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Jtasr.com Case Study
J. Technological Advances and Scientific Res./ eISSN- 2454-1788, pISSN- 2395-5600/ Vol. 2/ Issue 01/ Jan-Mar. 2016 Page 14
DESIGN AND ANALYSIS OF SIX CYLINDER FOUR STROKE ENGINE CRANK SHAFT
P. Preetham1, S. Srinivasa Prasad2
1Post Graduate Student, Department of Mechanical Engineering, Nova College of Engineering and Technology. 2Professor, Department of Mechanical Engineering, Nova College of Engineering and Technology.
ABSTRACT
The main objective of this study to analyze the average von-misses stress and principle shear stress over the crankshaft
using ANSYS Workbench software, the model creation can be created by well-known 3D modelling software SolidWorks.[1]
ANSYS will be used as a tool for analysis and optimization of crankshaft. The crankshaft conducting static analysis of the
crankshaft and dynamic analysis using modal analysis to find total deformation and frequency of the crankshaft. While
converting the reciprocating motion into rotary motion by the crankshaft, it is subjected to various stresses and vibrations. The
study to be carried out to check the load carrying capacity of the crankshaft. Static and dynamic analysis is conducted on the
structural steel crankshaft, Inconel x750 crankshaft of six cylinder four stroke engine.
KEYWORDS
Solid Works, ANSYS Workbench, FEM.
HOW TO CITE THIS ARTICLE: Preetham P, Prasad SS. Design and analysis of six cylinder four stroke engine crank shaft.
J. Technological Advances and Scientific Res. 2016;2(1):14-26, DOI: 10.14260/jtasr/2016/3
INTRODUCTION
The crankshaft plays a vital role in all Internal Combustion
Engine. It is a large component, which converts the
reciprocating displacement of the piston to a rotary motion
with a four link mechanism. It has complex shape of geometry.
The crankshaft experiences a cyclic load, due to the cyclic load
fatigue failure occur over a period. The fatigue analysis has to
be considered in the design stage itself. The design and
development of crankshaft has always been an important task
for the production industry in order to reduce the
manufacturing cost of the product minimum weight possible
and proper fatigue strength and other functional
requirements. These improvements result in lighter and
smaller engines with better fuel efficiency and higher power
output. This study was conducted on a single cylinder four
stroke cycle engine. Two different crankshafts from similar
engines were studied in this research. The finite element
analysis was performed in four static steps for each crankshaft.
Stresses from these analyses were used for superposition with
regards to dynamic load applied to the crankshaft. Further
analysis was performed on the forged steel crankshaft in order
to optimize the weight and manufacturing cost.
The crankshaft, sometimes casually abbreviated to crank
is the part of an engine which translates reciprocating linear
piston motion into rotation. To convert the reciprocating
motion into rotation, the crankshaft has “Crank throws” or
“Crankpins,” additional bearing surfaces whose axis is offset
from that of the crank, to which the "Big ends" of the
connecting rods from each cylinder attach. It typically
connects to a flywheel to reduce the pulsation characteristic of
the four-stroke cycle and sometimes atorsional or vibrational
Financial or Other, Competing Interest: None. Submission 22-01-2016, Peer Review 25-01-2016, Acceptance 28-01-2016, Published 02-02-2016. Corresponding Author: P. Preetham, D. No. 13-245, Chandamama Peta, Nandigama-521185. E-mail: [email protected] DOI:10.14260/jtasr/2016/3
damper at the opposite end to reduce the torsion vibrations
often caused along the length of the crankshaft by the cylinders
farthest from the output end acting on the torsional elasticity
of the metal.
1.1 Objective of the project
The automobile industry is showing increased interest in the
replacement of crankshaft with Inconel x750 crankshaft due to
high strength to weight ratio. Therefore; this project aims at
comparative study of design parameters of a traditional
crankshaft assembly by performing dynamic analysis using
ANSYS Workbench software the maximum bending stress and
corresponding payload have to be determined by considering
the factor of safety. Determining and assessing the behaviour
of the different parametric combinations of the crankshaft,
their natural frequencies are compared with the excitation
frequencies at different speeds of the crankshaft.
II OVERVIEW OF CRANKSHAFT
2.1 Crankshaft definition
A crankshaft is used to convert reciprocating motion of the
piston into rotary motion or vice versa. The crankshaft consists
of the shaft parts which revolve in the main bearings, the crank
pins to which the big ends of the connecting rod are connected,
the crank arms or webs which connect the crankpins and the
shaft parts. The crankshaft depending upon the position of
crank, may be divided into the following two types. The
crankshaft is the principal member of the crank train or crank
assembly, which latter converts the reciprocating motion of the
pistons into rotary motion. It is subjected to both torsional and
bending stresses and in modern high-speed, multi-cylinder
engines these stresses may be greatly increased by resonance,
which not only renders the engine noisy, but also may fracture
the shaft. In addition, the crankshaft has both supporting
bearings (Or main bearings) and crankpin bearings and all of
its bearing surfaces must be sufficiently large so that the unit
bearing load cannot become excessive even under the most
unfavourable conditions.
At high speeds the bearing loads are due in large part to
dynamic forces-inertia and centrifugal. Fortunately, loads on
main bearings due to centrifugal force can be reduced and even
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completely eliminated by the provision of suitable
counterweights. All dynamic forces increase as the square of
the speed of rotation. (i.e. FDynamic↑⇒Speed2 ↑).
2.2 Classification of crankshaft
Types of crankshaft
A crankshaft is composed of the crankpins, crank arms, crank
journals and driving ends. As a rule crankshafts are forged in a
single piece, but occasionally they are built up. Built-up
crankshafts are used in small single- and double-cylinder
motorcycle engines. The enclosed flywheels of these engines
take the place of the crank arms, the crankpin and crank
journals being bolted to the flywheels, which latter are cast
with solid webs. The built-up construction also has advantages
when it is desired to support the crankshaft in three or more
ball bearings, as with a one-piece shaft all intermediate
bearings would have to be stripped over the crank arms and
therefore would have to be made extraordinarily large. A
crankpin together with the two crank arms on opposite sides
of it is frequently referred to as a “Throw.” In some crankshafts,
there is only a single throw between a pair of main journals or
supporting bearings.
2.2.1 Based on the position of the crank pin
Overhung crankshaft or side crankshaft
Centre crankshaft
Fig. 2.2.1: Overhung crankshaft or side crankshaft
Fig. 2.2.2: Center crankshaft
2.3 Major parts of crankshaft
The major parts of crankshaft are shown in the below figure.
These figure illustrates the assembly of the crankshaft and
elucidates each and every part of the crankshaft, which is
assembled as in the figure. Every part assembled as in the
figure is elaborated and explained below.
Fig. 2.3: Crankshaft parts
Counter weight
Flywheel mounting flange
Oil hole
Main bearing journal
Main journals
2.3.1 Crank-Throw
This is the distance from the main journal centers to the big-
end-journal centers. It is the amount the cranked arms are
offset from the center of rotation of the crankshaft shown in
Fig 3.3. A small crank-throw reduces both the crankshaft
turning effort and the distance the piston moves between the
dead centers. A large crank-throw increases both the leverage
applied to the crankshaft and stroke of the piston.
2.3.2 Crank-Webs
These are the cranked arms of the shaft, which provide the
throws of the crankshaft. They support the big-end crankpin.
They must have adequate thickness and width to withstand
both the twisting and the bending effort, created within these
webs. But their excessive mass causes inertial effect, which
tends to wind and unwind the shaft during operation.
2.3.3 Main bearing Journal
Main-journal is the parallel cylindrical portions of the
crankshaft, supported rigidly by the plain bearings mounted in
the crankcase. The journals diameter must be proper to
provide torsion strength. The diameter and width of the
journal should have sufficient projected area to avoid
overloading of the plain bearing.
2.3.4 Connecting-Rod Big End (Crankpin) Journals
These journals have cylindrical smooth surfaces for the
connecting-rod big-end bearings to rub against.
Fig. 2.3.4: Model of crankshaft
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2.4 Function of crankshafts in IC engines
The crankshaft, connecting rod and piston constitute a four bar
slider crank mechanism, which converts the sliding motion of
the piston (Slider in the mechanism) to a rotary motion. Since
the rotation output is more practical and applicable for input
to other devices, the concept design of an engine is that the
output would be rotation. In addition the linear displacement
of an engine is not smooth, as the displacement is caused by
the combustion of gas in the combustion chamber. Therefore,
the displacement has sudden shocks and using this input for
another device may cause damage to it. The concept of using
crankshaft is to change these sudden displacements to a
smooth rotary output, which is the input to many devices such
as generators, pumps and compressors.
Crankshaft must be strong enough to take the downward
force of the power stroke without excessive bending, so the
reliability and life of the internal combustion engine depend on
the strength of the crankshaft largely. The crank pin is like a
built in beam with a distributed load along its length that
varies with crank positions. Each web is like a cantilever beam
subjected to bending and twisting. 1. Bending moment which
causes tensile and compressive stresses. 2. Twisting moment
causes shear stress. There are many sources of failure in the
engine one of the most common crankshaft failure is fatigue at
the fillet areas due to the bending load causes by the
combustion.
The moment of combustion the load from the piston is
transmitted to the crankpin, causing a large bending moment
on the entire geometry of the crankshaft. At the root of the fillet
areas stress concentrations exist and these high stress range
locations are the points where cyclic loads could cause fatigue
crank initiation leading to fracture.
2.5 Working of crankshaft in general
Power from the burnt gases in the combustion chamber is
delivered to the crankshaft through the piston pin and
connecting rod. The crankshaft changes reciprocating motion
of the piston in cylinder to the rotary motion of the flywheel.
Conversion of motion is executed by use of the offset in the
crankshaft. Each offset part of the crankshaft has a bearing
surface known as a crank pin to which the connecting rod is
attached. Crank-through is the offset from the crankshaft
centre line. The stroke of the piston is controlled by the throw
of the crankshaft. The combustion force is transferred to the
crank-throw after the crankshaft has moved past top dead
centre to produce turning effort or torque, which rotates the
crankshaft. Thus all the engine power is delivered through the
crankshaft. The cam-shaft is rotated by the crankshaft through
gears using chain driven or belt driven sprockets. The cam-
shaft drive is timed for opening of the valves in relation to the
piston position. The crankshaft rotates in main bearings, which
are split in half for assembly around the crankshaft main
bearing journals.
Both the crankshaft and camshaft must be capable of
withstanding the intermittent variable loads impressed on
them. During transfer of torque to the output shaft, the force
deflects the crankshaft. This deflection occurs due to bending
and twisting of the crankshaft. Crankshaft deflections are
directly related to engine roughness. When deflections of the
crankshaft occur at same vibrational or resonant frequency as
another engine part, the parts vibrate together. These
vibrations may reach the audible level producing a ―thumping
sound. The part may fail if this type of vibration is allowed to
continue. Harmful resonant frequencies of the crankshaft are
damped using a torsional vibration damper. Torsional stiffness
is one of the most important crankshaft design requirements.
This can be achieved by using material with the correct
physical properties and by minimizing stress concentration.
The crankshaft is located in the crankcase and is
supported by main bearings. Figure 3.62 represents schematic
view of a typical crankshaft. The angle of the crankshaft throws
in relation to each other is selected to provide a smooth power
output. V-8 engines use 90-degree and 6 cylinder engines use
120-degree crank throws. The engine firing order is
determined from the angles selected. A crankshaft for a four
cylinder engine is referred to a five bearing shaft. This means
that the shaft has five main bearings, one on each side of every
big end, which makes the crankshaft very stiff and supports it
well. As a result the engine is normally very smooth and long
lasting.
Because of the additional internal webs required to
support the main bearings, the crank case itself is very stiff.
The disadvantages of this type of bearing arrangement are that
it is more expensive and engine may have to be slightly longer
to accommodate the extra main bearings. Counter weights are
used to balance static and dynamic forces that occur during
engine operation. Main and rod bearing journal overlap
increases crankshaft strength because more of the load is
carried through the overlap area rather than through the fillet
and crankshaft web. Since the stress concentration takes place
at oil holes drilled through the crankshaft journals, these are
usually located where the crankshaft loads and stresses are
minimal. Lightening holes in the crank throws do not reduce
their strength if the hole size is less than half of the bearing
journal diameter, rather these holes often increase crankshaft
strength by relieving some of the crankshaft’s natural stress.
Automatic transmission pressure and clutch release forces
tend to push the crankshaft towards the front of the engine.
III MODELLING ON CRANKSHAFT
The software used for Modelling of crankshaft SOLID WORKS
and software it is developed by Dassault Syste mes. This is
CAD/CAM/CAE software, but we are using this for only 3-D
part modelling (CAD). This CAD includes. [2]
3.1 Steps involved in design of crankshaft
1. Open solid works software.
2. Open new part drawing.
3. Go to sketch command, select front plane.
4. Draw the profile using circle and fillet as per the
dimensions.
5. Exit the sketch and enter into feature manager and select
boss-extrude.
6. Extrude the object as per the dimension.
7. Again come to sketch manager and select plane1 and
draw a circle.
8. Exit sketch and extrude the selected sketch up to the
given dimension.
9. Draw a circle in the same plane and extrude it.
10. Repeat the same procedure by selecting up to 8 planes.
11. Revolve the required entities using sketch command.
12. Fillet all the sharp edges in the model.
13. Save the drawing in .x_t format.
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Fig. 3.1: In this figure shows that designing of crank web
from sketch tool bar
Fig. 3.2: In this figure draw a circle on web and use the
same command to extrude
Fig. 3.3: In this figure again draw the same web from sketch
tool bar and extrude by using boss extrude command
Fig. 3.4: In this figure copy the crank web already
drawn on planes
Fig. 3.5: In this figure follow the same to get six
cylinder positions
Fig. 3.6: In this figure use the command fillet to get smooth
surface on sharp edges
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Fig. 3.7: This figure shows the top view of completed design of crankshaft.[3]
IV BASICS OF FINITE ELEMENT ANALYSIS
4.1 Introduction to F.E.A
The name finite element is of recent origin, through the
concept has been used for centuries. The basic philosophy is to
replace the actual problem into a simpler model, which will
closely approximate the solution of the problem at hand. A
continuum is divided into a much; two adjacent regions placed
side by side will have a common edge. It is assumed that the
elements are connected at nodal points and it is only there that
the continuity requirements are to be satisfied. Once the
discrimination is made, the analysis follows a rather set
procedure. The stiffness matrix of the individual element is
formulated. The forces are distributed in the real structure are
transformed to actually distribute in the real structure are
transformed to act at the nodal lines. Assembly of individual
elements is carried out to obtain stiffness matrix of the whole
structure. In the finite element analysis, therefore the
continuum is divided into a finite number of elements, having
finite dimensions and reducing the continuum from infinite
degree of freedom to finite degrees of unknowns. The problem
to be solved by the finite element method is done in two stages:
1. The element formulation.
2. The system formulation.
The first stage involves the derivation of the element
stiffness matrix. The next stage is the formulation of stiffness
and load of the entire structure.
Static analysis
Static analysis calculates the effects of steady loading
conditions on a structure while ignoring inertia and damping
effects, such as those caused by time – varying loads.[4]
Static analysis is used to determine the displacements,
stress, stains and forces in structures or components caused by
loads that do not induce significant inertia and damping
effects. Steady loading and response conditions are assumed,
that is the loads and structures response are assumed to vary
slowly with respect to time.[5]
The kinds of loading that can be applied in a static
analysis include externally applied forces and pressure.
Steady–state inertial forces (Such as gravity or rotational
velocity) Temperatures (For thermal strain).
Modal analysis
In many engineering applications, the natural frequencies of
vibration are of interest. This is probably the most common
type of dynamic analysis and is referred to as ‘Eigenvalue
analysis.’ In addition to the frequencies, the mode shapes of
vibration which arise at the natural frequencies are also of
interest. These are the undamped free vibration response of
the structure caused by an initial disturbance from the static
equilibrium position. This solution derives from the general
equation by zeroing the damping and applied force terms.
Thereafter, it is assumed that each node is subjected to
sinusoidal functions of the peak amplitude for that node.[6]
If we deal with an FE (Finite element) structure for which
there is more than one d.o.f., R is the load which contains the
moments as well as forces, K is the stiffness matrix, C is the
damping matrix and M is the mass matrix.
KD+CD+MD=R
D is the nodal velocity; D is nodal acceleration and D
amplitude (global) d.o.f. With no damping C=0. Vibration is
free if loads are either zero or constant. Vibration motion
consist of displacements that very sinusoidally with time
relative to the mean configuration Dm created by constant
loads Rc.
D = Dm + DSinωt Dm is the vector of nodal displacements
in vibration and w is the natural frequency in radians per
second.
Where Dm = K-1Rc hence Dm = K-1Rc
Substituting all this information and C = 0 we obtain
[K - ω2 M]D = 0
As the governing equation of undamped free vibrations,
mathematically it is called Eigenvalue problem. A natural
frequency may also be called as resonant frequency and ωi2 is
various called Eigenvalue, latent root or characteristic number.
A mode may also be called an Eigenvector, mode shape, normal
mode or principal mode the smallest non-zero ωi is called the
fundamental natural frequency of vibration.
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Whereas the Eigenvalue, λ, is equal to the total number of
degrees of freedom in the model, each Eigenvalue or frequency
has a corresponding eigenvector or mode shape. Since each of
the Eigenvectors cannot be null vectors, the mode shapes are
also of interest to the engineer. These are normalized to the
maximum displacement of the structure. The Theoretical
solution implies that the structure will vibrate in any mode
shape indefinitely. However, since there is always some
damping present in any structure, the vibrations eventually
decay.
V DYNAMIC ANALYSIS OF CRANKSHAFT
5.1 Steps involved in ANSYS Workbench 14.5
1. Start menu-programs-ANSYS-ANSYS workbench.
2. Select finite element model in left menu bar and drag it
into the screen page.
3. Then import the model by using add input mesh.
4. After importing update the project.
5. Select static structural and drag into the screen.
6. Update the model and click setup.
7. Open the window and click static structural and insert
boundary conditions, pressure on the required areas.
8. Click solution and insert the solution parameters like
deformation, stress, strain, etc.
9. After inserting solve the model with given input
conditions.
10. To change the material go to geometry, select the model
and import new material.
11. Repeat the same procedure for different materials.
12. Save the file in .igs format.
Import the IGS format file to ANSYS workbench 14.5 and
mesh the crankshaft
Fig. 5.1: Imported the IGS format of crankshaft to ANSYS
workbench
Fig. 5.2: Meshing of model carried out in ANSYS 14.5
Mesh the Crankshaft
Mesh Statics:
Type of Element: Tetrahedrons
Number of Nodes: 753229
Number of Elements: 686492
5.2 STATIC STRUCTURAL ANALYSIS
A static structural analysis determines the displacements,
stresses, strains and forces in structures or components
caused by loads that do not induce significant inertia and
damping effects.[7] Steady loading and response conditions are
assumed, that is the loads and the structure’s response are
assumed to vary slowly with respect to time. The types of
loading that can be applied in a static analysis include
externally applied forces and pressures, steady-state inertial
forces (Such as gravity or rotational velocity), imposed
(Nonzero) displacements, temperatures (For thermal strain).
5.2.1 Applying material-1 for crankshaft
PROPERTY VALUE YOUNGS MODULUS(E) 2X105MPA SHEAR MODULUS(G) 0.769X105MPA POISSON’S RATIO(µ) 0.3
DENSITY(ρ) 7850kg/m3 Table 5.2.1: Material I details
Define boundary condition for analysis
Boundary conditions play an important role in Finite Element
Analysis. Here, we have taken fixed supports on ends and
which acts as bearings.
Fig. 5.2.1.1: Fix the ends with roller support bearing as
shown in the figure
Fig. 5.2.1.2: The pressure 3.5 MPa is applied on the top of
the crankpin surface then apply pressure on the crankpin
as shown in the figure
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Run the analysis and Get Results
Fig. 5.2.1.3: Total deformation(mm)
Fig. 5.2.1.4: Crankshaft von Mises stress (MPa).[8]
Fig. 5.2.1.5: Crankshaft shear stress (MPa)
5.2.2 Applying material-2 for crankshaft
PROPERTY VALUE YOUNGS MODULUS(E) 213.7KN/mm2 SHEAR MODULUS(G) 218.0KN/mm2 POISSON’S RATIO(µ) 0.29
DENSITY(ρ) 8.28X1000kg/m3 Table 5.2.2: Material II details
Fig. 5.2.2.1: Total deformation (mm)
Fig. 5.2.2.2: Crankshaft von Mises stress (MPa)
Fig. 5.2.2.3: Crankshaft shear stress (MPa)
MATERIAL TOTAL
DEFORMATION (mm)
EQUIVALENT STRESS (MPa)
SHEAR STRESS (MPa)
STRUCTURAL STEEL
0.0084988 4.2822 0.84067
INCONEL X750
0.0077197 4.2409 0.84445
Table 5.2.3: Results of structural analysis of two materials
5.3 MODAL ANALYSIS
In order to determine fundamental mode shapes and
corresponding natural frequencies, Modal Analysis of the
modified design of crankshaft is to be done.[9] Modal analysis
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is a technique to study the dynamic characteristics of a
structure under vibrational excitation. Natural frequencies,
mode shapes and mode vectors of a structure can be
determined using modal analysis. Modal analysis allows the
design to avoid resonant vibrations or to vibrate at a specified
frequency and gives engineers an idea of how the design will
respond to different types of dynamic loads.
5.3.1 Material I details
Material type:- Structural steel
Poisson ratio:- 0.3
Young’s modulus:- 2x105 MPa
Fig. 5.3.1.1: First mode of vibration
Fig. 5.3.1.2: Second mode of vibration
Fig. 5.3.1.3: Third mode of vibration
Fig. 5.3.1.4: Fourth mode of vibration
Fig. 5.3.1.5: Fifth mode of vibration
Fig. 5.3.1.6: Sixth mode of vibration
Fig. 5.3.1.7: Seventh mode of vibration
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Fig. 5.3.1.8: Eighth mode of vibration
Fig. 5.3.1.9: Ninth mode of vibration
Fig. 5.3.1.10: Tenth mode of vibration
5.3.2 Material II details
Material type:- Inconel X750
Poisson ratio:- 0.29
Young’s modulus:- 213.7KN/mm2
Fig. 5.3.2.1: First mode of vibration
Fig. 5.3.2.2: Second mode of vibration
Fig. 5.3.2.3: Third mode of vibration
Fig. 5.3.2.4: Fourth mode of vibration
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Fig. 5.3.2.5: Fifth mode of vibration
Fig. 5.3.2.6: Six mode of vibration
Fig. 5.3.2.7: Seventh mode of vibration
Fig. 5.3.2.8: Eighth mode of vibration
Fig. 5.3.2.9: Ninth mode of vibration
Fig. 5.3.2.10: Tenth mode of vibration
5.3.3 RESULTS OF MODAL ANALYSIS
VI RESULTS AND CONCLUSION
MODES 1 2 3 4 5 6 7 8 9 10
STRUCTURAL STEEL 1.753 1.753 1.766 1.655 2.114 2.977 2.2866 2.3458 3.1889 3.1793
INCONEL X750 1.707 1.707 1.72 1.611 1.611 2.891 2.276 3.10 3.06 3.38
Table 5.3.3: Results Modal Analysis
6.1 INTRODUCTION
From the two material specifications, the crankshaft is
performed dynamic analysis to find the maximum safe stress
and the corresponding pressure. And also modal analysis is
performed for various parametric combinations to find the
natural frequencies and mode shapes to find the behaviour of
the crankshaft. And these natural frequencies are compared
with the excitation frequencies.
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6.2 STATIC STRUCTURAL ANALYSIS
Static structural analysis is performed to crankshaft total
deformation, von Mises stress, shear stress by using ANSYS
workbench 14.5 software and the results are compared
between two different materials at a pressure 3.5 MPa.
6.2.1 Static analysis performed on steel material.[10]
Material properties 1:
Material type:- Structural steel
Poisson ratio:- 0.3
Young’s modulus:- 2x105 MPa
Material II details:
Material type:- Inconel X750
Poisson ratio:- 0.29
Young’s modulus:- 213.7KN/mm2
MATERIAL TOTAL
DEFORMATION (mm)
EQUIVALENT STRESS (MPa)
SHEAR STRESS (MPa)
STRUCTURAL STEEL
0.0084988 4.2822 0.84067
INCONEL X750
0.0077197 4.2409 0.84445
Table 6.2.1: Results of structural analysis
6.3 MODAL ANALYSIS
In order to determine fundamental mode shapes and
corresponding natural frequencies, Modal Analysis of the
modified design of crankshaft is to be done. Modal analysis is a
technique to study the dynamic characteristics of a structure
under vibrational excitation. Natural frequencies, mode shapes
and mode vectors of a structure can be determined using
modal analysis. Modal analysis allows the design to avoid
resonant vibrations or to vibrate at a specified frequency and
gives engineers an idea of how the design will respond to
different types of dynamic loads.
MODES 1 2 3 4 5 6 7 8 9 10 STRUCTURAL STEEL 1.753 1.753 1.766 1.655 2.114 2.977 2.2866 2.3458 3.1889 3.1793
INCONEL X750 1.707 1.707 1.72 1.611 1.611 2.891 2.276 3.10 3.06 3.38 Table 6.3.1: Results of modal analysis
Modal analysis is performed on two materials of crankshaft; the above table shows ten modes of natural frequencies.
Line graph shows the difference of modes between two materials
Fig. 6.3.2: Shows comparison of two different materials
CONCLUSION
From the above results, Inconel X750 is subjected to less
deformation compared to remaining two materials.
The crankshaft design is also safe since the von Mises
stresses are within the limits.
From the obtained results structural steel has less
frequency compared to other two materials.
Mode shapes and modal frequencies are determined for
all the mode numbers using modal analysis.
The maximum deformation appears at the center of
crankpin neck surface.
The maximum stress appears at the fillets between the
crankshaft journal and crank cheeks and near the central
point journal.
From the results it is concluded that the crankshaft
design is safe since the von mises stresses are within the
limits.
The maximum deformation was located at the link
between main bearing journal and crankpin and crank
cheeks.
The resonance vibration of system can be avoided
effectively by appropriate structure design.
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LITERATURE REVIEW
1. Rinkle Garg and Sunil Baghl.[1] have been analyzed
crankshaft model and crank throw were created by Pro/E
Software and then imported to ANSYS software. The result
shows that the improvement in the strength of the
crankshaft as the maximum limits of stress, total
deformation and the strain is reduced. The weight of the
crankshaft is reduced, thereby reduces the inertia force. As
the weight of the crankshaft is decreased this will decrease
the cost of the crankshaft and increase the IC engine
performance.
2. C.M. Balamurugan et al.[2] has been studied the Computer
aided Modelling and Optimization of crankshaft and
compare the fatigue performance of two competing
manufacturing technologies for automotive crankshafts,
namely forged steel and ductile cast iron. The three
dimensional model of crankshaft were created by solid
edge software and then imported to ANSYS software. The
optimisation process included geometry changes
compatible with the current engine, fillet rolling and
results in increased fatigue strength and reduced cost of
the crankshaft without changing connecting rod and
engine block.
3. Gu Yingkui, Zhou Zhibo.[3] have been discussed a three-
dimensional model of a diesel engine crankshaft were
established by using PRO/E software and analytical ANSYS
Software tool, it shows that the high stress region mainly
concentrates in the knuckles of the crank arm and the main
journal and the crank arm and connecting rod journal,
which is the area most easily broken.
4. Abhishek Choubey and Jamin Brahmbhatt.[4] have been
analyzed crankshaft model and 3-dimensional model of the
crankshaft were created by Solid Works Software and
imported to ANSYS software. The crankshaft maximum
deformation appears at the centre of crankpin neck
surface. The maximum stress appears at the fillets between
the crankshaft journals and crank cheeks and near the
central point journal. The edge of main journal is high
stress area.
5. R.J. Deshbhratar and Y.R. Suple.[5] have been analyzed 4-
cylinder crankshaft and model of the crankshaft were
created by Pro/E Software and then imported to ANSYS
software. The maximum deformation appears at the centre
of crankshaft surface. The maximum stress appears at the
fillets between the crankshaft journal and crank cheeks
and near the central point. The edge of main journal is high
stress area. The crankshaft deformation was mainly
bending deformation under the lower frequency and the
maximum deformation was located at the link between
main bearing journal and crankpin and crank cheeks. So
this area prone to appear the bending fatigue crack.
6. Solanki et al.[6] presented literature review on crankshaft
design and optimization. The materials, manufacturing
process, failure analysis, design consideration, etc. were
reviewed. The design of the crankshaft considers the
dynamic loading and the optimization can lead to a shaft
diameter satisfying the requirements of the automobile
specifications with cost and size effectiveness. They
concluded that crack grows faster on the free surface, while
the central part of the crack front becomes straighter.
Fatigue is the dominant mechanism of failure of the
crankshaft. Residual imbalances along the length of the
crankshafts are crucial to performance.
7. Meng et al.[7] discussed the stress analysis and modal
analysis of a 4 cylinder crankshaft. FEM software ANSYS
was used to analyze the vibration modal and distortion and
stress status of crank throw. The relationship between
frequency and the vibration modal was explained by the
modal analysis of crankshaft. This provides a valuable
theoretical foundation for the optimization and
improvement of engine design. Maximum deformation
appears at the center of the crankpin neck surface. The
maximum stress appears at the fillet between the
crankshaft journal and crank cheeks and near the central
point journal. The crankshaft deformation was mainly
bending deformation was mainly bending deformation
under the lower frequency. Maximum deformation was
located at the link between main bearing journal and
crankpin and crank cheeks. So the area prone to appear the
bending fatigue crack.
8. Guangming and Zhengfeng.[8] performed study on
torsional stiffness of engine crankshaft. Modified Ker
Wilson formula and Carter formula were employed to
calculate torsional stiffness of engine crank throw in the
case of different thickness and width of both sides of crank
throw. Furthermore, the finite element modals of crank
and free part of crankshaft linked to torsional dynamic
models were developed. Then the intrinsic torsional
vibration frequency of crank and free part of crankshaft are
carried out by finite element method. According to
mechanics of materials and empirical formula, a
theoretical calculation formula of crank torsional stiffness
is proposed in the conditions of the thickness and width on
both sides of crank throw are different. By calculation and
comparative analysis of a real crankshaft example to verify
the finite element analysis method and finite element
model is feasible.
9. Xiaoping et al.[9] sets the automatic solving model, which
integrates the parameters geometric module, finite
element analysis module, numerical calculation module.
This model was based on the multidisciplinary
collaborative design optimization platform, combining the
finite element analysis, variable structure parameters of
the design and the design of experiment. Then the sample
matrix is setup by Latin hypercube sampling method. The
sensitivity analysis, the main effect analysis and the
interaction analysis of the key structural parameters on
crankshaft fatigue strength were accomplished. Results
show that the crankshaft fillet radius has the greatest
influence on the crankshaft strength and the crank radius
has less influence on the crankshaft strength.
10. Ling et al.[10] conducted fatigue life prediction modeling
and residue life assessment based on Statistics of Historical
Working State (SHWS) at crankshaft using Fatigue Damage
Accumulation (FDA) theory. Dynamic response of typical
operation performance is analyzed with software ANSYS of
finite element analysis and high stress zone was found.
Then via rain flow cycle counting for stress time obtained
together with SHOP, fatigue load spectra of key parts are
compiled. Finally, FDA model is built up with nominal
stress method and residue life based on SHWS is predicted
for crankshafts of diesel engine. It was found that main
shaft journal of crankshaft near the power output side and
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J. Technological Advances and Scientific Res./ eISSN- 2454-1788, pISSN- 2395-5600/ Vol. 2/ Issue 01/ Jan-Mar. 2016 Page 26
connected rod journal have relatively high stress and FDA
of the same time is relatively larger.
11. Bin et al.[11] investigated the vibration model of 480 diesel
crankshaft and the stress analysis of crankpin. Three
dimensional models of 480 diesel engine crankshaft and
crankpin were created through Pro E software. Finite
element analysis software ANSYS was used to analyze the
vibration model and the distortion and the stress status of
the crankpin. This explains the relationship between the
frequency and the vibration model. Stress analysis of
crankpin provides the maximum deformation and
maximum stress point. The crankshaft deformation was
mainly bending deformation under lower frequency. The
maximum deformation was located at the link between
main bearing journal and crankpin and crank cheeks. So
the bending crack was prone to appear at this area. The
maximum deformation appears the bottom of crank cheek.
The maximum stress appears at the transition radius of
crank cheek and connecting rod journal.
12. Gongzhi et al.[12] carried out dynamic strength analysis of
crankshaft for marine diesel engine. The finite element
models of crankshaft, bearing, piston and connecting rod
was created in ANSYS and simplified by substructure
technique. The result files of reduced models were
introduced into EXCITE software to create multi-body
dynamics calculation of crankshaft in one working cycle.
Compared with single crankshaft strength analysis, non-
linear multi-body dynamics method is closer to the actual
boundary conditions of the crankshaft load. Combining
AVL-EXCITE multi-body dynamics and ANSYS finite
element method analyzed the dynamic characteristics of
marine crankshaft. This shows that under normal
operating conditions, the maximum stress of crankshaft
occurs on journal fillet.
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