: Measure from box A to the reference point and add this measurement to the measurement between box B and the reference point. Deduct the gain (Table -1). This will give you the length for the piece of conduit you need to run between boxes A and B (Figure -5).

 

 

                                      Figure -5 90° bend

 

Loss of Head in Bends:

The loss of head, due to bends in a pipe, depends upon three factors. First, loss due to change of direction of the water in the pipe; second, loss from friction as in an ordinary straight length of pipe; third, loss due to enlargements or contractions in the bend, such as are formed when the undreamed ends of pipe are screwed into ordinary elbows.

The second and third losses also apply to couplings and tees, and the loss is about the same as for bends of equal diameters. The loss of head for change of direction differs with the angle and with the radius of the bend. That is, there is less loss for change of direction in a 45 degree bend than in a 90 degree bend, and the loss is greater in a bend of one diameter radius than in one with a radius of two diameters. The loss in a 90 degree bend with a radius of five or more diameters and uniform smooth interior bore is no greater than in an equal length of straight pipe. In other words, there is practically no loss for change of direction in a bend of greater radius than 5 diameters.
The head lost in a 90 degree bend of less than 5 inch diameter and of the radius commonly found in practice (Radius=Diameter) with square undreamed ends of pipe screwed into the fitting, Fig-1 is found by experiment to equal the head lost in a length of pipe of about 100 times the diameter of the fitting.* The loss of head is divided into:




                                               
Fig-7
*Thus 100 diameters of 2-inch pipe=200 inches of straight 2-inch pipe.
Loss of head due to change of direction . . . . . .
38 diameters
Loss of head for entry with ordinary undreamed ends. .
58 diameters
Loss of head from friction due to length. . . . . .
4 diameters
Total
100 diameters
In pipes of larger diameter than 5 inches, these values would hold true only for the loss of head due to change of direction, as the pipes are not relatively as thick, nor the enlargements of the elbows relatively as greatThe loss of head when the ends of the pipe screwed into the fitting are reamed, as shown in Fig-2 is found by experiment to be equal to the loss of head in a pipe equal in length to about 50 diameters of the fitting. This loss of head is divided into:





                                                Fig-8   
Loss of head due to change in direction 38 diameters
Loss of head due to enlargement of the bend 8 diameters
Loss of head from friction due to length of fitting 4 diameters
Total=50 diameters
The loss of head in a bend of five or more diameter radius, with flush interior joints, Fig-3 is equal to the loss of head in a length of pipe four diameters of the fitting. This is comparatively shown as follows:
Loss of head due to change of direction
0 diameters
Loss of head due to enlargements of the bend
0 diameters
Loss of head from friction due to length of pipe
4 diameters
Total
4
From the foregoing it will be seen that the least possible head is consumed by using fittings of large radius with flush joints. That when common fittings are used the loss can be reduced to one-half by reaming the ends of the pipe with a triangular-shaped reamer, the length of which is just double the base.
Table -2 Values of Coefficient n

r R =
R=r
R=1.12r
R=1.25r
R=1.4r
R=1.6r
R=2r
R=2.5 r
R=3.3r
R=5r
n
1.98
141
.98
.66
.44
.29
.21
.16
.14






Fig-9
The loss of head due to bends can be calculated by the formula:
V2 h=n 2g
In which h=head lost in feet v = velocity in feet per second g = 32.16 acceleration due to gravity n = a coefficient for the bend.
The value of coefficient n depends upon the ratio between the radius r of the pipe and the radius R of the bend. Table -2 gives values of n corresponding to various values of the ratio r.
Losses in Pipe Bends:

·         Bends are provided in pipes to change the direction of flow through it. An additional loss of head, apart from that due to fluid friction, takes place in the course of flow through pipe bend.

·         The fluid takes a curved path while flowing through a pipe bend as shown in Fig 1             

 

 

 

Fig: 10 Flow through pipe bend

Whenever a fluid flows in a curved path, there must be a force acting radically inwards on the fluid to provide the inward acceleration, known as centripetal acceleration.

This results in an increase in pressure near the outer wall of the bend, starting at some point A (Fig-1) and rising to a maximum at some point B There is also a reduction of pressure near the inner wall giving a minimum pressure at C and a subsequent rise from C to D .Therefore between A and B and between C and D the fluid experiences an adverse pressure gradient (the pressure increases in the direction of flow).

Fluid particles in this region, because of their close proximity to the wall, have low velocities and cannot overcome the adverse pressure gradient and this leads to a separation of flow from the boundary and consequent losses of energy in generating local eddies. Losses also take place due to a secondary flow in the radial plane of the pipe because of a change in pressure in the radial depth of the pipe.

This flow, in conjunction with the main flow, produces a typical spiral motion of the fluid which persists even for a downstream distance of fifty times the pipe diameter from the central plane of the bend. This spiral motion of the fluid increases the local flow velocity and the velocity gradient at the pipe wall, and therefore results in a greater frictional loss of head than that which occurs for the same rate of flow in a straight pipe of the same length and diameter.
The additional loss of head (apart from that due to usual friction) in flow through pipe bends is known as bend loss and is usually expressed as a fraction of the velocity head as, Kv2/2g where V is the average velocity of flow through the pipe. The value of K depends on the total length of the bend and the ratio of radius of curvature of the bend and pipe diameter R/D. The radius of curvature R is usually taken as the radius of curvature of the centre line of the bend. The factor K varies slightly with Reynolds number Re in the typical range of Re encountered in practice, but increases with surface roughness.

Losses in Piping Systems:
Objective: One of the most common problems in fluid mechanics is the estimation of Pressure loss. It is the objective of this experiment to enable pressure loss measurements to be made on several small bore pipe circuit components such as pipe bends valves and sudden changes in area of flow.

Description of Apparatus: The apparatus is shown diagrammatically in Figure 1. There are essentially two separate hydraulic circuit’s one painted dark blue, and the other painted light blue, but having common inlet and outlets. A hydraulic bench is used to circulate and measure water. Each one of the two pipe circuits contains a number of pipe system components. The components in each of the circuits are as follows:

Dark blue circuit:
1. Gate Valve
2. Standard Elbow Bend
3. 90o MITRE Bend
4. Straight Pipe
Light blue circuit:
5. Globe Valve
6. Sudden Expansion
7. Sudden Contraction
8. 150 mm 90o Radius Bend
9. 100 mm 90o Radius Bend
10. 60 mm 90o Radius Bend

In all cases (except the gate and globe valves) the pressure change across each of the component is measured by a pair of pressurized piezometer tubes. In the case of the valves, pressure measurement is made by U-tubes containing mercury.

Theoretical Background: For an incompressible fluid flowing through a pipe (Fig. 2) the following equations apply:
Q = V1A1 = V2A2 (continuity)                                                         (1)


Z1 +P1/ρg +V12/2g = Z2 +P2/ ρg + V22/2g hL1 -2                                    (2)


Head Loss: The head loss in a pipe circuit falls into two categories:
a) That due to viscous resistance extending throughout the total length of the circuit
b) That due to localized affects such as valves, sudden changes in area of flow and bends.
The overall head loss is a combination of both these categories. Because of the mutual interference that exists between neighboring components in a complex circuit, the total head loss may differ from that estimated from the losses due to the individual components considered in isolation.

Head loss in straight pipes: The head loss along a length L of straight pipe of constant diameter d is given by the expression:
                                    hL + 2f LV2/gd
                                   
or f =hLgd/2LV2
Where f is a dimensionless constant (i.e. friction factor) which is a function of the Reynolds’s number of the flow and the roughness of the internal surface of the pipe.


Head loss Due to Sudden Changes in Area of Flow:
i) Sudden Expansion - The head loss at a sudden expansion is given by

hL = (V1-V2)2 /2g                                            (4)

ii) Sudden contraction - The head loss at a sudden contraction is given by
hL = KV22/2g                                                   (5)

Where K is a dimensionless coefficient which depends upon the area ratio as shown in Table I.


Table 1: Loss Coefficient for Sudden Contractions




A2/A1
0
0.1
0.2
0.3
0.4
0.6
0.8
1.10
K
0.50
0.46
0.41
0.36
0.30
0.18
0.06
0
Head loss Due to Bends: The head loss due to a bend is given by the expression:

hB = KBV2/2g                                                  (6)

Where KB is a dimensionless coefficient which depends on the bend radius/pipe radius ratio and the angle of the bend. It should also be noted that the loss given by this expression is not the total loss caused by the bend but the excess loss above that which would be caused by a straight pipe equal in length to the length of the pipe axis.


Head loss Due to Valves: The head loss due to a valve is given by the expression:

                        hL = KV2/2g                                                                (7)

Where KB is a dimensionless coefficient which depends on the bend radius/pipe radius ratio and the angle of the bend. It should also be noted that the loss given by this expression is not the total loss caused by the bend but the excess loss above that which would be caused by a straight pipe equal in length to the length of the pipe axis.

Table 2: Loss Coefficient


Valve type
K
Globe valve, fully open
10.0
Gate valve, fully open
0.2
Gate valve, half open
5.6


Experimental Procedure:
1. Open fully the water control on the hydraulic bench.
2. With the globe valve closed, open the gate valve fully to obtain maximum flow through the dark blue circuit. Record the readings on he piezometer tubes and the U-tube. Measure the flow rate by timing the level rise in the volumetric tank.
3. Repeat the above procedure for a total of ten different flow rates obtained by closing the gate valve, equally spaced over the full flow range.
4. With a simple mercury in glass thermometer record the water temperature in the sump tank.
5. Close the gate valve, open the globe valve and repeat the experimental procedure for the light blue circuit.

Report (Data Analysis): In addition to tables showing all experimental results, the report must include the followings:

Dark blue circuit experiment:

a) Obtain the relationship between the straight pipe head loss and the volume flow rate (hL & Qn) by plotting log hL against log Q (log hL vs. log Q).
b) Plot friction factor data versus Reynolds’s number for the straight pipe (L = 0.914 m, D = 13.7 mm). Also, obtain relationship between f & Ren by plotting log f against log Re. Comment on your result by comparing with the literature given equations (i.e. f =0.04 Re-0.16 for 4000<Re<107 & f = 0.079 Re-1/4 for 4000< Re < 105 ).
c) Obtain the value of K for the gate valve when it is fully opened and compare with literature (Table 2).
d) Discuss head losses in 90° Mitre and Standard Elbow bend.



Light blue circuit experiment:

a) If head rise across a sudden expansion (13.7 mm / 26.4 mm) is given by expression       
                       
hL = 1.303V12/2g
Compare this head rise with the measured head rise. Plot the measured and the calculated head rise.
b) If head loss due to sudden contraction (26.4 mm / 13.7 mm) is given by the expression
                        hL = 1.303V22/2g
 Compare this fall in the head with the measured head loss. Plot the measured and calculated fall in head due to sudden contraction.
c) Obtain the value of K for the globe valve when it is fully opened and compare with literature (Table 2)
d) What is the effect of bend radius on head losses?



Notation:
Q         volumetric flow rate, (m3/s)
V         mean velocity, (m/s)
A         cross-sectional area, (m2)
Z          height above datum, (m)
P          static pressure, (N/m2)
hL         head loss, (m)
ρ          density, (kg/m3)
g          acceleration due to gravity, (9.81 m/s2)
f           Friction factor
d          Diameter of pipe, (m)
L          Length of pipe, (m)
K         Loss Coefficient
KB      Loss coefficient due to bends
Re        Reynolds Number




Secondary losses in bends and fittings:

Objectives: It is required demonstrate the secondary losses through different types of bends and fittings.
Experimental Procedure:
1. Close the regulation valve and start the centrifugal pump.
2. Open the valve partially.
3. Wait for steady flow (piezometers readings=constant).
4. Read the differential readings of the peizometers connected to the mite the elbow, the short the enlargement and the contraction.
5. Read the initial volume in the collection tank V1.
6. Observe the time (t) to increase the collected volume to V2.
7. Increase the valve opening.
8. Repeat the experiment tow times.
9. After recording all the required readings, close the valve gradually then stop the centrifugal pump.
Conclusion: We learn here about different types of bends losses and how we will measure it.
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Control Dynamics for Vehicle


Executive Summary:
The dynamics of motor vehicle motion is an important field of study as it relates to safety, accident investigation and general ground vehicle performance. Aircraft are free to fly in the air, while ships can move freely on the water surface. In the same way, the road vehicle is free to move, by steering its wheels, and shares similarities with aircraft and ships, in the sense that its movements are unrestricted. From the viewpoint of dynamic motion, the similarity lies in the fact that these three moving bodies receive forces generated by their own movement that are used to accomplish the desired movement. Aircraft depend on the lift force caused by the relative motion of its wings and the air; ships rely on the lift force brought by the relative motion of its body and the water; and ground vehicles rely on the wheel lateral force created by the relative motion of the wheels and the road. For the study of vehicle dynamics and control, a typical vehicle mathematical model is assumed. This vehicle model has wheels that are steerable: two at the front and two at the rear, which are fitted to a rigid body. Passenger cars, trucks, 1 bus, and agricultural vehicles all fall into this category. At first sight, it may seem that there are no common dynamics among these vehicles, but by applying a simple four-wheeled vehicle model, as in Fig. 1.1, it is possible to obtain fundamental knowledge of the dynamics of all these vehicles. In the vehicle mathematical model, which is presented in Fig. 1.1, the wheels are regarded as weightless, and the rigid body represents the total vehicle weight. The coordinate system is fixed to the vehicle, the x-axis in the longitudinal direction, the y-axis in the lateral direction, and the z-axis in the vertical direction, with the origin at the vehicle center of gravity. Generally, when a vehicle is traveling in a straight line, the heading direction of the wheel coincides with the traveling direction. In other words, the wheel traveling direction is in line with the wheel rotational plane. However, when the vehicle has lateral motion and/or yaw motion, the traveling direction can be out of line with the rotational plane.




Chapter One
Vehicle Design and Manufacturing

 
1. Introduction
Ground vehicles can be divided into two main categories: vehicles that are restricted by a track set on the ground (e.g., the railway vehicles) and vehicles that are unrestricted by tracks, free to move in any direction on the ground by steering the wheels (e.g., road vehicles). Aircraft are free to fly in the air, while ships can move freely on the water surface. In the same way, the road vehicle is free to move, by steering its wheels, and shares similarities with aircraft and ships, in the sense that its movements are unrestricted. From the viewpoint of dynamic motion, the similarity lies in the fact that these three moving bodies receive forces generated by their own movement that are used to accomplish the desired movement. Aircraft depend on the lift force caused by the relative motion of its wings and the air; ships rely on the lift force brought by the relative motion of its body and the water; and ground vehicles rely on the wheel lateral force created by the relative motion of the wheels and the road. In the above described manner, the dynamics and control of the three moving bodies are closely related to their natural function, whereby for an airplane, it is established as flight dynamics, a ship as ship dynamics, and a vehicle, similarly, as vehicle dynamics. The vehicle studied in this book, is a vehicle, similar to the airplane and ship that is capable of independent motion on the ground, using the forces generated by its own motion.

1.2 Design
Introducing a new model of automobile generally takes three to five years from inception to assembly. Ideas for new models are developed to respond to unmet pubic needs and preferences. Trying to predict what the public will want to drive in five years is no small feat, yet automobile companies have successfully designed automobiles that fit public tastes. With the help of computer-aided design equipment, designers develop basic concept drawings that help them visualize the proposed vehicle's appearance. Based on this simulation, they then construct clay models that can be studied by styling experts familiar with what the public is likely to accept. Aerodynamic engineers also review the models, studying air-flow parameters and doing feasibility studies on crash tests. Only after all models have been reviewed and accepted are tool designers permitted to begin building the tools that will manufacture the component parts of the new model.

1.3 The Manufacturing Process:

1.3.1 Components

  • 1 The automobile assembly plant represents only the final phase in the process of manufacturing an automobile, for it is here that the components supplied by more than 4,000 outside suppliers, including company-owned parts suppliers, are brought together for assembly, usually by truck or railroad. Those parts that will be used in the chassis are delivered to one area, while those that will comprise the body are unloaded at another.

Fig 01: Components of Motor Vehicle

1.3.2 Chassis
2 The typical car or truck is constructed from the ground up (and out). The frame forms the base on which the body rests and from which all subsequent assembly components follow. The frame is placed on the assembly line and clamped to the conveyer to prevent shifting as it moves down the line. From here the automobile frame moves to component assembly areas where complete front and rear suspensions, gas tanks, rear axles and drive shafts, gear boxes, steering box components, wheel drums, and braking systems are sequentially installed.

Fig 02: Workers install engines on Model Ts at a Ford Motor Company plant. The photo is from about 1917.

The automobile, for decades the quintessential American industrial product, did not have its origins in the United States. In 1860, Etienne Lenoir, a Belgian mechanic, introduced an internal combustion engine that proved useful as a source of stationary power. In 1878, Nicholas Otto, a German manufacturer, developed his four-stroke "explosion" engine. By 1885, one of his engineers, Gottlieb Daimler, was building the first of four experimental vehicles powered by a modified Otto internal combustion engine. Also in 1885, another German manufacturer, Carl Benz, introduced a three-wheeled, self-propelled vehicle. In 1887, the Benz became the first automobile offered for sale to the public. By 1895, automotive technology was dominated by the French, led by Emile Lavassor. Lavassor developed the basic mechanical arrangement of the car, placing the engine in the front of the chassis, with the crankshaft perpendicular to the axles.
In 1896, the Duryea Motor Wagon became the first production motor vehicle in the United States. In that same year, Henry Ford demonstrated his first experimental vehicle, the Quadricycle. By 1908, when the Ford Motor Company introduced the Model T, the United States had dozens of automobile manufacturers. The Model T quickly became the standard by which other cars were measured; ten years later, half of all cars on the road were Model Ts. It had a simple four-cylinder, twenty-horsepower engine and a planetary transmission giving two gears forward and one backward. It was sturdy, had high road clearance to negotiate the rutted roads of the day, and was easy to operate and maintain.
  • 3 An off-line operation at this stage of production mates the vehicle's engine with its transmission. Workers use robotic arms to install these heavy components inside the engine compartment of the frame. After the engine and transmission are installed, a

Fig 03: Vehicle Installation

On automobile assembly lines, much of the work is now done by robots rather than humans. In the first stages of automobile manufacture, robots weld the floor pan pieces together and assist workers in placing components such as the suspension onto the chassis.
Worker attaches the radiator, and another bolts it into place. Because of the nature of these heavy component parts, articulating robots perform all of the lift and carry operations while assemblers using pneumatic wrenches bolt component pieces in place. Careful ergonomic studies of every assembly task have provided assembly workers with the safest and most efficient tools available.

1.3.3 Body
  • 4 Generally, the floor pan is the largest body component to which a multitude of panels and braces will subsequently be either welded or bolted. As it moves down the assembly line, held in place by clamping fixtures, the shell of the vehicle is built. First, the left and right quarter panels are robotically disengaged from pre-staged shipping containers and placed onto the floor pan, where they are stabilized with positioning fixtures and welded.
5 The front and rear door pillars, roof, and body side panels are assembled in the same fashion. The shell of the automobile assembled in this section of the process lends itself to the use of robots because articulating arms can easily introduce various component braces and panels to the floor pan and perform a high number of weld operations in a time frame and with a degree of accuracy no human workers could ever approach. Robots can pick and load 200-pound (90.8 kilograms) roof panels and place them precisely in the proper weld position with tolerance variations held to within .001 of an inch. Moreover, robots can also tolerate the

Fig 04: Body Construction

The body is built up on a separate assembly line from the chassis. Robots once again perform most of the welding on the various panels, but human workers are necessary to bolt the parts together. During welding, component pieces are held securely in a jig while welding operations are performed. Once the body shell is complete, it is attached to an overhead conveyor for the painting process. The multi-step painting process entails inspection, cleaning, undercoat (electrostatically applied) dipping, drying, topcoat spraying, and baking. smoke, weld flashes, and gases created during this phase of production. 6 As the body moves from the isolated weld area of the assembly line, subsequent body components including fully assembled doors, deck lids, hood panel, fenders, trunk lid, and bumper reinforcements are installed. Although robots help workers place these components onto the body shell, the workers provide the proper fit for most of the bolt-on functional parts using pneumatically assisted tools.

Fig 05: Body of a Motor Vehicle

1.3.4 Paint
  • 7 Prior to painting, the body must pass through a rigorous inspection process, the body in white operation. The shell of the vehicle passes through a brightly lit white room where it is fully wiped down by visual inspectors using cloths soaked in hi-light oil. Under the lights, this oil allows inspectors to see any defects in the sheet metal body panels. Dings, dents, and any other defects are repaired right on the line by skilled body repairmen. After the shell has been fully inspected and repaired, the assembly conveyor carries it through a cleaning station where it is immersed and cleaned of all residual oil, dirt, and contaminants.
  • 8 As the shell exits the cleaning station it goes through a drying booth and then through an undercoat dip—an electrostatically charged bath of undercoat paint (called the E-coat) that covers every nook and cranny of the body shell, both inside and out, with primer. This coat acts as a substrate surface to which the top coat of colored paint adheres.
  • 9 After the E-coat bath, the shell is again dried in a booth as it proceeds on to the final paint operation. In most automobile assembly plants today, vehicle bodies are spray-painted by robots that have been programmed to apply the exact amounts of paint to just the right areas for just the right length of time. Considerable research and programming has gone into the dynamics of robotic painting in order to ensure the fine "wet" finishes we have come to expect. Our robotic painters have come a long way since Ford's first Model Ts, which were painted by hand with a brush.
  • 10 Once the shell has been fully covered 1 V with a base coat of color paint and a clear top coat, the conveyor transfers the bodies through baking ovens where the paint is cured at temperatures exceeding 275 degrees Fahrenheit (135 degrees Celsius).

Fig 06: Painting
The body and chassis assemblies are mated near the end of the production process. Robotic arms lift the body shell onto the chassis frame, where human workers then bolt the two together. After final components are installed, the vehicle is driven off the assembly line to a quality checkpoint.
After the shell leaves the paint area it is ready for interior assembly.

1.3.5 Interior assembly
  • 11 The painted shell proceeds through the interior assembly area where workers assemble all of the instrumentation and wiring systems, dash panels, interior lights, seats, door and trim panels, headliners, radios, speakers, all glass except the automobile windshield, steering column and wheel, body weather strips, vinyl tops, brake and gas pedals, carpeting, and front and rear bumper fascias.
  • 12 Next, robots equipped with suction cups remove the windshield from a shipping container, apply a bead of urethane sealer to the perimeter of the glass, and then place it into the body windshield frame. Robots also pick seats and trim panels and transport them to the vehicle for the ease and efficiency of the assembly operator. After passing through this section the shell is given a water test to ensure the proper fit of door panels, glass, and weather stripping. It is now ready to mate with the chassis.

Fig 07: Interior Design

1.3.6 Mate

  • 13 The chassis assembly conveyor and the body shell conveyor meet at this stage of production. As the chassis passes the body conveyor the shell is robotically lifted from its conveyor fixtures and placed onto the car frame. Assembly workers, some at ground level and some in work pits beneath the conveyor, bolt the car body to the frame. Once the mating takes place the automobile proceeds down the line to receive final trim components, battery, tires, anti-freeze, and gasoline.
  • 14 The vehicle can now be started. From here it is driven to a checkpoint off the line, where its engine is audited, its lights and horn checked, its tires balanced, and its charging system examined. Any defects discovered at this stage require that the car be taken to a central repair area, usually located near the end of the line. A crew of skilled trouble-shooters at this stage analyze and repair all problems. When the vehicle passes final audit it is given a price label and driven to a staging lot where it will await shipment to its destination.

1.4 Quality Control
All of the components that go into the automobile are produced at other sites. This means the thousands of component pieces that comprise the car must be manufactured, tested, packaged, and shipped to the assembly plants, often on the same day they will be used. This requires no small amount of planning. To accomplish it, most automobile manufacturers require outside parts vendors to subject their component parts to rigorous testing and inspection audits similar to those used by the assembly plants. In this way the assembly plants can anticipate that the products arriving at their receiving docks are Statistical Process Control (SPC) approved and free from defects.
Once the component parts of the automobile begin to be assembled at the automotive factory, production control specialists can follow the progress of each embryonic automobile by means of its Vehicle Identification Number (VIN), assigned at the start of the production line. In many of the more advanced assembly plants a small radio frequency transponder is attached to the chassis and floor pan. This sending unit carries the VIN information and monitors its progress along the assembly process. Knowing what operations the vehicle has been through, where it is going, and when it should arrive at the next assembly station gives production management personnel the ability to electronically control the manufacturing sequence. Throughout the assembly process quality audit stations keep track of vital information concerning the integrity of various functional components of the vehicle.
This idea comes from a change in quality control ideology over the years. Formerly, quality control was seen as a final inspection process that sought to discover defects only after the vehicle was built. In contrast, today quality is seen as a process built right into the design of the vehicle as well as the assembly process. In this way assembly operators can stop the conveyor if workers find a defect. Corrections can then be made, or supplies checked to determine whether an entire batch of components is bad. Vehicle recalls are costly and manufacturers do everything possible to ensure the integrity of their product before it is shipped to the customer. After the vehicle is assembled a validation process is conducted at the end of the assembly line to verify quality audits from the various inspection points throughout the assembly process. This final audit tests for properly fitting panels; dynamics; squeaks and rattles; functioning electrical components; and engine, chassis, and wheel alignment. In many assembly plants vehicles are periodically pulled from the audit line and given full functional tests. All efforts today are put forth to ensure that quality and reliability are built into the assembled product.

Fig 08: Stress of a Vehicle

1.5 The Future
The development of the electric automobile will owe more to innovative solar and aeronautical engineering and advanced satellite and radar technology than to traditional automotive design and construction. The electric car has no engine, exhaust system, transmission, muffler, radiator, or spark plugs. It will require neither tune-ups nor—truly revolutionary—gasoline. Instead, its power will come from alternating current (AC) electric motors with a brushless design capable of spinning up to 20,000 revolutions/minute. Batteries to power these motors will come from high performance cells capable of generating more than 100 kilowatts of power. And, unlike the lead-acid batteries of the past and present, future batteries will be environmentally safe and recyclable. Integral to the braking system of the vehicle will be a power inverter that converts direct current electricity back into the battery pack system once the accelerator is let off, thus acting as a generator to the battery system even as the car is driven long into the future.
The growth of automobile use and the increasing resistance to road building have made our highway systems both congested and obsolete. But new electronic vehicle technologies that permit cars to navigate around the congestion and even drive themselves may soon become possible. Turning over the operation of our automobiles to computers would mean they would gather information from the roadway about congestion and find the fastest route to their instructed destination, thus making better use of limited highway space. The advent of the electric car will come because of a rare convergence of circumstance and ability. Growing intolerance for pollution combined with extraordinary technological advancements will change the global transportation paradigm that will carry us into the twenty-first century.

1.6             Virtual Four-Wheel Vehicle Model
For the study of vehicle dynamics and control, a typical vehicle mathematical model is assumed. This vehicle model has wheels that are steerable: two at the front and two at the rear, which are fitted to a rigid body. Passenger cars, trucks, 1 buses, and agricultural vehicles all fall into this category.At first sight, it may seem that there are no common dynamics among these vehicles, but by applying a simple four-wheeled vehicle model, it is possible to obtain fundamental knowledge of the dynamics of all these vehicles. In the vehicle mathematical model, which is presented in the wheels are regarded as weightless, and the rigid body represents the total vehicle weight. The coordinate system is fixed to the vehicle, the x-axis in the longitudinal direction, the y-axis in the lateral direction, and the z-axis in the vertical direction, with the origin at the vehicle center of gravity. With this coordinate system, the vehicle motion has six independent degrees of freedom:
1. vertical motion in z direction,
2. left and right motion in y direction,
3. longitudinal motion in x direction,
4. rolling motion around x-axis,
5. pitching motion around y-axis,
6. yawing motion around z-axis.
These can be divided into two main groups. One group consists of 1, 3, and 5 motions, which are the motions generated without direct relation to the steering. Motion 1 is the vertical motion caused by an uneven ground/road surface and is related to the vehicle ride. Motion 3 is the longitudinal, straight-line motion of the vehicle due to traction and braking during acceleration or braking. Motion 5 is the motion caused by either road unevenness, acceleration or braking and is also related to the vehicle ride. Motions 2 and 6, the yaw and lateral movements, are generated initially by steering the vehicle. Motion 4 is generated mainly by motions 2 and 6 but could occur due to road unevenness as well. As described earlier, the vehicle studied in this text can move freely in any direction on the ground, by steering the vehicle. The main behaviors studied here are motions 2, 4, and 6, which are caused by the steering of the vehicle.

Fig 09: Vehicle dynamics model.

Chapter Two
Motion and Force



2. Control of Motion
For normal vehicles, motions are controlled by the driver. The lateral, yaw, and roll motions of the vehicle are generated by the driver’s steering and depend on its dynamic characteristics. This doesn’t mean that the driver is steering the vehicle meaninglessly. The driver is continuously looking at the path in front, either following his target path, or setting a new target path to follow. The driver is observing many things, such as the current position of the vehicle with reference to the target path and the current vehicle motion. The driver is also predicting the imminent vehicle behavior. Based on this information, the driver decides and makes the suitable steer action. In this manner, the vehicle generates its motion in accordance to a target path that is a given or path set by the driver. The vehicle that is capable of free motion within a plane, without direct restrictions from preset tracks on the ground, only produces a meaningful motion when it is acted on by suitable steering control from the driver. The primary interest now lies on the inherent dynamic characteristics of the vehicle itself. This becomes clear from the motion of the vehicle to a certain steering input. Next is to study this vehicle’s characteristics when it is controlled by a human driver. Finally, the aim is to explore the vehicle dynamic characteristics that make it easier for the driver to control the vehicle.

2.1 Tire and side-slip angle
Generally, when a vehicle is traveling in a straight line, the heading direction of the wheel coincides with the traveling direction. In other words, the wheel traveling direction is in line with the wheel rotational plane. However, when the vehicle has lateral motion and/or yaw motion, the traveling direction can be out of line with the rotational plane is the wheel looked at from the top, where (a) is when the traveling direction is in line with the rotation plane, and (b) is when it is not.
(a)                                                                      (b)
Fig 10:  Vehicle tire in motion.

The wheel in (b) is said to have side slip. The angle between the wheel traveling direction and the rotational plane, or its heading direction, is called the side-slip angle. The wheel is also acted on by a traction force if the wheel is moving the vehicle in the traveling direction, or braking force if braking is applied. Also, a rolling resistance force is always at work. If the wheel has side slip, as in (b), a force that is perpendicular to its rotation plane is generated. This force could be regarded as a reaction force that prevents side slip when the wheel produces a side-slip angle. This is an important force that the vehicle depends on for its independent motion. Normally, this force is called the lateral force, while the component that is perpendicular to the wheel rotation plane, is called the cornering force. When the side-slip angle is small, these two are treated as the same. This force corresponds to the lift force, explained in fluid dynamics, which acts on a body that travels in a fluid at an attack angle, as shown in. There are many kinds of wheels, but all produce a force perpendicular to the rotation plane, when rotated with side slip. The schematic comparison of the lateral forces, at small side-slip angles, for a pneumatic tire wheel, a solid rubber-tire wheel, and an iron wheel. From here, it is clear that the magnitude of the force produced depends on the type of wheel and is very different. In particular, the maximum possible force produced by an iron wheel is less than 1/3rd of that produced by a rubber tire wheel. Compared to a solid rubber-tire wheel, a pneumatic tire wheel produces a larger force. For independent motion of the vehicle, the force that acts on a wheel with side slip is desired to be as large as possible. For this reason, the traveling vehicle that is free to move in the plane, without external restrictions, is usually fitted with pneumatic tires. These are fitted for both the purpose of vehicle ride, and for achieving a lateral force that is available for vehicle handling. In the following chapter, the pneumatic tire is called the tire, and the mechanism for generating a lateral force that acts on a tire with side slip is explained.

Fig 11: Lifting force.

2.2 Deformation of tire with side slip and lateral force
Generally, forces act through the contact surface between the tire and the road. A tire with lateral slip is expected to deform in the tire contact surface and its outer circumference: (a) shows the front and side views of the tire deformation; (b) shows the tire contact surface and outer circumference deformation viewed from the top. At the front of the surface, the deformation direction is almost parallel to the tire’s traveling direction. In this part, there is no relative slip to the ground
Fig 12: Lateral forces for several wheels.
A                                             B

Fig 13: Tire deflection with side slip.

When the tire slip angle is small, the whole contact surface is similar to this and the rear end of the contact surface has the largest lateral deformation. When the tire slip angle gets bigger, the front of the surface remains almost parallel to the tire traveling direction. The deformation reduces near the center of the contact patch, and the lateral deformation becomes largest at certain point between the front and rear of the surface. After this maximum, the tire contact surface slips away from the tire centerline and the lateral deformation does not increase. As tire slip angle gets even larger, the point where lateral deformation becomes maximum moves rapidly toward the front. When the slip angle is around 10–12_, the contact surface that is parallel to the tire travel direction disappears. The contact surface deformation is nearly symmetric around the wheel center and consists of nearly all the slip regions. The lateral deformation of the tire causes a lateral force to act through the contact surface, which is distributed according to the deformation. This lateral force is sometimes called the cornering force when the side-slip angle is small. By looking at the tire lateral deformation, the resultant lateral force may not be aligned with center of the contact surface. Thus, the lateral force creates a moment around the tire contact surface center. This moment is called the selfaligning torque and acts in the direction that reduces the tire slip angle.

2.2.1 Tire camber and lateral force
The angle between the tire rotation plane and the vertical axis is called the camber angle. If a tire with a camber angle of f is rotated freely on a horizontal plane, as shown in Fig. 2.5, the tire makes a circle with the radius of R=sin f and origin at O. If the circular motion is prohibited for a tire with camber angle, and the tire is forced to travel in a straight line only, a force will

Fig 14: Tire with camber angle and camber thrust.

act on the tire as shown in the figure. This force, due to the camber between the tire and the ground, is called camber thrust.

2.2.2 Tire Cornering Characteristics
The characteristics of the tire that produce lateral force and moment, as elaborated in Section 2.2, are defined as the cornering characteristics. In this section, the tire cornering characteristics will be examined in more detail.

2.3 Fiala’s theory
The mathematical model proposed by Fiala is widely accepted for the above analysis of the lateral force due to side slip of the tire. It is commonly called Fiala’s theory and is related to the tire cornering characteristics. It is one of the fundamental theories used by many people for explaining tire cornering characteristics. Here, based on Fiala’s theory, the tire cornering characteristics will be studied theoretically. The tire structure is modeled. A is a stiff body equivalent to the rim. B is the pneumatic tube and sidewall that can deform elastically in both vertical and lateral directions. C is the equivalent thin tread base joined to the sidewall at both sides. D is equivalent to the tread rubber. The tread rubber is not a continuous circular body, but consists of large numbers of independent spring bodies around the tire circumference. When a force acts in the lateral direction at the ground contact surface, the tire will deform in the lateral direction. The rim is stiff and it will not be deformed, but the tread base will have a bending deformation in the lateral direction. Moreover, the tread rubber will be deformed by the shear force between the tread base and ground surface. shows this kind of deformation in the lateral direction. Assuming that the tread base deforms equally at the front and rear ends of the ground contact surface, the line that connects these points is the centerline for the tread base and is defined as the x-axis. The y-axis is perpendicular to the x-axis and positioned at the front end point. The x-axis is parallel to the tire rim centerline and also the tread base centerline before deformation.
Fig15: Tire structural model.

2.4 Effects

2.4.1 Effects of Vertical Load and Road Condition

The effect of tire vertical load on lateral force is also shown in. The tire vertical load has almost no effect on lateral force at very small side-slip angles. The different saturation levels of lateral force become more obvious with larger side-slip angles. The mathematical model shows that the tire load only affects lateral force in the region where there is relative slip between the tread rubber and the ground. When this region occupies the majority of the contact surface, i.e., side-slip angle is large, the lateral force approaches the product of m and W, and so, the effect of  W is remarkable. Figure shows the effect of the tire vertical load effect on lateral force. Next is to study the effect of the tire vertical load on the tire cornering stiffness. when the tire load is small, the cornering stiffness increases together with the tire load, but after a certain limit, it seems to decrease. The cornering stiffness, divided by the corresponding tire load, is called the cornering stiffness coefficient. This cornering stiffness coefficient decreases with tire load almost linearly, In relation to tire load, cornering stiffness could be approximated as a parabolic that passes through the origin. Cornering stiffness increases with tire load to a peak value and beyond that it decreases. Tires are normally used in the region where cornering stiffness increases with vertical load. The dependence of tire cornering stiffness on tire load for a real tire. The approximation to a parabolic is verified. Usually, the effect of the tire vertical load is expressed in the form of mW: The friction coefficient between the tread rubber and ground, m; is expected to have an effect similar to the tire vertical load. The effects of the road surfaces on the cornering force as it changes with side-slip angle. From the figure, it can be seen that the friction coefficient has almost no effect on lateral force at small side-slip angles, but has a more obvious effect as side-slip angles get larger. The effect of friction coefficient on the lateral force is very similar to the vertical.
Fig 16: Effects of road surface on lateral force.

2.4.2 Tire Pressure Effects
From analysis of the mathematical model, it is clear that the tire lateral force becomes larger with a smaller tread base displacement under a constant force. From Equation, y becomes smaller with smaller a3l2=ð2kÞ: If k, the spring constant of the spring support, is large, and the tread base bending stiffness, EI, is also large, then the tread base displacement is small. Since spring constant, k, depends on tire air pressure, it is expected that cornering force also increases with tire pressure. However, the increase of tire pressure reduces the contact surface length, l, and Eqn (2.15) shows that the lateral force decreases with a decrease in contact length. Figure 16 is a good example of the relationship between lateral force and tire pressure. The increase of tire pressure contributes to the increase of k and an increase in the lateral force is expected; however, the reduction of the contact length, l, due to the increase of the tire pressure decreases the lateral force. Eventually, it is interesting to see that the lateral force is almost constant with the variation in the tire pressure in this case. The above point is shown in more detail by the relation of the cornering stiffness to the tire pressure. If the vertical load is relatively low, the decrease in contact length contributes more than the increase of k as the tire pressure increases. In this case, the cornering stiffness decreases with an increase in tire pressure. On the other hand, if the vertical load is relatively high, the effect of the increasing k is dominant compared with the decrease in the contact length and the cornering stiffness increases with the tire pressure. However, with even higher vertical loads, the excessive increase of the tire pressure has a greater effect on the contact length reduction and the cornering stiffness decreases with the increase of the tire pressure

2.4.3 Tire Shape Effects
The tread base bending stiffness, EI, is decided by the tire shape. If the tire material and the construction are given, the shape effect is dominated by the moment of inertia, I, of the tread base. This is generally larger for a larger tire. For tires with the same radius, it is larger for flatter tires with larger width. Therefore, low profile tires are desirable for obtaining larger cornering force. The cornering stiffness increases when b is larger and d is smaller. Figure 17 is an example of the relationship between the cornering stiffness and the tread depth, which corresponds to the tread rubber thickness. From this figure, the increase in cornering stiffness is seen for a tire with smaller d, i.e., with worn tread.

Fig 17: Effect of tire slit depth on cornering stiffness.

2.4.4 Braking and Traction Force Effects
The effects of tire parameters and vertical load on the lateral force have already been studied. During braking or traction, the tire is acted on by the vertical load that supports the vehicle weight and the longitudinal force at the contact surface that accelerates or stops the vehicle. These forces also affect the lateral force. Based on the classical Law of Friction, and as shown in Fig.18, the lateral force, F, and traction force (or braking force) T, acting on a tire, must always satisfy the following equation.


Fig 18: Friction circle.
In other words, the resultant of the horizontal, in-plane, forces that act on the contact surface between the tire and the ground cannot exceed the product of the tire load and the friction coefficient. This means that the resultant force vector is restricted to be inside a circle with radius mW: This circle is called the friction circle. If there is a longitudinal force, either traction force or braking force, acting on the tire, the maximum cornering force, for a large side-slip angle, is given by,
and, if T ¼ 0, then the above is the same as in Eqn (2.25). The relation of lateral force, F0, to side-slip angle, when traction or braking force is zero, is given by the line O–A0 in Fig. 2.25. The relation of lateral force to side-slip angle, when traction (or braking) force, T, is at work, is given by line O–A in the same figure. If the reduction ratio of lateral force due to traction (or braking) force is assumed to be the same at any side-slip angle.

2.5  Self-aligning torque
The theoretical analysis with the mathematical model shows that when the sideslip angle is small, the self-aligning torque increases linearly with side-slip angle, but when side-slip angle is large, the self-aligning torque approaches saturation and reaches its peak at a certain value. After this point, the self aligning torque decreases with side-slip angle. Figure 19 is a typical example of the relation between self-aligning torque and side-slip angle of a real tire. In Fig 19, the effect of tire load on self-aligning torque is shown together with the side slip. The effect of tire load on lateral force is small at small sideslip angles, and large at large side-slip angles. In comparison, the effect of tire
load on self-aligning moment is large at any side-slip angle. One of the reasons for this is that the load effect occurs in the region where there is relative slip between the contact surface and the tread rubber, and self-aligning torque itself also has a greater contribution from the lateral force acting at both the ends of the contact surface. Another reason is that the contact surface length increases with tire load and the moment produced by the acting lateral force increases too. This could be verified from Eqn. where the third order or more term of l is included in the equation. If the tire pressure is increased, as seen from the previous discussion, the lateral force increases in some cases and the self-aligning torque also increases. However, on a real tire, self-aligning torque decreases if the tire pressure is increased. It is thought that while even though the lateral force increases with tire pressure, the contact surface length decreases with tire pressure. This has a large effect on self-aligning torque. Self-aligning torque increases if the tire pressure is decreased, but beyond a certain limit, the self-aligning torque does not increase with decreasing tire pressure. It is thought that if the tire pressure is too small, the decrease in lateral force has a larger effect than the effect of  increasing the contact surface length. Self-aligning torque is the moment of the lateral force around the vertical axis that passes through the contact surface center. The relationship between xn ¼ M=F and j: The result shows that xn decreases dramatically when side-slip angle becomes larger.


2.6 Camber thrust
From Eqn (2.36), it is expected that the camber thrust of a tire is proportional to the camber angle when the side-slip angle is zero. The relationship between the camber angle and camber thrust of a normal tire. This example shows that the camber thrust is proportional to the camber angle. The effect of tire load is also noted in the same figure. As seen from the figure, the camber thrust coefficient, which is the camber thrust per unit camber angle, increases almost linearly with tire load. The tread base effective radius, R0 and depends on tire vertical load, W, as in Eqn. The contact surface length also increases with tire load. From Eqn, it is understood that camber thrust coefficient depends on tire vertical load, and increases with tire vertical load. Moreover, from the same equation, the camber thrust coefficient is equal to the product of the cornering stiffness and l/(6R0). It can now be assumed that the camber thrust coefficient has similar characteristics to the cornering stiffness. Since the ratio of contact surface length l to effective radius R0, l/R0, is generally about 0.3, the camber thrust coefficient is normally less than 1/10th of the cornering stiffness. So far, the camber thrust and lateral force produced by side-slip angle have been considered. However, the normal tire that is fitted to a real vehicle usually has both side-slip angle and camber during its travel. In this case, the tire is simultaneously acted on by the lateral force and the camber thrust and it is regarded that they act independently. The lateral force due to both side-slip angle and camber angle, as shown by Ellis. The curves showing the relationship between camber angle and lateral force, at different side-slip angles, and the curves showing the relation of side-slip angle and lateral force, at different camber angles, are both parallel to each other. This shows that the lateral forces acting on the tire, produced by the camber angle and the side-slip angle, can be treated individually and independently. In recent years, low profile tires have become more popular, especially among passenger cars. When this kind of tire cambers, the lateral distribution of the tire load in contact plane could easily give larger tire loads at the inner side, and smaller loads at the outer side. This kind of unequal distribution, compared to the case of equal distribution, causes a decrease in the generated lateral force at an axle. This is anticipated from the dependency of the lateral force and

Fig 19: Effect of camber angle on tire lateral force.

cornering stiffness on the tire vertical load, which is shown by parabolic curves in Figs 2.17 and 2.19. The decrease of the lateral force due to a reduction in tire load is larger than the increase of the lateral force due to a tire load increase. Consequently, even in cases where the camber angle is added so that the camber thrust and the lateral force caused by side-slip angle are in the same direction, the total lateral force produced by the tire with both side-slip angle and the camber anglemay be reduced. This is due to the decrease of lateral force caused by tire load distribution changes, which in turn are caused by the camber angle.
Fig 20: Effects of camber angle on lateral force of kart tire with small aspect ratio.



Chapter Three
Mathematical Analysis







3.0 Mathematical model

The tire cornering characteristics from Fiala’s theory have been explained. The mathematical model assumes that with side slip, the tire tread base deforms elastically in the lateral direction toward the tire rim and, at the same time, the tread rubber deforms elastically further more toward the tread base. The effect of longitudinal force, such as traction and braking, could be considered using the same mathematical model, but the model would become too complex. Instead, how the tread rubber is fitted circumferentially to the stiff rim, and the tread base is the only elastic part. This model allows elastic deformation in both the longitudinal and lateral directions. The tread rubber, similar to the previous model, is not a continuous circular body, but consists of a large number of independent springs around the tire circumference. This type of tire model is called the brush model. This tire model will be used to understand theoretically the force generated by the tire in the longitudinal and lateral directions.

Fig 21: Tire deformable in lateral and longitudinal directions.

3.1 Tire lateral force during traction and braking
The tire is rotating with an angular velocity, u; while traveling in a direction that forms an angle of b to the rotation plane. The velocity component in the rotation plane is taken as u. Three forces act upon this tire, namely the longitudinal force, Fx, lateral force, Fy, and vertical force, Fz.

3.1.1 Braking
The front end point of the tire contact surface centerline is taken as the origin of the coordinate axes, with the x-axis in longitudinal direction, and the y-axis in lateral direction. The point on the tread base directly on top of point O is taken as point O0. After a fraction of time, Dt; the contact surface point moves from O to P, and the point O0 on the tread base moved to P0. The projected point P0 on x-axis is marked as P00.
Fig 22: Tire forces in three directions.
The motion of the vehicle for a given steer input is studied and the mechanics of vehicle motion are explained. Only vehicle responses to a predetermined steering action are studied in this chapter, steering in response to vehicle motion is studied later in the book. There is an enormous amount of previous work that has studied the vehicle response to a predetermined steering action. These studies have established the fundamentals of vehicle dynamics. This chapter describes these fundamentals, which are necessary for understanding of the independent vehicle motion due to steering, i.e., the vehicle dynamics problem.

3.2 Vehicle Equation of Motion
The first chapter identified the vehicle motion degrees of freedom that should be considered as lateral, yaw, and roll. However, to understand the basic characteristics of vehicle motion, more simplicity is needed, provided the nature of the problem is not lost. The transient phenomena of the vehicle, such as sudden acceleration or deceleration are omitted, as is the case of a sudden large steer action. With these preconditions, the vehicle can be assumed to be traveling at a constant speed, and the roll motion can be neglected. If a vehicle travels at constant speed, and without roll, the vehicle vertical height can be neglected and only the lateral and yawing motions need to be considered. The vehicle is represented as a rigid body projected to the ground. In describing the motion of the rigid body, the definition of a reference coordinate frame is necessary. Depending on particular body motion 47 characteristics, there could be many ways of defining the coordinates for describing the body motion. Clever definition of a coordinate frame can simplify the description of the body motion, so selection of suitable coordinates for a particular body is important. Considering this, it is sensible to first derive the fundamental vehicle equations of motion.
3.2.1 Equations of motion with fixed coordinates on the vehicle
Consider the vehicle moving in the horizontal plane. The vehicle longitudinal and lateral directions are continuously changing with reference to a fixed coordinate frame on the ground. If the vehicle is examined on-board, regardless of the direction of the vehicle, the motion constraints are basically unchangeable. It is more convenient to describe the vehicle motion by fixed coordinates on the vehicle rather than by fixed coordinates on the ground. X–Yare the fixed plane coordinates on the ground, and x–y are the fixed coordinates on the vehicle, with x in the vehicle longitudinal direction, and y in the lateral direction. The origin of the system is at the vehicle center of gravity, P. The yaw angle around the vertical axis is taken as positive in the anti-clockwise direction. The vehicle is considered to be moving in plane with some speed. The position vector of point P, with reference to coordinate system X–Y, is defined as R. The velocity vector _R .here, i and j are the respective unit vectors in x and y directions. u and v are the velocity components of point P in the x and y directions. Differentiating Eqn with time, the acceleration could be written as a vector of point P, as below. Here, mean d=dt and d2=dt2:

Fig 23: Coordinate axes for vehicle plane motion.
Fig 24: Time derivative of unit vectors.










Chapter Four

Vehicle Dynamics



4.0 Vehicle Dynamic Characteristics
The basic characteristics of vehicle motion by looking at the vehicle steady-state cornering. The results obtained so far can only be classified as the static characteristics, in other words, the characteristics of the vehicle motion in steady state. To understand the characteristics of vehicle motion in more detail, the dynamic characteristics must be examined as well. Thus, continuing from here, the vehicle’s transient response to steer input will be analyzed from different points of view to further understand the fundamental characteristics of the vehicle motion.

4.1 Motion by Literal Force Exerted on the Center of Gravity
When the vehicle is traveling on a banked road for example, a component of the vehicle weight will act as a lateral force at the center of gravity. This section will look at the vehicle motion when the lateral force, Y, acts at the center of gravity.

4.2 Vehicle motion due to a step change in lateral force
In order to study the vehicle motion due to the lateral force, Y, the vehicle response to an idealized form of lateral force will be looked at. Generally, one ideal form of lateral force in this kind of situation is a step change. Consider the lateral force acting on the center of gravity of a vehicle traveling on a straight line. If this disturbance force acts for a long enough time, even if the Y0 value is small, the vehicle will eventually deviate away from its original path. The vehicle motion in this case is more conveniently expressed with coordinates fixed on the vehicle itself

Fig 25: Lateral force exerted on CG.
4.3 Steady State Condition
For a vehicle with an US characteristic, the traveling condition and force equilibrium during steady state. If the lateral disturbance, Y0; acts on the vehicle, the center of gravity, P, will move and produce a side-slip angle of b > 0: Due to this b; the forces of 2Kfb and 2Krb will be exerted on the front and rear tires. The resultant force of these two forces acts at the NSP. The magnitude of the resultant force is 2ðKf þ KrÞb and it acts in the opposite direction of Y0: If the vehicle exhibits an US characteristic, the NSP is behind the center of gravity, P, and the resultant force produces an anti-clockwise yaw moment around the point P. If the vehicle motion is in steady state, a moment must act to balance this yawing moment. This moment can only be produced by a force acting on the tire, so there must be relative motion in lateral direction, other than b; between the tire and the road surface. Here, the anti-clockwise yaw motion around point P produces side-slip angles of lfr=V and lrr=V on the front and rear tires, respectively. Two forces in an opposite direction to each other with the magnitude of lfKfr=V and lrKrr=V are exerted on the front and rear wheels to balance the yaw moment caused by the disturbance. This is why r in The centrifugal force, mrV; also acts at the center of gravity in a direction opposite to Y0: These forces are in the equilibrium so the vehicle is in steady-state cornering and heading outward from the circular path. The vehicle with NS characteristic has the traveling condition and force equilibrium. If the characteristic is NS, the NSP coincides with point P, and the resultant force of the tire forces, 2ðKf þ KrÞb; acts at the same position as Y0: This resultant force does not produce any moment around the center of gravity and the vehicle has no yawing motion. There is no centrifugal force acting at the center of gravity. This is why r is zero. The resultant force of the tire forces is in equilibrium with the external force, Y0: Consequently, the vehicle continues its transverse motion while producing a side-slip angle.


Fig 26: Steady state of US vehicle.
Fig 27: Steady state of NS vehicle.
The traveling condition and force equilibrium for an OS vehicle. Here, the lateral force Y0 moves the center of gravity to produce a side-slip angle. This side-slip angle generates forces of 2Kfb and 2Krb at the front and rear wheels, and the resultant force acts at the NSP. If the vehicle characteristic is OS, the NSP is in front of P, and the resultant force 2ðKf þ KrÞb produces a clockwise yaw moment around the vehicle center of gravity. In steady state, there must be a moment to balance this yawing moment. This moment is obtained from the front and rear lateral forces, 2Kf lfr=V and 2Krlrr=V; produced by the clockwise yawing motion of the vehicle. This is why r is negative. Then, the centrifugal force, mrV; acts at the center of gravity in the same direction as Y0: When the vehicle exhibits an OS characteristic, the steady-state cornering is in the opposite direction to the case of US and the vehicle heads inwards of the circular path.



Chapter Five

Geometrical Analysis




5.0 Roll Geometry
Eberan’s hypothesis of the roll center as the vehicle’s geometrical instantaneous rotation center and assumption that this roll center is always fixed have long been taken as the standard approach. This hypothesis is generally used due to its simplicity. Based on this hypothesis, the roll mechanism of the 165 vehicle will be studied with a constant lateral acceleration, which is caused by a constant centrifugal force.

5.1.1 Roll Center and Roll Axis
In general, there are various types of suspension systems, from the simple rigid axle type to the independent suspension that is common in passenger cars. The relative vertical displacement or angular displacement between the sprung and unsprung masses is dependant on the structure of the suspension system. The front and rear wheel roll centers are also determined by the suspension system configuration. The line that connects the front and rear roll centers is called the roll axis. The roll center is the vehicle’s instantaneous rotation center in the plane perpendicular to the vehicle’s longitudinal direction, which contains the left and right wheels’ ground contact point. The wheels are considered rigid in both up–down, left–right directions and the ground contact point is fixed. The axle type suspension system. The vehicle body at points A1 and B1 can only have vertical displacement relative to the unsprang mass due to the springs. Even if the sprung mass rolls, the unsprang mass including the wheels is assumed rigid and thus, doesn’t move, the roll center is at point O. In other words, when a rolling moment acts on the vehicle, the vehicle body will produce a roll angle, f; relative to the wheels with respect to the point O.
A typical independent type of suspension – often called the double wishbone suspension. As its name implies, each wheel can move independently, relative to the vehicle body. If the vehicle body is fixed, the instantaneous rotation centers of the left and right unsprung mass relative to the vehicle body are the points O1 and O2, respectively. The point O1 is the intersecting point of the extended lines of A1–A2 and A3–A4, while the point O2 is the intersecting point of the extended lines ofB1–B2 andB3–B4. Here, when the vehicle body rolls during cornering, the wheel contact points with the ground,Aand B, are fixed and the unsprung masses must roll around them. The points O1 and O2 move in the direction perpendicular to O1A and O2B. O1 and O2 are the virtual points on the vehicle body as well as on the unsprung masses. Consequently, the vehicle body instantaneous rotating center, or the roll center is the intersection of the extended  lines of O1A and O2B, which is the point O.

Fig 28: Roll center for rigid axle suspension.

Based on this way of thinking, the roll center for other types of suspension. It is clear that the vehicle roll center position is dependant on the structure of the suspension system. Usually, the suspension system and the vehicle are symmetrical on the left and right, and the roll center is always on the symmetric axis. In this case, it is the height of the roll center that is dependent on the suspension system structure. The roll center is the vehicle instantaneous rotation center, and its position can move during suspension movement. The point O shown here is the roll centerwhen roll angle is zero; if the vehicle rolls, the roll center will also move. If the roll angle is not large, the movement of the roll center is small, and it is possible to assume that the roll centers are fixed at point O. It is still possible to understand the vehicle roll mechanism, even with a moving roll center. But the fixed roll center concept is easier to understand and gives a good understanding of the basic vehicle dynamics. Based on Eberan’s roll center hypothesis, the front and rear roll centers are determined, and if the vehicle body is rigid, the vehicle’s fixed roll axis is determined. The roll center at the front and rear may not have the same height above the ground and the roll axis is not necessarily parallel to the vehicle longitudinal axis. Furthermore, when vehicle motion is accompanied by large roll angles, the fixed roll center and roll axis concepts are not suitable anymore. In such cases, vehicle roll is usually dealt with as the indeterminate problemof the vehicle’s four wheels.

5.1.2 Roll stiffness and load transfer
Now, the vehicle is assumed to have a constant lateral acceleration and centrifugal force acting at the vehicle center of gravity. The center of gravity

Fig 29: Roll axis.

Doesn’t normally coincide with the vehicle roll axis, but is usually above the roll axis. The centrifugal force acting at the center of gravity produces a rolling moment around the roll axis resulting in a constant roll angle. If the vehicle body rolls, the left and right vertical springs of the suspension system will be stretched at one side and be compressed on the other side. This produces an equilibrium moment to the rolling moment due to the centrifugal force. The magnitude of the moment produced by the stretch and the compression of the spring per unit roll angle is called the roll stiffness. Here, the respective roll stiffness for the front and rear suspension systems is defined as Kff ; Kfr; the roll center height from the ground as hf ; hr; the front and rear tread as df ; dr; the distance between the vehicle center of gravity and the roll axis as hs; and the distance between the front and rear axles to the center of gravity as lf ; lr: The weight of the unsprung mass is small compared to the weight of the sprung mass and could be neglected. In this case, the vehicle weight is taken to be equal to the vehicle body weight, and written as Ws: The vehicle lateral acceleration is taken as €y and the centrifugal force acting on the vehicle is €yWs: Assuming that the vehicle is rigid, and the roll angle is small, the rolling moment by the centrifugal force is €yWshs and the roll moment by the vehicle weight due to tilting of the vehicle body is Wshsf; the vehicle roll angle becomesThe centrifugal force, €yWs; acting on the vehicle requires tire cornering forces to achieve equilibrium. Distributing the €yWs force acting at the center of gravity to the front and rear wheels, the forces €yWslr=l and €yWslf=l could be considered to act on the front and rear wheels, respectively, where l ¼ lf þ lr: These forces are equal to the front and rear wheel lateral forces. If the vehicle body rolls, the left and right wheels at both front and rear axles will increase in load at one side and decrease at the other side. This is called the load transfer due to roll. Defining the load transfer for the front and rear as DWf  and DWr; respectively, the roll moment around the roll center at the front and rear wheels in the plane perpendicular to the vehicle longitudinal direction has to be in equilibrium,

5.2 Camber change and roll steer
If the ground contact point of the wheels is fixed, as the vehicle body rolls, the unsprang mass, including the wheels, tilts relative to the ground. This gives the FIGURE 6.7 Transversal load transfer due to body roll.

5.3 Vehicle Body Roll and Vehicle Dynamics
Camber change of the wheel, which is measured relative to the ground and is due to body roll. The vehicle roll also gives the wheels an up-and-down displacement relative to the vehicle body. At such time, depending on the structure of the suspension system, the wheels may produce some angular displacement in the horizontal plane along with the up-and-down movement relative to the vehicle body. This is called the roll steer. The camber change and roll steer are dependent on the structure of the suspension system. The suspension system is designed with keen consideration of these characteristics, often using them to affect the vehicle dynamics or sometimes trying to avoid them completely. This chapter will skip the detailed explanation of camber change and roll steer mechanism for various suspension systems, and only look at the basic characteristics of camber change and roll steer. The collective term for camber change and roll steer is sometimes called the alignment change due to roll. In axle type suspensions, the wheel doesn’t produce any camber change due to vehicle roll. The camber change due to roll only occurs for independent suspension systems, where depending on the suspension structure, there could be one of two cases: camber change in the same direction as roll, which is called positive camber, or in the opposite direction, negative camber.  Independent suspension systems are constructed by a linkage mechanism, and the vehicle roll angle and camber change can be determined from geometrical analysis of the linkage. The actual measured value and calculated value of the camber change for a wishbone type suspension system. This relationship varies substantially with the arrangement of the links, even for suspension systems of the same type. From the figure, if the roll angle is not large, the camber change can be considered as nearly proportional to the roll angle. As the roll angle becomes large, this linear relation is lost, and nonlinearity appears. This is generally for other types of suspension systems. The non-linear characteristic of the camber change is one of the main factors that


Fig 30: Camber change due to body roll.






Chapter Six
Analysis and simulation




6.0 Analysis and simulation:
The dynamic behavior of vehicles can be analysed in several different ways. This can be as straightforward as a simple spring mass system, through a three-degree of freedom (DoF) bicycle model, to a large degree of complexity using a multibody system simulation package such as MSC ADAMS or Modelica. As computers have gotten faster, and software user interfaces have improved, commercial packages such as CarSim have become widely used in industry for rapidly evaluating hundreds of test conditions much faster than real time. Vehicle models are often simulated with advanced controller designs provided as software in the loop (SIL) with controller design software such as Simulink, or with physical hardware in the loop (HIL).
Vehicle motions are largely due to the shear forces generated between the tires and road, and therefore the tire model is an essential part of the math model. The tire model must produce realistic shear forces during braking, acceleration, cornering, and combinations, on a range of surface conditions. Many models are in use. Most are semi-empirical, such as the Pacejka Magic Formula model.
Racing car games or simulators are also a form of vehicle dynamics simulation. In early versions many simplifications were necessary in order to get real-time performance with reasonable graphics. However, improvements in computer speed have combined with interest in realistic physics, leading to driving simulators that are used for vehicle engineering using detailed models such as CarSim.
It is important that the models should agree with real world test results, hence many of the following tests are correlated against results from instrumented test vehicles.



Chapter Seven

Traubel Shooting of Vehicle


Possible causes and remedies of mechanical fuel pump.


1. Fuel pump is unable to supply fuel.

Possible cause
Remedies
1. Petrol tank and middle of the pump will be protected.
1. Remove the protection of fuel line.
2. Diaphragm materials become so hard.
2. Replace the diaphragm.
3. If air is leaking by petrol and middle of the fuel pump.
3. Need to perfect lick in pipe in pipe line.
4. If pump inlet is take off by the ridge.
4. Need to clean pump inlet ridge.


2. If lick the fuel pump.

1. Housing screw is losing.
1. Need to high the housing screw.
2. Diaphragms become prude.
2. Change the diaphragm.
3. Connecting is losing.
3. Need to tighten the connecting.
   4. Fitting thread is disappearing.
   4. Need replace the fitting.


3. Pump is unable to supply sufficient fuel.
1. Connection of fuel line is losing.
  1. Need to tighten the fitting
2. Diaphragm is weak.
  2. Need to replace the diaphragm.
3. Fuel line is break.
  3. Replace the fuel line.
   4. Diaphragm spring is weak.
  4. Need to replace the diaphragm.


4. Fuel pump creates sound.

1. Pump mounting is losing.
1. Need to tighten the mounting.
2. Rocker arm became decay.
2. Need to replace the decky parts.
3. Rocker arm spring is weak
3. Replace the rocker arm spring.


5. Fuel pumps pressure & high volume.
1. If gasoline is enter in the layer of
1. Need to replace diaphragm.
 diaphragm.

2. If diaphragm is very tight to the
2. Replace the diaphragm.
 middle.

3. Flexibility of diaphragm become
3. Replace the diaphragm.
disappear.

4. If rocker arm link become frozen
4. Replace the diaphragm.


with the diaphragm.

5. Diaphragm spring is very hard.
5. Replace the diaphragm.

Struggle / Problem of the electrical fuel pump & servicing possible cause.


1. Pump supplies the un sufficient fuel.

Possible cause
Remedies
1. Carburetor float chamber middle
1. Need to adjust the needle valve.
obstructed by anything.

2. Insufficient of petrol tank venting.
2. Need to sufficient venting.
3. If pump inlet obstructed by anything.
3. Need to vapor the filter.


2. Pump is completely unable to supply the fuel.
1. Electricity is not label in pump.
1. Need to supply electricity in pump.
2. Pump contact point is become decay
2.Ndde to adjusting the contact point or
or adjustment is not is right position.
replacing the contact point.
3. Petrol tank of the middle pipe line is
3. Need to remove the obstruction of pump.
obstruction by anything.



3. Pump is operate but fuel is not sufficient.
1. Leaking air by the contact point of
1. Leak proofs the contact point.
the petrol tank and pipe line.

2. Leaking air by the pump body joint.
2. Need to leak proof joint.
3. Pump valve obstructing by the ridge at
3. Need to clean the pump.
the position of open.



Possible causes and remedies of carburetor main problems.


1. Flooding or leaking the carburetor.

1. Carburetor body become crack.
1. Replace the crack body.
2. If main body or fuel gasket is in
2. Replace the gasket.
trouble.

3. Fuel level or float setting is high.
3. Need to adjust the float level.


2. Idle is not plain.

1. Idle speed is so normal.
1. Need to adjusting idle speed.
2. Idle fuel mixture is not right.
2. Need to adjust idle fuel mixture.


3. Acceleration is weak.

1. Accelerator pump link is not adjusting.
1. Need to adjust accelerator pump link.
2. Check valve of the accelerator is in
2. Need to change the check valve.



4. Engine is in hard starting.

1. Engine create flooding for miss use the
1. Use the right starting process.
right starting process.

2. Fuel level of carburetor is not right.
2. Need to adjusting the fuel level.
3. Adjustment idle is not right.
3. Adjust the low or high speed right.
4. Fuel inlet valve is not adjusting
4. Need to change middle valve.
righting rightly.

5. Fuel pump pressure is not right.
5. Need to repair on change the fuel pump.


5. Stalling engine cold.

1. Mixture of idle fuel is not right.
1. Need to adjusting the idle fuel mixture.
2. Engine idle speed is very slow.
2. Adjusting the first idle.
3. Fuel filter contain ridge, water and ice.
3. Clean the filtering element.
4. Crankcase ventilation is in trouble.
4. Need to repair the trouble parts.
5. Leaking air in fuel line.
5. Need to lighting the fuel line.


6. Engine stalling in heat.

1. Despot is not adjusting in rightly.
1. Adjusting the despot.
2. Idle speed is too slow.
2. Adjust the float speed.
3. Idle fuel mixer is not right.
3. Need to adjusting idle mixture.
4. Head of the idle screw is become
4. Need to replace.
decay.

5. Fuel pump is in trouble.
5. Repaire on charge the fuel pump.


7. Acceleration or in high speed decreasing the power.
1. Accelerating carburetor circuit is in
1. Pump connecting, plunger, valve checking.
trouble.

2. Centrifugal mechanism of distributor
2. Need to check the centrifugal mechanism
is in trouble.
or replace the centrifugal mechanism.
3. High speed circuit of carburetor is in
3. Need to service the carburetor.
 trouble.

4. Air cleaner jam.
4. Clean the air cleaner.
5. Ignition system is in trouble.
5. Need to check the ignition system.


8. Reduced top Speed.

1. Fuel level of carburetor is not in right
1. Adjusting the float level.
 level.

2. Fuel pump pressure or volume is not
2. Need to maintenance the fuel pump.
 right.

3. The size of main jet is narrow.
3. Need to clean the main jet.
Possible causes and remedies of diesel fuel system trouble.


1. Diesel fuel pump is unable to supply the fuel.
Possible cause
Remedies
1. Pump rack jammed.
1. Rack free by the adjusting.
2. Control pawl, control plunger is unable
2. Need to seat the position of troubling
to maintaining.
parts of governor liner and accelerator paddle.


2. Pump is unable to supply sufficient fuel.
1. Calibration of pump is not in right
1. Need to calibrate the pump.
position or inside barrel position of

plunger is not right.

2. Fuel return line is in obstruction.
2. Need to remove the obstruction.
3. Fuel tank bent is closed.
3. Cleaning the fuel tank vent.


3. Control rack jammed.

1. Governor linking, liver and calibrating
1. Necessary to checking the governor
screw is not in right position.
linkage, liver & calibrating area.
2. Rack gear & quadrant pinion are not
2. Need to checking the rack gear and
in right position.
quadrant pinion.


5. Too high injection pressure.

1. Nozzle opening is taken off by carbon.
1. Nee dot clean the nozzle.
2. Nozzle valve is not clean.
2. Need to clean the nozzle.
3. Nozzle valve is in decay.
3. Replace the nozzle valve.


6. Too low injection pressure.

1. Nozzle spring is weak.
1. Change the nozzle spring.
2. Nozzle spring has been broken.
2. Replace the nozzle spring.

Trouble shooting and diagnosis of Vehicle

1. Engine will not turn over.

1. Weak battery.
1. Need to charging the battery or replace the

battery. Engine can be start by the jumper

battery or cable.
2. Open starting circuit.
2. Find the open circuit & remove it.
3. Starting motor drive is jammed.
3. Replace the starting motor.
4. Engine jammed.
4. Check the engine for solving the problem.







Chapter Eight


Conclusion



8.1 Conclusion
For a technical service provider company O&M activities are very important as its service mostly depends on the availability of its equipment & technology. AG Automobiles Ltd is providing Maintenance and Trouble shooting service for vehicle where uninterrupted is the key element to have success over its competitor. To maintain properly it requires doing Maintenance activities very efficiently and with minimum costing.  Using Plant Maintenance schedule can save cost and maximizes profit of CE.
The theme of this report is relatively new in Bangladesh and all over the world.  During this study it has been observed from the organizational point of view where it has been implemented. The use of servicing schedule has shown tremendous potential in developed countries worldwide. There are so many improvement and application that can be offered through these ERP systems which of course would have direct benefit for the organization.

The key findings of the report include:
Ø  To study maintenance activities of vehicle.
Ø  To study the standard process required by AG Automobiles Ltd for the Maintenance activities and incorporation which help to meet the requirement.
Ø  To make an analysis on the Maintenance activities through whole operation Systems 
Ø  To study Troubleshooting of IC engines.
Ø  The Status & Performance of O&M team reflects from the service schedule
Ø  Servicing schedule integrated all the equipment, manpower & other resources of the organization
Ø  All the O&M activities can be properly tracked using service schedule.
Ø  Working in Servicing schedule is user friendly
Ø  Work become systematic & different process has improved the O&M work
Ø  Extra cost for the O&M activities reduces
Ø  Existing Manpower uses the system besides their usual O&M job which increase additional work load with pressure.


8.2 Recommendations

AG Automobiles being one of the largest different vehicle suppliers to the customer’s vehicles in Bangladesh is keep to stay competitive offers to its customers. With the set mission and vision AG automobiles Ltd is committed to keep it up with quality for possible maximum time to serve its customers. As its Quality Policy states, it is eager to adopt new and advanced technologies to provide high and new age service to the customers with satisfaction of its customer.
 In line with these view the following recommendation can be made for Covanta out of the study:
Ø  Automated System to Create Notification in servicing schedule for different Module for O&M works due to fault.
Ø  Automated closing of job when fault rectified.
Ø  Dedicated Team to monitor the activity (updated & escalated) of SAP PM Schedule.
Ø  Taking feedback from Servicing Module for the OT & Man-hour to use for financial purpose.
Ø  It can increase the comfortable of using Servicing schedule.
Ø  Severity of operation and maintenance work can reduce critical and warning type by doing more efficiently servicing work.

8.3 Appendix


m : vehicle mass
I : vehicle yaw moment inertia
l : wheel base
lf : longitudinal position of front wheel(s) from vehicle center of gravity
lr : longitudinal position of rear wheel(s) from vehicle center of gravity
Kf : cornering stiffness of front tire
Kr : cornering stiffness of rear tire
V : vehicle speed
d : front wheel steer angle
b : side slip angle
r : yaw rate
q : yaw angle
x : vehicle longitudinal direction
y : vehicle lateral direction and lateral displacement
t : time
s : Laplace transform variable
8.4 Reference

01.    AG Automobiles Ltd. Abdullahpur, Uttara Dhaka-1230.
02.    Masato Abe A Text Book of Vehicle Handling Dynamics
03.    R.S Khurmi, J.K Gupta a Text Book of Thermal Engineering.
04.    www.madehow.com/Volume-1/Automobile.html
05.    www.google.com
06.    www.wikipedia.com
10.    ttp://www.ag+automobiles&sourceid=chrome&ie=UTF-8&q=ag+automobiles+bangladesh