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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1611
DESIGN OF A COMPACT GO KART VEHICLE
R. Santosh Kumar1, R. Rohith2, S. Srinivas3
1,2,3Department of mechanical engineering, Panimalar Engineering college, Affiliated by Anna university, Chennai-
600123, Tamil nadu, India.
---------------------------------------------------------------------***----------------------------------------------------------------------
Abstract - The design of the go kart is the amalgamation
of the design for chassis, driver ergonomics, cost
effectiveness and safety while avoiding the possibility of over
design. Design software’s along with manual calculations
were utilized. The goal of our project is to design and
fabricate a fully functional Go-Kart vehicle which is suitable
for competitive racing. To achieve this, a bottom up
approach of designing was utilized. Design process began
with the chassis (foundation) and then was built up to the
exterior parts.
Key Words: Go kart, Design, Calculations.
1. INTRODUCTION
We approached our design by considering all the possible
alternatives for the system and modeling them in CAD
software like CATIA, SOLIDWORKS, CREO ect.., and
subjected to analysis using ANSYS software for finite
elemental analysis of the complete go kart vehicle. Based
on the analyses result, the model was modified and
retested and a final design was choosed. Our main
objective is to fabricate a Kart which is comfort for the
driver, to achieve this design and analysis was done for
assumed height and weight of the driver. The position of
various components was optimized based on the driver’s
comfort. The manufacturing approach we used was cost
effective, ergonomics and ease of fabrication.
2. TECHNICAL SPECIFICATIONS OF THE VEHICLE:
2.1 Overall dimensions
2.1.1 Chassis material
o
Material used: AISI 1018
o
Ultimate strength: 440 MPa
o
Yield strength :370 MPa
2.1.2 Chemical composition
2.1.3 Engine
The engine used is Honda stunner, 125 cc
Engine technology Air cooled, 4 stroke,
SI engine
Length*width*Height(approx.) 300 mm* 200mm*250
mm
Bore x stroke 52.4 x 57.838 mm
Displacement (cc) 124.7
Net power output 11BPH@ 8000 rpm
Net torque 11 Nm @ 6500 rpm
Overall Reduction Ratios 1st gear: 31.645
2nd gear: 21.604
3rd gear: 14.577
4tthgear: 12.245
5th gear:10.62
Fuel tank capacity 10 liters
Oil capacity 0.5 L
2.1.5 Wheel Specification:
Tyre
Size
Position Section
width(mm)
Overall
Diameter(mm)
4.5 x
10-5
Front 114.3 254
7.1 x
11-5
Rear 180.34 279.5
2.2 BRAKING SYSTEM
Braking system of our vehicle was designed to achieve
maximum braking efficiency and to provide greater
vehicle safety
2.2.1 Brake pedal
Passenger cars generally use a pedal ratio between 4 to 6.
A pedal ratio of 5:1 was selected.
ELEMENT %COMPOSITION
Carbon 0.14 - 0.20%
Phosphorous
and Sulphur
< 0.050%
Manganese 0.6 - 0.9%
WHEEL BASE 42.5”
REAR TRACK WIDTH 42”
TOTAL WEIGHT 125 Kg
GROUND CLEARANCE 2.5”
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1612
2.2.2 Master cylinder
Analyzing the available ones, we chose the master cylinder
of TVS APACHE RTR 160. The piston diameter of this MC is
19.05 mm.
2.2.3 Caliper and rotor selection
The caliper and the rotor are selected from KTM DUKE
390 with diameter of caliper being 32 mm and effective
radius of rotor being 100 mm.
2.2.4 Brake system specifications
Brake type: Single disc brake
Brake fluid :DOT 4
Brake disc: Diameter - 195 mm
Thickness- 5 mm
Brake pad lining thickness: 4.5 mm
Master cylinder diameter: 19.05 mm
Caliper inside cylinder: 32 mm
Assumptions:
Pedal ratio = 5: 1
Max force applied by the driver on the brake pedal= 400 N
Area of the Master cylinder piston (AMC) = π x (DMC)2 ÷ 4 =
π x (0.01905)2 ÷ 4 =2.85*10^-4 m2
+ Area of the piston in the calipers (ACAL) = π x (DCAL)2 ÷ 4=
π x (0.032)2 ÷ 4= 8.0384*10^-4 m2
Effective rotor radius = 100 mm
Co-efficient of friction between the brake pad and disc,
µB = 0.3 (wet)
= 0.7 (dry)
Brake fluid = DOT-4
Disc diameter = 195 mm
Disc material = Cast Iron
Losses due to compression were neglected.
2.2.5 Brake analysis
Force on the master cylinder (FMC) = max force applied x
pedal ratio = 400 x 5 = 2,000 N
Pressure developed in the system on applying the brakes,
p = FMC ÷ AMC = 2,000 ÷ 2.85*10^-4 = 7.0177*10^6 N/m2
The above pressure is same throughout the system.
Force on the calipers (FCAL) = p x ACAL = 7.0177*10^6 x
8.0384*10^-4 = 5,641.842 N
Force on the rotor / disc (clamping force) = FCAL x 2 =
5,643.842 x 2 = 11,287.637 N
Total Frictional force = clamping force x µB = 11,287.637 x
0.3 = 3,386.306 N(wet)
Total Frictional force = clamping force x µB = 11,287.637 x
0.7 = 7,901.341 N(dry)
2.2.6 Assuming wet surface
Torque on the rotor = Frictional force x Effective rotor
radius = 3,386.306 x 0.1 = 338.6306 1N-m
Deceleration produced = Frictional force ÷ mass of the
kart = 3,386.306 ÷ 190 = 17.8226 m/s2
Stopping distance (from max speed to zero) = (Velocity)2
÷ (2 x deceleration) = (23.92) 2 ÷ (2 x 21.1644) = 13.51 m
2.2.7 Assuming dry surface
Torque on the rotor = Frictional force x Effective rotor
radius = 7,901.341 x 0.1 = 790.13411N-m
Deceleration produced = frictional force ÷ mass of the kart
= 7,901.341 ÷ 190 = 41.38 m/s2
Stopping distance (from max speed to zero) = (Velocity)2
÷ (2 x deceleration) = (12.76) 2 ÷ (2 x 49.38) = 6.88 m
2.2.8 Thermal analysis
Kinetic energy of the vehicle at max speed = mV2 ÷ 2 =
(190 x 23.92 x 23.92) ÷ 2 = 54355.80J
Brake time = Stopping distance ÷ speed = 13.51÷ 23.92 =
0.564 s
Brake power = Kinetic energy ÷ Brake time = 54355.80 ÷
0.564 = 96375.53 W
Rubbing area on one side of the disc=(π÷4) x [(pad outer
diameter) 2 – (Pad inner diameter) 2]
Brake Type Single disc brake
Recommended fluid Dot 4
Brake Disc Diameter-195
Brake pad thickness 4.5mm
Master cylinder
diameter
19.05mm
Caliper inside cylinder 32mm
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1613
= (π÷4) x [(0.195)2 – (0.152) 2]
[Width of the pad = 43 mm]
= 0.01172 m2
Total rubbing area = 0.01172 x 2
= 0.02344 m2
Heat flux (q) = brake power ÷ Total rubbing area
= 96375.53 ÷ 0.02344
= 4111584.12 W/ m2
Rise in temperature of the disc while braking (T) =
= (0.527 x 4111584.126 x √0.306) ÷ √ (7250 x 500 x 58)
….[Cast Iron disc]
T = 112.22’C
Max temperature produced in the disc during hard
braking = 36.51 + 30 (ambient temperature) = 142.2’c
3.1 STEERING SYSTEM
The steering used here is based on Ackermann’s principle
in order to avoid the need for tyres to slip sideways, when
following the path around a curve.
3.1.1 Steering calculations
When a vehicle is cornering, each wheel describes a
turning circle. The outer turning circle, or its radius, is the
main subject of interest. The calculation is not precise
because when a vehicle is cornering the perpendiculars
through the centers of all wheels do not intersect at the
curve centre point (Ackermann condition). In addition,
while the vehicle is moving dynamic forces will arise that
will affect the cornering maneuver. The values stated
below were found out by using the graphical method.
NOTATIONS VALUES
STEERING GEOMETRY Ackermann
WHEEL BASE 1040mm
FRONT TRACK WIDTH 680mm
REAR TRACK WIDTH 1050mm
DISTANCE FROM FRAME TO
WHEEL CENTER (FRONT WHEEL)
340mm
DISTANCE FROM FRAME TO
WHEEL CENTER (REAR WHEEL)
320mm
INNER STEER ANGLE 27degree
OUTER STEER ANGLE 19.32degree
TURN RADIUS 2440.155mm
CASTER 1 degree
TOE IN AND TOE OUT 2 degrees
KING PIN INCLINATION N/A
TIE ROD Equal length of
340mm
STEERING RATIO 1:1
STEERING ARM LENGTH 460mm
STEERING ARM ANGLE 74.22 degree
PERCENTAGE OF ACKERMAN STEERING ACHIEVED:
Let us assume the inner turning angle to be 27 degrees,
(A)
Now, by formula
Tan A = L/(R-D/2)
Where, L- Wheel base
D- Track width
R- Turning radius
Therefore,
Tan27= 1070/(R-680/2)
R=2440.115mm
Similarly
Tan B= L/(R+D/2)
B=18.92 degree
Steering arm angle = 4*A*tan(d/2l)
SAA=73.2degree
Now,
% Ackerman = 6*(A-B)/atan(1/(tanB-1)-B
=87.77%
Therefore, percentage of Ackerman achieved=
87.77percentage
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1614
3.1.2 Target performance of the kart
● STUNNER 125 engine was chosen as it offers the max
power (11 BHP @8000RPM) under the 125CC
segment.
● Direct drive was implemented (no jackshaft) so that
the transmission efficiency ameliorates.
● When a choice was to be made between the two types
of chains (R 1278) for the drive, #R 1278 was chosen
as the load transfer capability of this chain was higher
and also the minimum breaking load is 18200 N. This
gave us a high FOS.
● A small experiment was done to determine the max
force a driver can apply on the brake pedal. The
seating position was simulated and in the place of the
brake pedal, a weight machine was kept. The subject
was able to apply a maximum force of 40 Kgf or 400 N.
● The target stopping distance during hard braking
from max speed (135.6 Kmph) to zero was 6 to 13 m.
To achieve this, a pedal ratio of 5:1 was considered.
The calculated stopping distance was 6.8 m under dry
conditions, which is assumed to be the track
conditions.
● The effective rotor radius of the disc used is 0.1 m.
This offered higher braking torque on the disc and
thus higher braking force on the tires.
● A live rear axle provides better traction when
compared to a dead rear axle. Hence a live rear axle
was used.
4.1 TRANSMISSION SYSTEM
Engine: Honda STUNNER125 cc
Transmission:
Primary reduction = 3.35
Final reduction = 1.41
Secondary reduction:
First gear 3.076: 1
Second gear 1.944: 1
Third gear 1.473: 1
Fourth gear 1.19: 1
Fifth gear 1.038:1
Rear Axle Type: live axle
Wheels: (in inches)
Front = 4.5 x 10-5
Rear = 7.1 x 11-5
Diameter of the rear wheel (D) = 280 mm [circumference
= 398.98 mm]
Gear Ratio (G): 1.41[14 T clutch sprocket and 20 T axle
sprocket]
The calculations have been done for 8000 RPM crankshaft
speed as max power is available only at that speed.
Assumed total weight of the kart:
 Driver = 65 Kg
 Chassis = 15 Kg
 Engine = 30 Kg
 Other stuff = 80 Kg
Total = 190 Kg
Max angular speed of the rear wheel (N):
Gear Reduction ratio Speed of the
Rear wheel
(RPM)
First gear 14.29 514.8
Second gear 9.182 871.62
Third gear 6.95 1151.07
Fourth gear 5.62 1423.48
Fifth gear 4.90 1632.6
Chain: R 1278 OR 08B-1(pitch, p = 12.7 mm)
Since the engine used has a five gear speed variation
system, some of the calculations below are done for each
gear.
4.2 Max Speed of the kart:
V(max)4 = (π x D x N) ÷ 60
= (π x 0.28 x 1632.6)÷ 60
= 23.92m/s
V(max)4= 86.122 Kmph
Similarly, for the other gears,
First gear 7.54 m/s
Second gear 12.77 m/s
Third gear 16.87 m/s
Fourth gear 20.86 m/s
Fifth gear 23.92m/s
4.3 Max Acceleration:
a(max)1 = [g x HP] ÷ [V x weight]
= [9.81 x7673.5]/ [7.54x 190 x 9.81]
a(max)1 = 5.35
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1615
First gear 5.35 m/s2
Second gear 3.162 m/s2
Third gear 2.384m/s2
Fourth gear 1.93 m/s2
Fifth gear 1.688m/s
4.4 Transmission:
Gear ratio = 1.41
Clutch sprocket (Z1) = 14
Axle sprocket (Z2) = 20
Engine torque (T1) = 11 N-m at 6500 RPM
Torque at the axle (T2) = ?
Engine sprocket speed (N1) =2301.96
Axle sprocket speed (N2)=1632.6
First gear 514.8
Second gear 871.62
Third gear 1151.02
Fourth gear 1423.48
Fifth gear 1632.6
4.5 Pitch circle diameter of the sprockets:
Engine sprocket: 14T
D1 = p x cosec (180÷14)
= 12.7 x cosec (12.85)
D1 = 57.07mm
Axle (driven) sprocket: 20T
D2 = p x cosec (180÷20)
= 12.7 x cosec (9)
D2 =81.18mm
D2< D (280 mm) The axle sprocket doesn’t hit the track
during operation.
4.6 Chain Drive Calculations:
R 1278 Chain specs:
Pitch (p) = 12.7 mm
Max Roller diameter (Dr) = 8.51 mm
Min width between the inner plates (W) = 8.00 mm
Max pin body diameter (Dp) = 4.45 mm
Max plate depth (Gpl) = 11.70 mm
Transverse pitch (Pt) = -NIL-
Max overall over joint = 20.5 mm
Bearing area = 0.50 cm2
Weight per metre = 7 N
Min breaking load = 18200 N
4.6.1 Chain velocity:
VC(max) = π x D1 x N1 ÷ 60
= π x 0.069 x 2301.96 ÷ 60
VC(max) = 8.31 m/s
4.6.2 Chain Length:
L=Kxp
K = Constant
K = [(Z1+Z2) ÷ 2] + [(2 x C) ÷ p] + { [(Z2 – Z1) ÷ (2π)]2 x [p
÷ C] }
Z1 = 14
Z2 = 20
P = 12.7
C = 30p – 4 = (30 x 12.7) – 4 = 377 mm
…C = minimum distance between sprocket centers.
K = [(14 + 20) ÷ 2] + [(2 x 377) ÷ 12.7] + {[(20 – 14) ÷
(2π)]2 x [12.7 ÷ 377]}
K = 76.40
L = K x p = 76.37 x 12.7 = 970.28 mm
L ≈ 970 mm
4.6.3 Factor of Safety of the chain drive:
FOS =
= WB ÷ W ……A
For R1278 , WB = 18200 N
First gear 726.27 RPM
Second gear 1288.9 RPM
Third gear 1623.0 RPM
Fourth gear 2007.106 RPM
Fifth gear 2301.96 RPM
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1616
W = Tangential force (FT) + Centrifugal force (FC) +
Sagging tension (FS) ……B
FT =
=
= 1096.21 N
FC = m x v 2 = 0.7 x (8.31)2 = 48.33N
FS = k x m x g x C ….. [k = constant = 3, C =
minimum centre distance between sprockets = 0.377 m]
= 3 x 0.7 x 9.81 x 0.377
= 7.849 N
B W = 1096.21+ 48.33 + 7.849
W = 1152.38N
A FOS =
= 15.79
4.7 Transmission efficiency:
Efficiency = 1 – (power lost ÷ input power)
Input power = 7673.5 W
Power lost = (Drag force + Rolling resistance) x Velocity
Drag force (Fd) = Cd x A x V2 x density of air ÷ 2
[A = Frontal area] = 0.7 x 0.57 x (23.92)2 x 1.16 ÷ 2
Fd = 132.41 N
Rolling resistance (Rr) = µ x W x number of wheels
= (0.03) x (190 x 9.81) x 4
[for Asphalt, µ = 0.03]
Rr= 223.668 N
Power lost =(132.41+223.68) x 14.07 = 5010 W
Efficiency = 1 –(5010÷ 7673.5)
= 0.3471 = 34.71%
4.8 Wheel torque
Tw = Overall Gear ratio x transmission efficiency x engine
torque
= Overall gear ratio x 0.3471 x 11
Gear
Overall gear
ratio
Wheel
torque (N-m)
First gear 15.54 59.33
Second gear 9.18 35.05
Third gear 6.95 26.535
Fourth gear 5.62 21.45
Fifth gear 4.90 18.70
4.9 Tractive effort:
TE = Tw ÷ (Radius of the rear wheel, R)
First gear 423.78 N
Second gear 250.35 N
Third gear 189.53 N
Fourth gear 153.21N
Fifth gear 133.57 N
Checking the above obtained values…
Max tractive effort that can be applied = TEmax = µt x
(Weight of the kart, W) …For Asphalt, µt = 0.7
TEmax = 0.7 x (160 x 9.81) = 1304.73 N
Since the tractive effort produced in 1st, 2nd, 3rd and 4th,
5th gears is lesser than the max applicable tractive effort,
slip won't occur. There is a LESS chance for wheel slip.
4.10 Gradability:
Tractive effort = W x sin θ
W = m x g = (160 x 9.81) = 1570 N
First gear 13.12 deg
Second gear 7.718 deg
Third gear 5.831 deg
Fourth gear 4.703 deg
Fifth gear 4.105 deg
5. 3D VIEWS OF THE KART
ISOMETRIC VIEW:
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072
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FRONT VIEW:
SIDE VIEW:
REARVIEW:
5.1Calculation of center of gravity using CATIA
The center of gravity is somewhat in the engine side and
between the seat and engine.
5.2 DESIGN PROCESS :( design methodology)
● A hollow rod was chosen instead of solid rod for
the purpose of cost reduction and better power to
weight ratio. Hence the outer and inner diameter
of the rod is 26 mm and 20 mm.
● The priority was given to design a stable structure
with an aerodynamic arrangement in the front
part of the chassis.
● A non-symmetric rear end was designed to
facilitate the engine support, driver comfort and
also provide a slight rear lift during turns.
● Cross bars were used to provide uniform stress
distribution under running conditions.
● Chassis was designed with only x-axis and y-axis.
The usage of z-axis was avoided to prevent
complications and to simplify the analysis
process.
5.3 ERGONOMICS
Driver ergonomics played a major role in designing of our
vehicle chassis. The cockpit has been designed to allow
considerable comfort of the driver. Large leg space and
enough room for movement inside the cockpit are some
salient points.
The approach adopted for driver ergonomics was to
question our driver on his requirements and using him as
our base for measurements, calculation and designing of
our chassis. The output has been successful design of
cockpit that is safe and comfortable with driver in. The
chassis has been designed to enhance the driver’s
visibility.
All the essential controls in vehicle have been placed such
a way that it can be accessed with ease. The accelerator,
brake pedals are positioned such that the driver shall
stretch his legs for a long time without any stress.
We have placed the kill switch near the centre of the
vehicle for easy accessand the other one in the side of the
seat.
• Wide and spacious cockpit.
• Egress time: 5 seconds.
• All controls within the reach envelop of the driver’s
hand.
• The seat has been designed to withstand any kind of
sudden motion.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1618
5.4 DIFFERENT VIEWS OF THE CHASSIS:
A. : TOP VIEW:
B. ISOMETRIC VIEW:
C. PROTOTYPE:
FLOOR PLANNING:
5.5 PROPERTIES OF MATERIAL AISI 1018:
CHEMICAL COMPOSITION
 Carbon - 0.20% (max)
 Phosphorous, sulphur - 0.050% (max)
 Manganese – 0.6-0.9%
MECHANICAL PROPERTIES

Ultimate strength : 440 MPa

Yield strength : 370 MPa

The material has good weldability, machinability
and cost effective.
5.6 WEIGHT CALCULATION OF CHASSIS:
Total length of the rods used in design=6 m
Density of the chassis material = 7.87gm/cm3
Outer diameter of the rod = 26 mm
Inner diameter of the rod = 20 mm
Volume of the rod = [π/4] x [((26 x 10-3)2
- (20 x10-3)2) x 6]
Volume of the rod = 1.3 x 10-3 m3
Weight of the chassis =1.3 x 10-3 x 7.87 x1000
Weight of the chassis =10.23 Kg (11kg approx.)
6. CHASSIS ANALYSIS
This analysis was done in order to check the safety of the
chassis design. It was completed by conducting dynamic,
static, torsional and modal analysis over the chassis.
Deceleration after the impact was assumed to be zero
during Impact tests. Driver safety was ensured even at the
worst case. The following tests were conducted
● Front impact
● Rear impact
● Side impact
● Static analysis
● Modal analysis
● Torsional analysis
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1619
6.1 DYNAMIC ANALYSIS
6.1.1 FRONT IMPACT
The first analysis to be completed was that of a front
collision with a stationary object. In this case a
deceleration of 10836 N was the assumed loading.For the
front impact test, the front nodes are applied with the load
calculated. The rear is completely constrained allowing
displacement to occur only in direction of the load applied.
The maximum stress after front impact was 200Mpa. But
the yield stress of the material is 370 Mpa. So, our design
proved to be safe.
The factor of safety calculated from the front impact is
1.8499
6.1.2 REAR IMPACT
Next rear impact analysis was done while assuming
7225.1N as the impact force.
It is same as the front impact but the rear portion was
constrained. The maximum stress after rear impact was
178.99Mpa. But the yield stress of the material is 370Mpa.
So, our design proved to be safe.
The factor of safety for the given load is calculated as 2.03
The total deformation for the given load is 2.365
6.1.3 SIDE IMPACT
The next step in the analysis was to analyse a side impact
with a 7225.1N load.
As a side impact is most likely to occur with the vehicle
being hit by another kart vehicle it was assumed that
neither vehicle would be a fixed object. The maximum
stress after side impact was 342.19Mpa. But the yield
stress of the material is 370MPa
The factor of safety is calculated as 1.08 for the given load
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1620
6.2 STATIC ANALYSIS
Total load acted=95+30=125kg=125*9.81=1226.25 N
Where, weight of the driver assumed as 95 kg at the max
conditions and the weight of the engine is assumed as 30
kg.
The weight is assumed to be acted on the specific regions
such as the driver seating and the engine mounting.
Both the deformation and the stress analysis are done for
static analysis.
The weights of the other sub systems are negligible
compared to driver’s weight and the weight of the engine.
The maximum displacement during static analysis is
1.142. and fos=5.7
6.3 MODAL / VIBRATION ANALYSIS:
Next for the vibrational analysis, the vibrational frequency
applied to the frame is assumed to be is 133.3HZ
calculated for 8000 rpm engine(stunner).
The maximum displacement during vibrational analysis is
51.5mm
6.4 TORSION ANALYSIS
In torsional analysis, among four wheels three wheels are
fixed and a bumping load is acted on one wheel.
The load acted on the single wheel =9.81(chassis weight+
driver weight+ engine weight)
9.81*(30+70+15)=1275.3 N
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
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The maximum deflection of the chassis during torsional
analysis is 3.219mm.
FOS=3.4
6.5 STATIC ANALYSIS OF SPROCKET
Here the inside is kept fixed. The moment of 157.29N-m
at first gear engagement is applied to the teeth that
meshes with the chain.
A maximum deformation of 0.0068mm is obtained.
A maximum stress of 45.812MPa is obtained.
A factor of safety of 5.45 is obtained when the load is
157.29N-m (first gear is engaged)
6.6 STATIC ANALYSIS OF STUB AXLE
Here the axle part is fixed and the part attached to the
wheel is given a load about 15 kN . here this load is due to
the wobling of tires.we get quite a small amount of
deformation of about 2.5*10^3mm in the left axle.
6.7 AXLE ANALYSIS:
In the axle analysis,the live axle of the kart is mounted to
the rear wheels. The loads and moment acting on the
axle’s end and sprocket is calculated and the results are
obtained. The moment acting on the sprocket is calculated
as 157.5N-m ( Torque transferred when first gear is
engaged ). Also the load of the kart is evenly distributed to
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1622
each wheel hub positions and its calculated as 520N on
each wheels.
The deformation is calculated as 0.063021mm.
The maximum deformation is calculated as 74.59MPa
The factor of saftey is calculated as 4.905.
6.8 BRAKE PEDAL ANALYSIS:
In the brake pedal analysis,The force given by the driver to
the brake pedal is calculated and applied on the brake pad.
By the standards the pedal force is about 400N.Its
recommended that no more than this force is required to
stop a passengers car.since a pressure of 200N applied
othe brake and the result is observed.
A deformation of 0.4404mm maximum is obtained.
A maximum stress of 66.17MPa is obtained.
A maximum factor of saftery of 5.5 is obtained for a load of
400N.
ACKNOWLEDGEMENT
The design process is not a single-handed effort and it is
our team, whom we wanted to thank for standing with us
under all circumstances. We would also like to express our
gratitude towards the Mechanical department and on the
whole towards the college for their support and also
BFKCT for providing such a wonderful opportunity to
learn and grow.
Special thanks to our Head of the Department Dr.
L.Karthikeyan and to the team mentor
Mr.S.Dhanasekhar for their guidance and support.
7. CONCLUSIONS
The finite element analysis method is used to evaluate the
system and create and modify the best vehicle design to
achieve its goal. The main goal was to simplify the overall
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1623
design to make it more light weight without sacrificing
performance and durability also make the driver
comfortable. The result is lighter, faster and more angle
vehicle that improves go kart design.
REFERENCES
 Fundamentals of vehicle dynamics by Thomas D.
Gillespe.
 Theory of machines by R.S. Khurmi
 A textbook of machine design- R.S.Khurmi and
J.K.Gupta
 www.asos1.com
 www.DIYgokart.com
 www.Pirate 4x4.com
 International Journal of Engineering Applied
Sciences and Technology, 2016 Vol. 1, Issue ISSN
No. 2455-2143
 International Journal of Scientific & Engineering
Research, Volume 7, Issue 4, April-2016 429 ISSN
2229-5518 IJSER © 2016 http://www.ijser.org
DESIGN, ANALYSIS AND FABRICATION OF GO-
KART Kiral Lal, Abhishek
 International Journal of Science, Engineering and
Technology Research (IJSETR) Volume 6, Issue 3,
March 2017, ISSN: 2278 -7798 448 All Rights
Reserved © 2017 IJSETR DESIGN OF A GO KART
VEHICLE
 Milliken & Milliken, “Race Car Vehicle Dynamics”
 Reza M. jazar, “Vehicle Dynamics Theory and
Applications(BBS)”
 Asfan Mohiuddin, Mohd Sayeed, Md Nawaz
“Steering System of Electric Go-Kart”
International Journal for Research in Applied
Science & Engineering Technology (IJRASET)
Volume 5 Issue I, January 2017, IC Value: 45.98
ISSN: 2321-9653,Page 453-456.
 .Govardhana Reddy, Md. Hameed, “design report
of a go kart vehicle”, International Journal of
Engineering Applied Sciences and Technology,
2016,Vol. 1, Issue 9, ISSN No. 2455-2143 , Pages
95- 102, Published Online July – August 2016
 Dr.D.Ravikanth,Dr.K.Rajagopal,Dr.V.S.S. Murty, A.
Harikrishna, “design of a go kart vehicle”,
International Journal of Science, Engineering and
Technology Research (IJSETR) Volume 6, Issue 3,
March 2017, ISSN: 2278 -7798 ,Page 448-456.
BIOGRAPHIES:
R. Santosh kumar
Department of Mechanical
Engineering.
R. Rohith
Department of Mechanical
Engineering.
S. Srinivas
Department of Mechanical
Engineering.

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IRJET- Design of a Compact Go Kart Vehicle

  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1611 DESIGN OF A COMPACT GO KART VEHICLE R. Santosh Kumar1, R. Rohith2, S. Srinivas3 1,2,3Department of mechanical engineering, Panimalar Engineering college, Affiliated by Anna university, Chennai- 600123, Tamil nadu, India. ---------------------------------------------------------------------***---------------------------------------------------------------------- Abstract - The design of the go kart is the amalgamation of the design for chassis, driver ergonomics, cost effectiveness and safety while avoiding the possibility of over design. Design software’s along with manual calculations were utilized. The goal of our project is to design and fabricate a fully functional Go-Kart vehicle which is suitable for competitive racing. To achieve this, a bottom up approach of designing was utilized. Design process began with the chassis (foundation) and then was built up to the exterior parts. Key Words: Go kart, Design, Calculations. 1. INTRODUCTION We approached our design by considering all the possible alternatives for the system and modeling them in CAD software like CATIA, SOLIDWORKS, CREO ect.., and subjected to analysis using ANSYS software for finite elemental analysis of the complete go kart vehicle. Based on the analyses result, the model was modified and retested and a final design was choosed. Our main objective is to fabricate a Kart which is comfort for the driver, to achieve this design and analysis was done for assumed height and weight of the driver. The position of various components was optimized based on the driver’s comfort. The manufacturing approach we used was cost effective, ergonomics and ease of fabrication. 2. TECHNICAL SPECIFICATIONS OF THE VEHICLE: 2.1 Overall dimensions 2.1.1 Chassis material o Material used: AISI 1018 o Ultimate strength: 440 MPa o Yield strength :370 MPa 2.1.2 Chemical composition 2.1.3 Engine The engine used is Honda stunner, 125 cc Engine technology Air cooled, 4 stroke, SI engine Length*width*Height(approx.) 300 mm* 200mm*250 mm Bore x stroke 52.4 x 57.838 mm Displacement (cc) 124.7 Net power output 11BPH@ 8000 rpm Net torque 11 Nm @ 6500 rpm Overall Reduction Ratios 1st gear: 31.645 2nd gear: 21.604 3rd gear: 14.577 4tthgear: 12.245 5th gear:10.62 Fuel tank capacity 10 liters Oil capacity 0.5 L 2.1.5 Wheel Specification: Tyre Size Position Section width(mm) Overall Diameter(mm) 4.5 x 10-5 Front 114.3 254 7.1 x 11-5 Rear 180.34 279.5 2.2 BRAKING SYSTEM Braking system of our vehicle was designed to achieve maximum braking efficiency and to provide greater vehicle safety 2.2.1 Brake pedal Passenger cars generally use a pedal ratio between 4 to 6. A pedal ratio of 5:1 was selected. ELEMENT %COMPOSITION Carbon 0.14 - 0.20% Phosphorous and Sulphur < 0.050% Manganese 0.6 - 0.9% WHEEL BASE 42.5” REAR TRACK WIDTH 42” TOTAL WEIGHT 125 Kg GROUND CLEARANCE 2.5”
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1612 2.2.2 Master cylinder Analyzing the available ones, we chose the master cylinder of TVS APACHE RTR 160. The piston diameter of this MC is 19.05 mm. 2.2.3 Caliper and rotor selection The caliper and the rotor are selected from KTM DUKE 390 with diameter of caliper being 32 mm and effective radius of rotor being 100 mm. 2.2.4 Brake system specifications Brake type: Single disc brake Brake fluid :DOT 4 Brake disc: Diameter - 195 mm Thickness- 5 mm Brake pad lining thickness: 4.5 mm Master cylinder diameter: 19.05 mm Caliper inside cylinder: 32 mm Assumptions: Pedal ratio = 5: 1 Max force applied by the driver on the brake pedal= 400 N Area of the Master cylinder piston (AMC) = π x (DMC)2 ÷ 4 = π x (0.01905)2 ÷ 4 =2.85*10^-4 m2 + Area of the piston in the calipers (ACAL) = π x (DCAL)2 ÷ 4= π x (0.032)2 ÷ 4= 8.0384*10^-4 m2 Effective rotor radius = 100 mm Co-efficient of friction between the brake pad and disc, µB = 0.3 (wet) = 0.7 (dry) Brake fluid = DOT-4 Disc diameter = 195 mm Disc material = Cast Iron Losses due to compression were neglected. 2.2.5 Brake analysis Force on the master cylinder (FMC) = max force applied x pedal ratio = 400 x 5 = 2,000 N Pressure developed in the system on applying the brakes, p = FMC ÷ AMC = 2,000 ÷ 2.85*10^-4 = 7.0177*10^6 N/m2 The above pressure is same throughout the system. Force on the calipers (FCAL) = p x ACAL = 7.0177*10^6 x 8.0384*10^-4 = 5,641.842 N Force on the rotor / disc (clamping force) = FCAL x 2 = 5,643.842 x 2 = 11,287.637 N Total Frictional force = clamping force x µB = 11,287.637 x 0.3 = 3,386.306 N(wet) Total Frictional force = clamping force x µB = 11,287.637 x 0.7 = 7,901.341 N(dry) 2.2.6 Assuming wet surface Torque on the rotor = Frictional force x Effective rotor radius = 3,386.306 x 0.1 = 338.6306 1N-m Deceleration produced = Frictional force ÷ mass of the kart = 3,386.306 ÷ 190 = 17.8226 m/s2 Stopping distance (from max speed to zero) = (Velocity)2 ÷ (2 x deceleration) = (23.92) 2 ÷ (2 x 21.1644) = 13.51 m 2.2.7 Assuming dry surface Torque on the rotor = Frictional force x Effective rotor radius = 7,901.341 x 0.1 = 790.13411N-m Deceleration produced = frictional force ÷ mass of the kart = 7,901.341 ÷ 190 = 41.38 m/s2 Stopping distance (from max speed to zero) = (Velocity)2 ÷ (2 x deceleration) = (12.76) 2 ÷ (2 x 49.38) = 6.88 m 2.2.8 Thermal analysis Kinetic energy of the vehicle at max speed = mV2 ÷ 2 = (190 x 23.92 x 23.92) ÷ 2 = 54355.80J Brake time = Stopping distance ÷ speed = 13.51÷ 23.92 = 0.564 s Brake power = Kinetic energy ÷ Brake time = 54355.80 ÷ 0.564 = 96375.53 W Rubbing area on one side of the disc=(π÷4) x [(pad outer diameter) 2 – (Pad inner diameter) 2] Brake Type Single disc brake Recommended fluid Dot 4 Brake Disc Diameter-195 Brake pad thickness 4.5mm Master cylinder diameter 19.05mm Caliper inside cylinder 32mm
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1613 = (π÷4) x [(0.195)2 – (0.152) 2] [Width of the pad = 43 mm] = 0.01172 m2 Total rubbing area = 0.01172 x 2 = 0.02344 m2 Heat flux (q) = brake power ÷ Total rubbing area = 96375.53 ÷ 0.02344 = 4111584.12 W/ m2 Rise in temperature of the disc while braking (T) = = (0.527 x 4111584.126 x √0.306) ÷ √ (7250 x 500 x 58) ….[Cast Iron disc] T = 112.22’C Max temperature produced in the disc during hard braking = 36.51 + 30 (ambient temperature) = 142.2’c 3.1 STEERING SYSTEM The steering used here is based on Ackermann’s principle in order to avoid the need for tyres to slip sideways, when following the path around a curve. 3.1.1 Steering calculations When a vehicle is cornering, each wheel describes a turning circle. The outer turning circle, or its radius, is the main subject of interest. The calculation is not precise because when a vehicle is cornering the perpendiculars through the centers of all wheels do not intersect at the curve centre point (Ackermann condition). In addition, while the vehicle is moving dynamic forces will arise that will affect the cornering maneuver. The values stated below were found out by using the graphical method. NOTATIONS VALUES STEERING GEOMETRY Ackermann WHEEL BASE 1040mm FRONT TRACK WIDTH 680mm REAR TRACK WIDTH 1050mm DISTANCE FROM FRAME TO WHEEL CENTER (FRONT WHEEL) 340mm DISTANCE FROM FRAME TO WHEEL CENTER (REAR WHEEL) 320mm INNER STEER ANGLE 27degree OUTER STEER ANGLE 19.32degree TURN RADIUS 2440.155mm CASTER 1 degree TOE IN AND TOE OUT 2 degrees KING PIN INCLINATION N/A TIE ROD Equal length of 340mm STEERING RATIO 1:1 STEERING ARM LENGTH 460mm STEERING ARM ANGLE 74.22 degree PERCENTAGE OF ACKERMAN STEERING ACHIEVED: Let us assume the inner turning angle to be 27 degrees, (A) Now, by formula Tan A = L/(R-D/2) Where, L- Wheel base D- Track width R- Turning radius Therefore, Tan27= 1070/(R-680/2) R=2440.115mm Similarly Tan B= L/(R+D/2) B=18.92 degree Steering arm angle = 4*A*tan(d/2l) SAA=73.2degree Now, % Ackerman = 6*(A-B)/atan(1/(tanB-1)-B =87.77% Therefore, percentage of Ackerman achieved= 87.77percentage
  • 4. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1614 3.1.2 Target performance of the kart ● STUNNER 125 engine was chosen as it offers the max power (11 BHP @8000RPM) under the 125CC segment. ● Direct drive was implemented (no jackshaft) so that the transmission efficiency ameliorates. ● When a choice was to be made between the two types of chains (R 1278) for the drive, #R 1278 was chosen as the load transfer capability of this chain was higher and also the minimum breaking load is 18200 N. This gave us a high FOS. ● A small experiment was done to determine the max force a driver can apply on the brake pedal. The seating position was simulated and in the place of the brake pedal, a weight machine was kept. The subject was able to apply a maximum force of 40 Kgf or 400 N. ● The target stopping distance during hard braking from max speed (135.6 Kmph) to zero was 6 to 13 m. To achieve this, a pedal ratio of 5:1 was considered. The calculated stopping distance was 6.8 m under dry conditions, which is assumed to be the track conditions. ● The effective rotor radius of the disc used is 0.1 m. This offered higher braking torque on the disc and thus higher braking force on the tires. ● A live rear axle provides better traction when compared to a dead rear axle. Hence a live rear axle was used. 4.1 TRANSMISSION SYSTEM Engine: Honda STUNNER125 cc Transmission: Primary reduction = 3.35 Final reduction = 1.41 Secondary reduction: First gear 3.076: 1 Second gear 1.944: 1 Third gear 1.473: 1 Fourth gear 1.19: 1 Fifth gear 1.038:1 Rear Axle Type: live axle Wheels: (in inches) Front = 4.5 x 10-5 Rear = 7.1 x 11-5 Diameter of the rear wheel (D) = 280 mm [circumference = 398.98 mm] Gear Ratio (G): 1.41[14 T clutch sprocket and 20 T axle sprocket] The calculations have been done for 8000 RPM crankshaft speed as max power is available only at that speed. Assumed total weight of the kart:  Driver = 65 Kg  Chassis = 15 Kg  Engine = 30 Kg  Other stuff = 80 Kg Total = 190 Kg Max angular speed of the rear wheel (N): Gear Reduction ratio Speed of the Rear wheel (RPM) First gear 14.29 514.8 Second gear 9.182 871.62 Third gear 6.95 1151.07 Fourth gear 5.62 1423.48 Fifth gear 4.90 1632.6 Chain: R 1278 OR 08B-1(pitch, p = 12.7 mm) Since the engine used has a five gear speed variation system, some of the calculations below are done for each gear. 4.2 Max Speed of the kart: V(max)4 = (π x D x N) ÷ 60 = (π x 0.28 x 1632.6)÷ 60 = 23.92m/s V(max)4= 86.122 Kmph Similarly, for the other gears, First gear 7.54 m/s Second gear 12.77 m/s Third gear 16.87 m/s Fourth gear 20.86 m/s Fifth gear 23.92m/s 4.3 Max Acceleration: a(max)1 = [g x HP] ÷ [V x weight] = [9.81 x7673.5]/ [7.54x 190 x 9.81] a(max)1 = 5.35
  • 5. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1615 First gear 5.35 m/s2 Second gear 3.162 m/s2 Third gear 2.384m/s2 Fourth gear 1.93 m/s2 Fifth gear 1.688m/s 4.4 Transmission: Gear ratio = 1.41 Clutch sprocket (Z1) = 14 Axle sprocket (Z2) = 20 Engine torque (T1) = 11 N-m at 6500 RPM Torque at the axle (T2) = ? Engine sprocket speed (N1) =2301.96 Axle sprocket speed (N2)=1632.6 First gear 514.8 Second gear 871.62 Third gear 1151.02 Fourth gear 1423.48 Fifth gear 1632.6 4.5 Pitch circle diameter of the sprockets: Engine sprocket: 14T D1 = p x cosec (180÷14) = 12.7 x cosec (12.85) D1 = 57.07mm Axle (driven) sprocket: 20T D2 = p x cosec (180÷20) = 12.7 x cosec (9) D2 =81.18mm D2< D (280 mm) The axle sprocket doesn’t hit the track during operation. 4.6 Chain Drive Calculations: R 1278 Chain specs: Pitch (p) = 12.7 mm Max Roller diameter (Dr) = 8.51 mm Min width between the inner plates (W) = 8.00 mm Max pin body diameter (Dp) = 4.45 mm Max plate depth (Gpl) = 11.70 mm Transverse pitch (Pt) = -NIL- Max overall over joint = 20.5 mm Bearing area = 0.50 cm2 Weight per metre = 7 N Min breaking load = 18200 N 4.6.1 Chain velocity: VC(max) = π x D1 x N1 ÷ 60 = π x 0.069 x 2301.96 ÷ 60 VC(max) = 8.31 m/s 4.6.2 Chain Length: L=Kxp K = Constant K = [(Z1+Z2) ÷ 2] + [(2 x C) ÷ p] + { [(Z2 – Z1) ÷ (2π)]2 x [p ÷ C] } Z1 = 14 Z2 = 20 P = 12.7 C = 30p – 4 = (30 x 12.7) – 4 = 377 mm …C = minimum distance between sprocket centers. K = [(14 + 20) ÷ 2] + [(2 x 377) ÷ 12.7] + {[(20 – 14) ÷ (2π)]2 x [12.7 ÷ 377]} K = 76.40 L = K x p = 76.37 x 12.7 = 970.28 mm L ≈ 970 mm 4.6.3 Factor of Safety of the chain drive: FOS = = WB ÷ W ……A For R1278 , WB = 18200 N First gear 726.27 RPM Second gear 1288.9 RPM Third gear 1623.0 RPM Fourth gear 2007.106 RPM Fifth gear 2301.96 RPM
  • 6. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1616 W = Tangential force (FT) + Centrifugal force (FC) + Sagging tension (FS) ……B FT = = = 1096.21 N FC = m x v 2 = 0.7 x (8.31)2 = 48.33N FS = k x m x g x C ….. [k = constant = 3, C = minimum centre distance between sprockets = 0.377 m] = 3 x 0.7 x 9.81 x 0.377 = 7.849 N B W = 1096.21+ 48.33 + 7.849 W = 1152.38N A FOS = = 15.79 4.7 Transmission efficiency: Efficiency = 1 – (power lost ÷ input power) Input power = 7673.5 W Power lost = (Drag force + Rolling resistance) x Velocity Drag force (Fd) = Cd x A x V2 x density of air ÷ 2 [A = Frontal area] = 0.7 x 0.57 x (23.92)2 x 1.16 ÷ 2 Fd = 132.41 N Rolling resistance (Rr) = µ x W x number of wheels = (0.03) x (190 x 9.81) x 4 [for Asphalt, µ = 0.03] Rr= 223.668 N Power lost =(132.41+223.68) x 14.07 = 5010 W Efficiency = 1 –(5010÷ 7673.5) = 0.3471 = 34.71% 4.8 Wheel torque Tw = Overall Gear ratio x transmission efficiency x engine torque = Overall gear ratio x 0.3471 x 11 Gear Overall gear ratio Wheel torque (N-m) First gear 15.54 59.33 Second gear 9.18 35.05 Third gear 6.95 26.535 Fourth gear 5.62 21.45 Fifth gear 4.90 18.70 4.9 Tractive effort: TE = Tw ÷ (Radius of the rear wheel, R) First gear 423.78 N Second gear 250.35 N Third gear 189.53 N Fourth gear 153.21N Fifth gear 133.57 N Checking the above obtained values… Max tractive effort that can be applied = TEmax = µt x (Weight of the kart, W) …For Asphalt, µt = 0.7 TEmax = 0.7 x (160 x 9.81) = 1304.73 N Since the tractive effort produced in 1st, 2nd, 3rd and 4th, 5th gears is lesser than the max applicable tractive effort, slip won't occur. There is a LESS chance for wheel slip. 4.10 Gradability: Tractive effort = W x sin θ W = m x g = (160 x 9.81) = 1570 N First gear 13.12 deg Second gear 7.718 deg Third gear 5.831 deg Fourth gear 4.703 deg Fifth gear 4.105 deg 5. 3D VIEWS OF THE KART ISOMETRIC VIEW:
  • 7. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1617 FRONT VIEW: SIDE VIEW: REARVIEW: 5.1Calculation of center of gravity using CATIA The center of gravity is somewhat in the engine side and between the seat and engine. 5.2 DESIGN PROCESS :( design methodology) ● A hollow rod was chosen instead of solid rod for the purpose of cost reduction and better power to weight ratio. Hence the outer and inner diameter of the rod is 26 mm and 20 mm. ● The priority was given to design a stable structure with an aerodynamic arrangement in the front part of the chassis. ● A non-symmetric rear end was designed to facilitate the engine support, driver comfort and also provide a slight rear lift during turns. ● Cross bars were used to provide uniform stress distribution under running conditions. ● Chassis was designed with only x-axis and y-axis. The usage of z-axis was avoided to prevent complications and to simplify the analysis process. 5.3 ERGONOMICS Driver ergonomics played a major role in designing of our vehicle chassis. The cockpit has been designed to allow considerable comfort of the driver. Large leg space and enough room for movement inside the cockpit are some salient points. The approach adopted for driver ergonomics was to question our driver on his requirements and using him as our base for measurements, calculation and designing of our chassis. The output has been successful design of cockpit that is safe and comfortable with driver in. The chassis has been designed to enhance the driver’s visibility. All the essential controls in vehicle have been placed such a way that it can be accessed with ease. The accelerator, brake pedals are positioned such that the driver shall stretch his legs for a long time without any stress. We have placed the kill switch near the centre of the vehicle for easy accessand the other one in the side of the seat. • Wide and spacious cockpit. • Egress time: 5 seconds. • All controls within the reach envelop of the driver’s hand. • The seat has been designed to withstand any kind of sudden motion.
  • 8. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1618 5.4 DIFFERENT VIEWS OF THE CHASSIS: A. : TOP VIEW: B. ISOMETRIC VIEW: C. PROTOTYPE: FLOOR PLANNING: 5.5 PROPERTIES OF MATERIAL AISI 1018: CHEMICAL COMPOSITION  Carbon - 0.20% (max)  Phosphorous, sulphur - 0.050% (max)  Manganese – 0.6-0.9% MECHANICAL PROPERTIES  Ultimate strength : 440 MPa  Yield strength : 370 MPa  The material has good weldability, machinability and cost effective. 5.6 WEIGHT CALCULATION OF CHASSIS: Total length of the rods used in design=6 m Density of the chassis material = 7.87gm/cm3 Outer diameter of the rod = 26 mm Inner diameter of the rod = 20 mm Volume of the rod = [π/4] x [((26 x 10-3)2 - (20 x10-3)2) x 6] Volume of the rod = 1.3 x 10-3 m3 Weight of the chassis =1.3 x 10-3 x 7.87 x1000 Weight of the chassis =10.23 Kg (11kg approx.) 6. CHASSIS ANALYSIS This analysis was done in order to check the safety of the chassis design. It was completed by conducting dynamic, static, torsional and modal analysis over the chassis. Deceleration after the impact was assumed to be zero during Impact tests. Driver safety was ensured even at the worst case. The following tests were conducted ● Front impact ● Rear impact ● Side impact ● Static analysis ● Modal analysis ● Torsional analysis
  • 9. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1619 6.1 DYNAMIC ANALYSIS 6.1.1 FRONT IMPACT The first analysis to be completed was that of a front collision with a stationary object. In this case a deceleration of 10836 N was the assumed loading.For the front impact test, the front nodes are applied with the load calculated. The rear is completely constrained allowing displacement to occur only in direction of the load applied. The maximum stress after front impact was 200Mpa. But the yield stress of the material is 370 Mpa. So, our design proved to be safe. The factor of safety calculated from the front impact is 1.8499 6.1.2 REAR IMPACT Next rear impact analysis was done while assuming 7225.1N as the impact force. It is same as the front impact but the rear portion was constrained. The maximum stress after rear impact was 178.99Mpa. But the yield stress of the material is 370Mpa. So, our design proved to be safe. The factor of safety for the given load is calculated as 2.03 The total deformation for the given load is 2.365 6.1.3 SIDE IMPACT The next step in the analysis was to analyse a side impact with a 7225.1N load. As a side impact is most likely to occur with the vehicle being hit by another kart vehicle it was assumed that neither vehicle would be a fixed object. The maximum stress after side impact was 342.19Mpa. But the yield stress of the material is 370MPa The factor of safety is calculated as 1.08 for the given load
  • 10. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1620 6.2 STATIC ANALYSIS Total load acted=95+30=125kg=125*9.81=1226.25 N Where, weight of the driver assumed as 95 kg at the max conditions and the weight of the engine is assumed as 30 kg. The weight is assumed to be acted on the specific regions such as the driver seating and the engine mounting. Both the deformation and the stress analysis are done for static analysis. The weights of the other sub systems are negligible compared to driver’s weight and the weight of the engine. The maximum displacement during static analysis is 1.142. and fos=5.7 6.3 MODAL / VIBRATION ANALYSIS: Next for the vibrational analysis, the vibrational frequency applied to the frame is assumed to be is 133.3HZ calculated for 8000 rpm engine(stunner). The maximum displacement during vibrational analysis is 51.5mm 6.4 TORSION ANALYSIS In torsional analysis, among four wheels three wheels are fixed and a bumping load is acted on one wheel. The load acted on the single wheel =9.81(chassis weight+ driver weight+ engine weight) 9.81*(30+70+15)=1275.3 N
  • 11. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1621 The maximum deflection of the chassis during torsional analysis is 3.219mm. FOS=3.4 6.5 STATIC ANALYSIS OF SPROCKET Here the inside is kept fixed. The moment of 157.29N-m at first gear engagement is applied to the teeth that meshes with the chain. A maximum deformation of 0.0068mm is obtained. A maximum stress of 45.812MPa is obtained. A factor of safety of 5.45 is obtained when the load is 157.29N-m (first gear is engaged) 6.6 STATIC ANALYSIS OF STUB AXLE Here the axle part is fixed and the part attached to the wheel is given a load about 15 kN . here this load is due to the wobling of tires.we get quite a small amount of deformation of about 2.5*10^3mm in the left axle. 6.7 AXLE ANALYSIS: In the axle analysis,the live axle of the kart is mounted to the rear wheels. The loads and moment acting on the axle’s end and sprocket is calculated and the results are obtained. The moment acting on the sprocket is calculated as 157.5N-m ( Torque transferred when first gear is engaged ). Also the load of the kart is evenly distributed to
  • 12. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1622 each wheel hub positions and its calculated as 520N on each wheels. The deformation is calculated as 0.063021mm. The maximum deformation is calculated as 74.59MPa The factor of saftey is calculated as 4.905. 6.8 BRAKE PEDAL ANALYSIS: In the brake pedal analysis,The force given by the driver to the brake pedal is calculated and applied on the brake pad. By the standards the pedal force is about 400N.Its recommended that no more than this force is required to stop a passengers car.since a pressure of 200N applied othe brake and the result is observed. A deformation of 0.4404mm maximum is obtained. A maximum stress of 66.17MPa is obtained. A maximum factor of saftery of 5.5 is obtained for a load of 400N. ACKNOWLEDGEMENT The design process is not a single-handed effort and it is our team, whom we wanted to thank for standing with us under all circumstances. We would also like to express our gratitude towards the Mechanical department and on the whole towards the college for their support and also BFKCT for providing such a wonderful opportunity to learn and grow. Special thanks to our Head of the Department Dr. L.Karthikeyan and to the team mentor Mr.S.Dhanasekhar for their guidance and support. 7. CONCLUSIONS The finite element analysis method is used to evaluate the system and create and modify the best vehicle design to achieve its goal. The main goal was to simplify the overall
  • 13. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1623 design to make it more light weight without sacrificing performance and durability also make the driver comfortable. The result is lighter, faster and more angle vehicle that improves go kart design. REFERENCES  Fundamentals of vehicle dynamics by Thomas D. Gillespe.  Theory of machines by R.S. Khurmi  A textbook of machine design- R.S.Khurmi and J.K.Gupta  www.asos1.com  www.DIYgokart.com  www.Pirate 4x4.com  International Journal of Engineering Applied Sciences and Technology, 2016 Vol. 1, Issue ISSN No. 2455-2143  International Journal of Scientific & Engineering Research, Volume 7, Issue 4, April-2016 429 ISSN 2229-5518 IJSER © 2016 http://www.ijser.org DESIGN, ANALYSIS AND FABRICATION OF GO- KART Kiral Lal, Abhishek  International Journal of Science, Engineering and Technology Research (IJSETR) Volume 6, Issue 3, March 2017, ISSN: 2278 -7798 448 All Rights Reserved © 2017 IJSETR DESIGN OF A GO KART VEHICLE  Milliken & Milliken, “Race Car Vehicle Dynamics”  Reza M. jazar, “Vehicle Dynamics Theory and Applications(BBS)”  Asfan Mohiuddin, Mohd Sayeed, Md Nawaz “Steering System of Electric Go-Kart” International Journal for Research in Applied Science & Engineering Technology (IJRASET) Volume 5 Issue I, January 2017, IC Value: 45.98 ISSN: 2321-9653,Page 453-456.  .Govardhana Reddy, Md. Hameed, “design report of a go kart vehicle”, International Journal of Engineering Applied Sciences and Technology, 2016,Vol. 1, Issue 9, ISSN No. 2455-2143 , Pages 95- 102, Published Online July – August 2016  Dr.D.Ravikanth,Dr.K.Rajagopal,Dr.V.S.S. Murty, A. Harikrishna, “design of a go kart vehicle”, International Journal of Science, Engineering and Technology Research (IJSETR) Volume 6, Issue 3, March 2017, ISSN: 2278 -7798 ,Page 448-456. BIOGRAPHIES: R. Santosh kumar Department of Mechanical Engineering. R. Rohith Department of Mechanical Engineering. S. Srinivas Department of Mechanical Engineering.