This document summarizes a study on failures of shafts in coil car assemblies. The researchers investigated a failed coil car shaft and found that reversed bending fatigue caused it to fracture, occasionally due to misalignment. They calculated loads on the existing shaft theoretically and analytically and found the stresses exceeded permissible levels, indicating it was prone to failure. To improve shaft design, they examined increasing diameter and using fillets/chamfers to disperse stresses. A literature review showed other shaft failures were due to low radius of curvature, incorrect chamfer size increasing stress concentration, and vibrations from imbalance.
FEA OF A CRANKSHAFT IN CRANK-PIN WEB FILLET REGION FOR IMPROVING FATIGUE LIFEijiert bestjournal
A crankshaft is often designed with a fillet radius to improving fatigue life of crankshaft. The fatigue life of crankshaft is depend on the proper fillet radius. This fillet radius is changes than fatigue life is also changes of crankshaft. In most of the time fatigue failure is occur in crank-pin web fillet region. The crankshaft fillet rolling process is one of the commonly adopted methods in engineering to improve fatigue life of the crankshaft. A finite element analysis is implemented to approximate the stress distribution induced in the crankpin fillet region. The modelling of crankshaft is created by Creo-parametric. Finite element analysis is performed to obtain the variation of stress at critical locations and fatigue life of the crank shaft using the ANSYS software and applying th e boundary conditions. Radius of fillet is changes in model of crankshaft to improvement in fatigue life. Th is work in doing for optimization of a crankshaft in crank-pin web fillet region with fatigue life as well as to study a relation between fillet radius/diameter of crankpin to fatigue life. .
A REVIEW ON HELICAL COMPRESSION SPRING TO DESIGN A SHOCK ABSORBER OF BIKEJournal For Research
A spring is an elastic object used to store mechanical energy. A shock absorber is a mechanical device designed to smooth out or damp shock impulse & dissipate kinetic energy. In this paper there is reviewed some papers on suspension system. The aim of this review paper is to represent a general study on the analysis of spring to fulfil the requirement of suspension system.
Rocker arms are part of the valve-actuating mechanism. A rocker arm is designed to pivot on a pivot
pin or shaft that is secured to a bracket. The bracket is mounted on the cylinder head. One end of a
rocker arm is in contact with the top of the valve stem, and the other end is actuated by the camshaft.
In installations where the camshaft is located below the cylinder head, the rocker arms
are actuated by pushrods. The lifters have rollers which are forced by the valve springs to follow the
profiles of the cams. Failure of rocker arm is a measure concern as it is one of the important
components of push rod IC engines.Present work finds the various stresses under extreme load
condition. For this we are modeling the arm using design software and the stressed regions are
found out usingAnsys software. Here in this thesis we are observing that by changing different
materials how the stresses are varying in the rocker arm under extreme load condition. And after
comparing results we are proposing best suitable material for the rocker arm under extreme load conditions.
Rocker arms are part of the valve-actuating mechanism. A rocker arm is designed to pivot on a pivot pin or shaft that is secured to a bracket. The bracket is mounted on the cylinder head. One end of a rocker arm is in contact with the top of the valve stem, and the other end is actuated by the camshaft. In installations where the camshaft is located below the cylinder head, the rocker arms are actuated by pushrods. The lifters have rollers which are forced by the valve springs to follow the profiles of the cams. Failure of rocker arm is a measure concern as it is one of the important components of push rod IC engines.Present work finds the various stresses under extreme load condition. For this we are modeling the arm using design software and the stressed regions are found out usingAnsys software. Here in this thesis we are observing that by changing different materials how the stresses are varying in the rocker arm under extreme load condition. And after comparing results we are proposing best suitable material for the rocker arm under extreme load conditions.
Stress and fatigue analysis of landing gear axle of a trainer aircrafteSAT Journals
Abstract The undercarriage or landing gear of an aircraft is the structure that supports an aircraft on the ground and allows it to taxi, takeoff and land. Among the various parts of landing gear, axle is the most critical component where the loads (landing and ground loads) act on the axle first, then transferred to the structure. In this study stress and fatigue analysis of the axle is performed to meet the strength and life requirements. The modeling of the axle is done using UniGraphics (UG) software. Stress analysis is carried out using MSC Patran (pre-processing and post-processing)/Nastran (solver) for different landing loads (spin up, spring back, maximum vertical and drift) and ground handling loads (braking, taxing and turning). Stress analysis was carried out by both classical and FEM approaches and by comparing the results it was obvious that they were in correlation with one another. Fatigue analysis was also carried out for the axle using landing spectrum and ground handling spectrum to estimate the fatigue life. By the iteration process, the requirement of 10000 landings was satisfied. Keywords: Static, Fatigue, Axle, Fatigue life, UniGraphics, MSC Patran, MSC Nastran
Failure prediction of propeller shaft prototype using finite element analysiseSAT Journals
Abstract
A premature failure that occurs before the expected load cycle during the torsional fatigue test of a propeller shaft assembly prototype is studied. In these test crack mainly originated repetitively from one of the components, namely Flange yoke at same region. To determine the root reason of the failure a detail CAD model of Flange yoke was developed and analyzed by Finite Element Method. Fatigue crack initiation and location were determined and compared with test data. We found good correlation between FEM results with testing failure results. Design improvements solutions are proposed to increase the fatigue life. Mechanical properties of the Flange yoke were determined by the tensile strength test. Using these input datas stress and strain analysis was performed in ANSYS software.
Keywords: Finite Element Analysis, Stress Concentration, Structural Analysis
Modeling and Analysis of Two Wheeler Connecting Rod by Using AnsysIOSR Journals
Connecting rod is a major link inside of a internal combustion engine. It is the intermediate member
between the piston and the crankshaft. Its primary function is to transmit the push and pull from the piston pin
to the crank pin thus converting the reciprocating motion of piston in to rotary motion of the crank. In this paper
a static analysis is conducted on a connecting rod of a single cylinder 4-stroke petrol engine. The model is
developed using Solid modeling software i.e. PRO/E (creo-parametric). Further finite element analysis is done
to determine the von-misses stresses shear stress and strains for the given loading conditions.
DESIGN, OPTIMIZATION AND FINITE ELEMENT ANALYSIS OF CRANKSHAFTijiert bestjournal
Crankshaft is a crucial component in an engine asse mbly. Crankshaft is consisting of two web sections and one crankpin,which converts the reciprocating displacement of the pist on to a rotary motion with a four link mechanism. G enerally crankshafts are manufactured using cast iron and forged steel mater ial. In this work to design and finite element anal ysis of crankshaft of 4 cylinder petrol engine of Maruti swift Vxi. of 1200 cubic capacity. The finite element analysis in ABA QUS software by using six materials based on their composition viz. Cast iron,EN30B,SAE4340,Structural steel,C70 Alloy steel and Aluminium based composite material reinforced with silicon carbide & fly ash. The parameter like von misses stress,deformation;maximum and minimum principal stress & strain were obtained from analysis software. The results of Finite element show that t he Aluminium based composite material is best mater ial among all. Compare the result like weight and Stiffness parameter. It is resulted of 65.539 % of weight,with reduction i n deformation.
ANALYSIS OF CNC LATHE SPINDLE FOR MAXIMUM CUTTING FORCE CONDITION AND BEARING...AM Publications
The present CNC machine structures consist of spindle system which plays a relating to the quality of the
final product and the overall productivity and efficiency of the machine tool itself. The spindle of a CNC lathe
machine, which is rotated by the main motor, holds the cutting tool, which cuts the work piece, so that the cutting
forces are generated which effects the spindle accuracy directly. The forces which are affecting the CNC machine tool
spindle are tangential force (Ft), feed force (Fc), radial force (Fr) and will be estimated. Based on maximum cutting
force incurred the analysis will be carried out. The main objective is to find the static, fatigue analysis of spindle
structure for maximum cutting force condition and predicting life of bearings. From static analysis stress and
deformation of the spindle can be found. Stress obtained from the stress analysis is less than the yield strength of the
material and deformation of the spindle is very less which can be neglected. Equivalent alternating stress, factor of
safety and life of the spindle is found by fatigue analysis and which results are closely matches with the analytical
value
FEA OF A CRANKSHAFT IN CRANK-PIN WEB FILLET REGION FOR IMPROVING FATIGUE LIFEijiert bestjournal
A crankshaft is often designed with a fillet radius to improving fatigue life of crankshaft. The fatigue life of crankshaft is depend on the proper fillet radius. This fillet radius is changes than fatigue life is also changes of crankshaft. In most of the time fatigue failure is occur in crank-pin web fillet region. The crankshaft fillet rolling process is one of the commonly adopted methods in engineering to improve fatigue life of the crankshaft. A finite element analysis is implemented to approximate the stress distribution induced in the crankpin fillet region. The modelling of crankshaft is created by Creo-parametric. Finite element analysis is performed to obtain the variation of stress at critical locations and fatigue life of the crank shaft using the ANSYS software and applying th e boundary conditions. Radius of fillet is changes in model of crankshaft to improvement in fatigue life. Th is work in doing for optimization of a crankshaft in crank-pin web fillet region with fatigue life as well as to study a relation between fillet radius/diameter of crankpin to fatigue life. .
A REVIEW ON HELICAL COMPRESSION SPRING TO DESIGN A SHOCK ABSORBER OF BIKEJournal For Research
A spring is an elastic object used to store mechanical energy. A shock absorber is a mechanical device designed to smooth out or damp shock impulse & dissipate kinetic energy. In this paper there is reviewed some papers on suspension system. The aim of this review paper is to represent a general study on the analysis of spring to fulfil the requirement of suspension system.
Rocker arms are part of the valve-actuating mechanism. A rocker arm is designed to pivot on a pivot
pin or shaft that is secured to a bracket. The bracket is mounted on the cylinder head. One end of a
rocker arm is in contact with the top of the valve stem, and the other end is actuated by the camshaft.
In installations where the camshaft is located below the cylinder head, the rocker arms
are actuated by pushrods. The lifters have rollers which are forced by the valve springs to follow the
profiles of the cams. Failure of rocker arm is a measure concern as it is one of the important
components of push rod IC engines.Present work finds the various stresses under extreme load
condition. For this we are modeling the arm using design software and the stressed regions are
found out usingAnsys software. Here in this thesis we are observing that by changing different
materials how the stresses are varying in the rocker arm under extreme load condition. And after
comparing results we are proposing best suitable material for the rocker arm under extreme load conditions.
Rocker arms are part of the valve-actuating mechanism. A rocker arm is designed to pivot on a pivot pin or shaft that is secured to a bracket. The bracket is mounted on the cylinder head. One end of a rocker arm is in contact with the top of the valve stem, and the other end is actuated by the camshaft. In installations where the camshaft is located below the cylinder head, the rocker arms are actuated by pushrods. The lifters have rollers which are forced by the valve springs to follow the profiles of the cams. Failure of rocker arm is a measure concern as it is one of the important components of push rod IC engines.Present work finds the various stresses under extreme load condition. For this we are modeling the arm using design software and the stressed regions are found out usingAnsys software. Here in this thesis we are observing that by changing different materials how the stresses are varying in the rocker arm under extreme load condition. And after comparing results we are proposing best suitable material for the rocker arm under extreme load conditions.
Stress and fatigue analysis of landing gear axle of a trainer aircrafteSAT Journals
Abstract The undercarriage or landing gear of an aircraft is the structure that supports an aircraft on the ground and allows it to taxi, takeoff and land. Among the various parts of landing gear, axle is the most critical component where the loads (landing and ground loads) act on the axle first, then transferred to the structure. In this study stress and fatigue analysis of the axle is performed to meet the strength and life requirements. The modeling of the axle is done using UniGraphics (UG) software. Stress analysis is carried out using MSC Patran (pre-processing and post-processing)/Nastran (solver) for different landing loads (spin up, spring back, maximum vertical and drift) and ground handling loads (braking, taxing and turning). Stress analysis was carried out by both classical and FEM approaches and by comparing the results it was obvious that they were in correlation with one another. Fatigue analysis was also carried out for the axle using landing spectrum and ground handling spectrum to estimate the fatigue life. By the iteration process, the requirement of 10000 landings was satisfied. Keywords: Static, Fatigue, Axle, Fatigue life, UniGraphics, MSC Patran, MSC Nastran
Failure prediction of propeller shaft prototype using finite element analysiseSAT Journals
Abstract
A premature failure that occurs before the expected load cycle during the torsional fatigue test of a propeller shaft assembly prototype is studied. In these test crack mainly originated repetitively from one of the components, namely Flange yoke at same region. To determine the root reason of the failure a detail CAD model of Flange yoke was developed and analyzed by Finite Element Method. Fatigue crack initiation and location were determined and compared with test data. We found good correlation between FEM results with testing failure results. Design improvements solutions are proposed to increase the fatigue life. Mechanical properties of the Flange yoke were determined by the tensile strength test. Using these input datas stress and strain analysis was performed in ANSYS software.
Keywords: Finite Element Analysis, Stress Concentration, Structural Analysis
Modeling and Analysis of Two Wheeler Connecting Rod by Using AnsysIOSR Journals
Connecting rod is a major link inside of a internal combustion engine. It is the intermediate member
between the piston and the crankshaft. Its primary function is to transmit the push and pull from the piston pin
to the crank pin thus converting the reciprocating motion of piston in to rotary motion of the crank. In this paper
a static analysis is conducted on a connecting rod of a single cylinder 4-stroke petrol engine. The model is
developed using Solid modeling software i.e. PRO/E (creo-parametric). Further finite element analysis is done
to determine the von-misses stresses shear stress and strains for the given loading conditions.
DESIGN, OPTIMIZATION AND FINITE ELEMENT ANALYSIS OF CRANKSHAFTijiert bestjournal
Crankshaft is a crucial component in an engine asse mbly. Crankshaft is consisting of two web sections and one crankpin,which converts the reciprocating displacement of the pist on to a rotary motion with a four link mechanism. G enerally crankshafts are manufactured using cast iron and forged steel mater ial. In this work to design and finite element anal ysis of crankshaft of 4 cylinder petrol engine of Maruti swift Vxi. of 1200 cubic capacity. The finite element analysis in ABA QUS software by using six materials based on their composition viz. Cast iron,EN30B,SAE4340,Structural steel,C70 Alloy steel and Aluminium based composite material reinforced with silicon carbide & fly ash. The parameter like von misses stress,deformation;maximum and minimum principal stress & strain were obtained from analysis software. The results of Finite element show that t he Aluminium based composite material is best mater ial among all. Compare the result like weight and Stiffness parameter. It is resulted of 65.539 % of weight,with reduction i n deformation.
ANALYSIS OF CNC LATHE SPINDLE FOR MAXIMUM CUTTING FORCE CONDITION AND BEARING...AM Publications
The present CNC machine structures consist of spindle system which plays a relating to the quality of the
final product and the overall productivity and efficiency of the machine tool itself. The spindle of a CNC lathe
machine, which is rotated by the main motor, holds the cutting tool, which cuts the work piece, so that the cutting
forces are generated which effects the spindle accuracy directly. The forces which are affecting the CNC machine tool
spindle are tangential force (Ft), feed force (Fc), radial force (Fr) and will be estimated. Based on maximum cutting
force incurred the analysis will be carried out. The main objective is to find the static, fatigue analysis of spindle
structure for maximum cutting force condition and predicting life of bearings. From static analysis stress and
deformation of the spindle can be found. Stress obtained from the stress analysis is less than the yield strength of the
material and deformation of the spindle is very less which can be neglected. Equivalent alternating stress, factor of
safety and life of the spindle is found by fatigue analysis and which results are closely matches with the analytical
value
Similar to Review of shaft failure in Coil Car Assembly (20)
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