The document discusses using motion simulation and finite element analysis (FEA) to analyze and optimize the design of an engine valve. It describes measuring and modeling a valvetrain in CAD software. A motion simulation is performed to analyze valve stress, displacement, rotation and reaction forces. The initial FEA results show the valve experiences maximum stress of 255 MPa, within the material strength. Modifications are made to reduce valve weight by decreasing diameter and using a titanium alloy, which experience increased stresses still within material limits. The goal is to improve engine performance through a lighter, higher strength valve design validated through virtual testing methods.
Yanmar 3 jh2 (b)e marine diesel engine service repair manualfjsekfsmeme
This document provides service information for the 3JH2 series marine diesel engines, including specifications, component diagrams, maintenance procedures, and troubleshooting guides. It has been revised twice to include additional engine models and technical updates. The manual covers general technical details, disassembly and repair of major engine systems, testing procedures, and part replacement torque specifications.
Liebherr lr 624 lr624 crawler loader series 4 litronic service repair manualhfjsejdkemmn
This document provides a table of contents for a service manual. It lists sub group indexes and sections covering topics such as general information, tools and application, technical data, maintenance guidelines, descriptions of engine, hydraulic, electrical and other systems, and attachments. The table of contents spans over 4 pages and includes over 170 entries organized by section number and title.
Liebherr lr 634 lr634 crawler loader series 4 litronic service repair manualregdfcgvdgvf
This document provides a table of contents for a service manual. It lists sub group indexes and sections covering topics such as general information, tools and application, technical data, maintenance guidelines, descriptions of engine, hydraulic, electrical and other systems, and attachments. The table of contents spans over 4 pages and includes over 170 entries organized by section number and title.
This thesis presents a position control method for a pneumatic actuation system. It first develops a dynamic model for the pneumatic actuator based on energy methods. It then applies a nonlinear backstepping control method to provide accurate trajectory tracking for the actuator despite disturbances from external forces varying between 250-1050 N. Simulation and experimental results on a test rig demonstrate the controller's excellent tracking of sinusoidal and square wave reference signals. An appendix also includes an original methodology for modeling the actuator's mass flow rate based on experimental identification.
This document is a textbook on electro-hydraulics that is divided into three parts. Part A provides an introduction and covers topics like hydraulic and electrical symbols, basic electro-hydraulic control systems, and exercises involving actuating cylinders and logic operations. Part B covers fundamentals of electro-hydraulic systems, electrical engineering, components, and safety. Part C contains solutions to the exercises. The book aims to teach basic and applied electro-hydraulics through explanations, diagrams, and practical exercises.
This document provides information about a textbook on pneumatics published by Festo Didactic GmbH & Co. It includes details such as the authors, publication date, copyright information, table of contents, and chapter summaries. The textbook covers topics such as characteristics of pneumatic systems, components, symbols and standards, development methods, and troubleshooting. It is intended to be used for training courses and self-study on pneumatics.
The document describes the steps to create a finite element model in ABAQUS. It involves pre-processing tasks like creating individual parts for the model, assigning material properties, assembling parts, applying loads and boundary conditions, and generating a mesh. Specific steps are provided to create each of the five parts that make up the model - the ceramic, cap, solder, copper, and PC board. Detailed instructions are given on creating the geometry of each part using the part module in ABAQUS. The document also outlines other pre-processing tasks like defining interactions and jobs before solving the model.
Audi was founded in 1909 by August Horch and was later merged with other companies to become Audi in 1932. In 1985 it was renamed Audi after being acquired by Volkswagen. Audi focuses on innovation, fuel cell vehicles, electric cars, and working with cities on sustainability. Its vision is "Advancement through Technology" and its strategies include creating long term customer relationships, customizing messages, ensuring satisfaction, and looking into complaints to build loyalty. This summary was prepared by an intern during their marketing internship under the guidance of a professor.
Yanmar 3 jh2 (b)e marine diesel engine service repair manualfjsekfsmeme
This document provides service information for the 3JH2 series marine diesel engines, including specifications, component diagrams, maintenance procedures, and troubleshooting guides. It has been revised twice to include additional engine models and technical updates. The manual covers general technical details, disassembly and repair of major engine systems, testing procedures, and part replacement torque specifications.
Liebherr lr 624 lr624 crawler loader series 4 litronic service repair manualhfjsejdkemmn
This document provides a table of contents for a service manual. It lists sub group indexes and sections covering topics such as general information, tools and application, technical data, maintenance guidelines, descriptions of engine, hydraulic, electrical and other systems, and attachments. The table of contents spans over 4 pages and includes over 170 entries organized by section number and title.
Liebherr lr 634 lr634 crawler loader series 4 litronic service repair manualregdfcgvdgvf
This document provides a table of contents for a service manual. It lists sub group indexes and sections covering topics such as general information, tools and application, technical data, maintenance guidelines, descriptions of engine, hydraulic, electrical and other systems, and attachments. The table of contents spans over 4 pages and includes over 170 entries organized by section number and title.
This thesis presents a position control method for a pneumatic actuation system. It first develops a dynamic model for the pneumatic actuator based on energy methods. It then applies a nonlinear backstepping control method to provide accurate trajectory tracking for the actuator despite disturbances from external forces varying between 250-1050 N. Simulation and experimental results on a test rig demonstrate the controller's excellent tracking of sinusoidal and square wave reference signals. An appendix also includes an original methodology for modeling the actuator's mass flow rate based on experimental identification.
This document is a textbook on electro-hydraulics that is divided into three parts. Part A provides an introduction and covers topics like hydraulic and electrical symbols, basic electro-hydraulic control systems, and exercises involving actuating cylinders and logic operations. Part B covers fundamentals of electro-hydraulic systems, electrical engineering, components, and safety. Part C contains solutions to the exercises. The book aims to teach basic and applied electro-hydraulics through explanations, diagrams, and practical exercises.
This document provides information about a textbook on pneumatics published by Festo Didactic GmbH & Co. It includes details such as the authors, publication date, copyright information, table of contents, and chapter summaries. The textbook covers topics such as characteristics of pneumatic systems, components, symbols and standards, development methods, and troubleshooting. It is intended to be used for training courses and self-study on pneumatics.
The document describes the steps to create a finite element model in ABAQUS. It involves pre-processing tasks like creating individual parts for the model, assigning material properties, assembling parts, applying loads and boundary conditions, and generating a mesh. Specific steps are provided to create each of the five parts that make up the model - the ceramic, cap, solder, copper, and PC board. Detailed instructions are given on creating the geometry of each part using the part module in ABAQUS. The document also outlines other pre-processing tasks like defining interactions and jobs before solving the model.
Audi was founded in 1909 by August Horch and was later merged with other companies to become Audi in 1932. In 1985 it was renamed Audi after being acquired by Volkswagen. Audi focuses on innovation, fuel cell vehicles, electric cars, and working with cities on sustainability. Its vision is "Advancement through Technology" and its strategies include creating long term customer relationships, customizing messages, ensuring satisfaction, and looking into complaints to build loyalty. This summary was prepared by an intern during their marketing internship under the guidance of a professor.
This document describes experimental studies of aeroelasticity conducted in a 30cm x 30cm wind tunnel. Divergence and flutter experiments were performed on a typical airfoil section model with pitch and plunge degrees of freedom. In the divergence experiment, the divergence speed was measured in the wind tunnel and calculated theoretically, with some difference observed likely due to model assumptions. In the flutter experiment, a data acquisition system was used to record acceleration data during testing, and a MATLAB code was used to analyze the data and calculate the flutter point, allowing comparison to theoretical predictions. Open loop control was also explored by adding a control surface to modify the flutter point.
Finite Element Analysis of Shaft of Centrifugal PumpIOSR Journals
Centrifugal pump is world one of the oldest water pumping devises. The current work deals study
Shaft of centrifugal pump for static and dynamic analysis. As we know rotodynamic machineries are designed
keenly as there is lot of fluctuation in the loads and speeds. The shaft is analyzed by using finite element analysis
technique for stresses and deflections. The total work is carried out in two stages first stage is static analysis. In
this stage pump shaft is analyzed for stresses and deflection and same results are verified using graphical
integration method. And second for dynamic analysis, in this stage result obtained by static analysis are used to
calculate dynamic forces coming in pump shaft. Again shaft is analyzed in dynamic input condition and results
are verified by using graphical integration method. The software used for the finite element meshing is
HYPERMESH and solver used is RADIOSS. Result values obtained for deflection and stresses are compared in
both cases. Result obtained by graphical method and FEA are nearly similar and are in acceptable limits.
The document describes a numerical simulation of flow through a centrifugal pump impeller. Hassan Adel Talaat El-Sheshtawy conducted 3D CFD simulations using ANSYS/CFX to analyze the flow field and evaluate the slip factor. The simulation results agreed well with the design performance curve, especially near the best efficiency point. Several empirical slip factor correlations were compared to the numerically obtained slip factor. The effects of adding splitters and increasing the number of blades on slip factor, head rise and hydraulic efficiency were also investigated. It was found that while slip factor improved with more blades or longer splitters, hydraulic efficiency did not always increase due to additional losses.
Experimental and numerical stress analysis of a rectangular wing structureLahiru Dilshan
Structures of an aircraft can be categorised as primary structural components and secondary structure components. Primary structure components are the components which lead to failure of the aircraft if such component is failed during the flight cycle. Secondary components are load sharing components in an aircraft but will not pave the way to catastrophic failure.
Designing aircraft structures should follow several strategies to assure safety. For that, there are three main methods used in designing and maintenance procedures. First one is the safe flight, which an aircraft component has a lifetime. That component is not used beyond that limit and should replace though it is not failed. The fail-safe method is another one that redundant systems or components are there to ensure there is another way to carry the load or do necessary control. The final one is the damage tolerance which measures the current damages are within acceptable limit and carry out the main functions until the next main maintenance process.
To determine the safety of a structure component load distribution, stress and strain variation, deflection can be used as parameters to make sure that component can withstand maximum allowable load with safety factor. There are several techniques used to get accurate results as numerical methods, Finite Element Method (FEM) and experimental methods. In the design process, those three steps are followed in an orderly manner to ensure the safety of an aircraft.
The document describes a project to automate the design of a single cylinder internal combustion engine using linked analysis and simulation software. Specifically, the project will design the connecting rod and crankshaft, perform motion and stress analysis, and create a Visual Basic interface to allow the user to modify design parameters in Excel and automatically update the Solidworks model and analysis results in MATLAB. The interface will optimize the design to achieve an acceptable factor of safety while minimizing shaking forces during operation.
Semi-Automatic Engine Valve Cleaning Machine Using Cam and Follower MechanismIRJET Journal
This document describes the design and development of a semi-automatic engine valve cleaning machine that uses a cam and follower mechanism. The machine aims to make the valve lapping process, which is currently time-consuming and labor-intensive, more efficient. The machine was modeled in CAD software and analyzed for stress and deformation using FEA. Testing showed the machine reduces the time taken for valve cleaning compared to manual methods. The automated design requires less human intervention and effort during maintenance of internal combustion engine valves.
The document discusses mesh analysis and computational fluid dynamics (CFD) simulations of internal combustion engines. It begins by explaining the process of mesh analysis, which involves breaking a geometry into nodes and solving governing equations at each node. It describes different mesh geometries and algorithms used in meshing. The document then discusses how CFD can be used to analyze engine phenomena like scavenging efficiency, trapping efficiency, and flame stretch through solving conservation equations. It provides examples of CFD simulations analyzing these properties by varying parameters. In conclusion, it emphasizes how CFD enables optimizing engine performance through studying various properties by changing inputs in simulations.
Final Project_ Design and FEM Analysis of Scissor JackMehmet Bariskan
The document describes the design and finite element analysis of a scissor jack. It includes an overview of scissor jack components and operation, as well as calculations of forces and stresses on members. A series of mesh refinement studies were performed on the carrier member, lifting arms, and shaft screw to determine maximum stresses and displacements under expected loading conditions.
This document presents a thesis on winglet design and optimization for unmanned aerial vehicles (UAVs). The author develops a vortex lattice method (VLM) based design methodology. Various winglet designs are modeled and evaluated using the VLM code Pecos. Physical winglet models are also tested in small-scale and full-scale wind tunnels. Results show that winglets can improve the aerodynamic efficiency of UAVs like the RQ7 Shadow and Predator A by reducing drag and increasing range. Future work may include further wind tunnel testing and evaluation of additional UAV platforms.
The document describes a regenerative braking system that uses a spiral torsion spring to store kinetic energy during vehicle braking. When braking, the kinetic energy is transferred to the spring, causing it to wind and store potential energy. This stored energy can then be used to assist in accelerating the vehicle by allowing the spring to unwind and transfer rotational energy to the wheels. A mathematical model of the system is developed in MATLAB to analyze the spring deflection and stresses over time. The goal of the system is to improve fuel efficiency by recovering braking energy for reuse during acceleration.
3-component force balance and angle of attack actuatorTobias Reichold
This document provides a summary of the final report for a 3rd year engineering project to construct a 3-component force balance and angle of attack actuator for a wind tunnel. It describes the manufacturing and assembly process, electronics system, control software, installation, and progress compared to the initial proposal. Many of the original components had design flaws and most manufacturing tasks needed to be redone. Key components constructed include a modified floating plate, gear assembly, potentiometer bracket, and electrical enclosure. The completed system will measure lift, drag and pitching forces on airfoils in the wind tunnel and allow remote control of the angle of attack.
This document discusses vehicle testing and data analysis for aerodynamic parameters. It begins with introductions to key aerodynamic principles like drag, lift, and boundary layer separation. It then describes the methodology for simulator testing of different wing angles of attack. Results and analysis are presented on coefficients of drag, lift, and lap performance for varying setups. The document concludes with recommendations for wing parameters and directions for further work.
This document discusses modeling a hot compression test using finite element analysis in ABAQUS. It describes:
1) Creating parts for the deformable bulk material and rigid press and assembling them, defining materials, contacts, steps, and meshing.
2) Developing a viscoplastic constitutive model and implementing it in ABAQUS through user subroutines UMAT and VUMAT.
3) Running a simulation of hot plain strain compression of copper and comparing results from UMAT and VUMAT.
FEATool Multiphysics Matlab FEM and CFD Toolbox - v1.6 Quickstart GuideFEATool Multiphysics
FEATool Multiphysics v1.6 Quickstart Guide
FEATool Multiphysics is a fully integrated and easy to use Matlab Multiphysics PDE and FEM Finite Element Analysis simulation toolbox, featuring built-in support for heat transfer, computational fluid dynamics CFD, chemical and reaction engineering, and structural mechanics modeling and simulation.
Visit https://www.featool.com for more information.
IRJET- Stress Analysis and Fatigue Failure of Typical Compressor ImpellerIRJET Journal
This document summarizes a study on the stress analysis, modal analysis, and fatigue failure analysis of a typical centrifugal compressor impeller. A 3D model of the impeller was created in Solid Edge and imported into ABAQUS for finite element analysis. Stress analysis found maximum stresses of 357 MPa, which could cause permanent deformation and reduce fatigue life. Modal analysis determined the first four natural frequencies and mode shapes. Fatigue analysis using the Goodman equation estimated a fatigue life of over 10^7 cycles for the impeller material of AL2618 based on an equivalent stress of 176 MPa. The analyses aimed to understand stresses and vibration modes that could lead to early fatigue failure of compressor impeller blades.
Computer Aided Design and Analysis of Load Deflection Behaviour Of Diaphragm ...IRJET Journal
1) The document analyzes the load deflection behavior of diaphragm springs used in clutch assemblies through computer aided design and finite element analysis.
2) A diaphragm spring is modeled in CATIA and analyzed in ANSYS to study deformation, stress, and force values under different loads and for various materials.
3) The analysis found aluminum alloy to have the lowest stress and reaction force values compared to magnesium alloy and mild steel under the same loading conditions, making it the best material for automotive clutch applications.
This document summarizes a study analyzing the design and material selection for a 245 KN resistant block crane hook. The study models a hook design using the alloy Alloy 1.2367 (X38CrMoV5-3) in Solidworks. Finite element analysis is conducted in Solidworks Simulation to analyze the hook's performance. The results show that with the new alloy, the maximum Von Mises stress of 2.04796e+07 N/m2 is well below the alloy's yield strength. The study concludes that Alloy 1.2367 (X38CrMoV5-3) can withstand the same loads as traditional materials but with reduced mass, making it a suitable replacement for crane hooks
The document summarizes the portfolio of Liu Huang, a master's student in mechanical engineering at UC Berkeley. It includes descriptions and analyses of several projects:
1. A flywheel-motor system for electric vehicles that can capture regenerative braking energy, improving efficiency by 60% and fuel economy by 15%. Analyses include bearing life calculation, glue strength calculation, FEA analysis, and control system design.
2. An air filtration system for asthma patients, including calculations of air pressure drop and flow rate, selection of fan and filter products, CAD modeling, and analyses of air velocity and pressure distribution in the mask.
3. A gearbox design for connecting a motor to a pump, including gear
IRJET- Weight Optimization of API 6D 12”-150 Class Plug Valve Body by Finite ...IRJET Journal
This document summarizes research conducted to optimize the weight of an API 6D 12”-150 class plug valve body through finite element analysis and experimental testing. A 3D model of the existing valve body was created in CATIA and meshed in ANSYS Workbench. Stress analysis was performed at working pressures of 290 PSI and test pressures of 325 PSI. Modifications including reducing wall and flange thicknesses and adding fillets resulted in approximately 6.4% weight reduction while maintaining safety factors above 1. Experimental strain gauge testing validated the FEA stress results.
The standard disc brake of a 4-wheeler model was done using Autodesk Mechanical Simulation through which the properties like deflection, heat flux and temperature of disc brake model were calculated. It is important to understand action force and friction force on the disc brake new material, how disc brake works more efficiently, which can help to reduce the accident that may happen at anytime.
This document describes experimental studies of aeroelasticity conducted in a 30cm x 30cm wind tunnel. Divergence and flutter experiments were performed on a typical airfoil section model with pitch and plunge degrees of freedom. In the divergence experiment, the divergence speed was measured in the wind tunnel and calculated theoretically, with some difference observed likely due to model assumptions. In the flutter experiment, a data acquisition system was used to record acceleration data during testing, and a MATLAB code was used to analyze the data and calculate the flutter point, allowing comparison to theoretical predictions. Open loop control was also explored by adding a control surface to modify the flutter point.
Finite Element Analysis of Shaft of Centrifugal PumpIOSR Journals
Centrifugal pump is world one of the oldest water pumping devises. The current work deals study
Shaft of centrifugal pump for static and dynamic analysis. As we know rotodynamic machineries are designed
keenly as there is lot of fluctuation in the loads and speeds. The shaft is analyzed by using finite element analysis
technique for stresses and deflections. The total work is carried out in two stages first stage is static analysis. In
this stage pump shaft is analyzed for stresses and deflection and same results are verified using graphical
integration method. And second for dynamic analysis, in this stage result obtained by static analysis are used to
calculate dynamic forces coming in pump shaft. Again shaft is analyzed in dynamic input condition and results
are verified by using graphical integration method. The software used for the finite element meshing is
HYPERMESH and solver used is RADIOSS. Result values obtained for deflection and stresses are compared in
both cases. Result obtained by graphical method and FEA are nearly similar and are in acceptable limits.
The document describes a numerical simulation of flow through a centrifugal pump impeller. Hassan Adel Talaat El-Sheshtawy conducted 3D CFD simulations using ANSYS/CFX to analyze the flow field and evaluate the slip factor. The simulation results agreed well with the design performance curve, especially near the best efficiency point. Several empirical slip factor correlations were compared to the numerically obtained slip factor. The effects of adding splitters and increasing the number of blades on slip factor, head rise and hydraulic efficiency were also investigated. It was found that while slip factor improved with more blades or longer splitters, hydraulic efficiency did not always increase due to additional losses.
Experimental and numerical stress analysis of a rectangular wing structureLahiru Dilshan
Structures of an aircraft can be categorised as primary structural components and secondary structure components. Primary structure components are the components which lead to failure of the aircraft if such component is failed during the flight cycle. Secondary components are load sharing components in an aircraft but will not pave the way to catastrophic failure.
Designing aircraft structures should follow several strategies to assure safety. For that, there are three main methods used in designing and maintenance procedures. First one is the safe flight, which an aircraft component has a lifetime. That component is not used beyond that limit and should replace though it is not failed. The fail-safe method is another one that redundant systems or components are there to ensure there is another way to carry the load or do necessary control. The final one is the damage tolerance which measures the current damages are within acceptable limit and carry out the main functions until the next main maintenance process.
To determine the safety of a structure component load distribution, stress and strain variation, deflection can be used as parameters to make sure that component can withstand maximum allowable load with safety factor. There are several techniques used to get accurate results as numerical methods, Finite Element Method (FEM) and experimental methods. In the design process, those three steps are followed in an orderly manner to ensure the safety of an aircraft.
The document describes a project to automate the design of a single cylinder internal combustion engine using linked analysis and simulation software. Specifically, the project will design the connecting rod and crankshaft, perform motion and stress analysis, and create a Visual Basic interface to allow the user to modify design parameters in Excel and automatically update the Solidworks model and analysis results in MATLAB. The interface will optimize the design to achieve an acceptable factor of safety while minimizing shaking forces during operation.
Semi-Automatic Engine Valve Cleaning Machine Using Cam and Follower MechanismIRJET Journal
This document describes the design and development of a semi-automatic engine valve cleaning machine that uses a cam and follower mechanism. The machine aims to make the valve lapping process, which is currently time-consuming and labor-intensive, more efficient. The machine was modeled in CAD software and analyzed for stress and deformation using FEA. Testing showed the machine reduces the time taken for valve cleaning compared to manual methods. The automated design requires less human intervention and effort during maintenance of internal combustion engine valves.
The document discusses mesh analysis and computational fluid dynamics (CFD) simulations of internal combustion engines. It begins by explaining the process of mesh analysis, which involves breaking a geometry into nodes and solving governing equations at each node. It describes different mesh geometries and algorithms used in meshing. The document then discusses how CFD can be used to analyze engine phenomena like scavenging efficiency, trapping efficiency, and flame stretch through solving conservation equations. It provides examples of CFD simulations analyzing these properties by varying parameters. In conclusion, it emphasizes how CFD enables optimizing engine performance through studying various properties by changing inputs in simulations.
Final Project_ Design and FEM Analysis of Scissor JackMehmet Bariskan
The document describes the design and finite element analysis of a scissor jack. It includes an overview of scissor jack components and operation, as well as calculations of forces and stresses on members. A series of mesh refinement studies were performed on the carrier member, lifting arms, and shaft screw to determine maximum stresses and displacements under expected loading conditions.
This document presents a thesis on winglet design and optimization for unmanned aerial vehicles (UAVs). The author develops a vortex lattice method (VLM) based design methodology. Various winglet designs are modeled and evaluated using the VLM code Pecos. Physical winglet models are also tested in small-scale and full-scale wind tunnels. Results show that winglets can improve the aerodynamic efficiency of UAVs like the RQ7 Shadow and Predator A by reducing drag and increasing range. Future work may include further wind tunnel testing and evaluation of additional UAV platforms.
The document describes a regenerative braking system that uses a spiral torsion spring to store kinetic energy during vehicle braking. When braking, the kinetic energy is transferred to the spring, causing it to wind and store potential energy. This stored energy can then be used to assist in accelerating the vehicle by allowing the spring to unwind and transfer rotational energy to the wheels. A mathematical model of the system is developed in MATLAB to analyze the spring deflection and stresses over time. The goal of the system is to improve fuel efficiency by recovering braking energy for reuse during acceleration.
3-component force balance and angle of attack actuatorTobias Reichold
This document provides a summary of the final report for a 3rd year engineering project to construct a 3-component force balance and angle of attack actuator for a wind tunnel. It describes the manufacturing and assembly process, electronics system, control software, installation, and progress compared to the initial proposal. Many of the original components had design flaws and most manufacturing tasks needed to be redone. Key components constructed include a modified floating plate, gear assembly, potentiometer bracket, and electrical enclosure. The completed system will measure lift, drag and pitching forces on airfoils in the wind tunnel and allow remote control of the angle of attack.
This document discusses vehicle testing and data analysis for aerodynamic parameters. It begins with introductions to key aerodynamic principles like drag, lift, and boundary layer separation. It then describes the methodology for simulator testing of different wing angles of attack. Results and analysis are presented on coefficients of drag, lift, and lap performance for varying setups. The document concludes with recommendations for wing parameters and directions for further work.
This document discusses modeling a hot compression test using finite element analysis in ABAQUS. It describes:
1) Creating parts for the deformable bulk material and rigid press and assembling them, defining materials, contacts, steps, and meshing.
2) Developing a viscoplastic constitutive model and implementing it in ABAQUS through user subroutines UMAT and VUMAT.
3) Running a simulation of hot plain strain compression of copper and comparing results from UMAT and VUMAT.
FEATool Multiphysics Matlab FEM and CFD Toolbox - v1.6 Quickstart GuideFEATool Multiphysics
FEATool Multiphysics v1.6 Quickstart Guide
FEATool Multiphysics is a fully integrated and easy to use Matlab Multiphysics PDE and FEM Finite Element Analysis simulation toolbox, featuring built-in support for heat transfer, computational fluid dynamics CFD, chemical and reaction engineering, and structural mechanics modeling and simulation.
Visit https://www.featool.com for more information.
IRJET- Stress Analysis and Fatigue Failure of Typical Compressor ImpellerIRJET Journal
This document summarizes a study on the stress analysis, modal analysis, and fatigue failure analysis of a typical centrifugal compressor impeller. A 3D model of the impeller was created in Solid Edge and imported into ABAQUS for finite element analysis. Stress analysis found maximum stresses of 357 MPa, which could cause permanent deformation and reduce fatigue life. Modal analysis determined the first four natural frequencies and mode shapes. Fatigue analysis using the Goodman equation estimated a fatigue life of over 10^7 cycles for the impeller material of AL2618 based on an equivalent stress of 176 MPa. The analyses aimed to understand stresses and vibration modes that could lead to early fatigue failure of compressor impeller blades.
Computer Aided Design and Analysis of Load Deflection Behaviour Of Diaphragm ...IRJET Journal
1) The document analyzes the load deflection behavior of diaphragm springs used in clutch assemblies through computer aided design and finite element analysis.
2) A diaphragm spring is modeled in CATIA and analyzed in ANSYS to study deformation, stress, and force values under different loads and for various materials.
3) The analysis found aluminum alloy to have the lowest stress and reaction force values compared to magnesium alloy and mild steel under the same loading conditions, making it the best material for automotive clutch applications.
This document summarizes a study analyzing the design and material selection for a 245 KN resistant block crane hook. The study models a hook design using the alloy Alloy 1.2367 (X38CrMoV5-3) in Solidworks. Finite element analysis is conducted in Solidworks Simulation to analyze the hook's performance. The results show that with the new alloy, the maximum Von Mises stress of 2.04796e+07 N/m2 is well below the alloy's yield strength. The study concludes that Alloy 1.2367 (X38CrMoV5-3) can withstand the same loads as traditional materials but with reduced mass, making it a suitable replacement for crane hooks
The document summarizes the portfolio of Liu Huang, a master's student in mechanical engineering at UC Berkeley. It includes descriptions and analyses of several projects:
1. A flywheel-motor system for electric vehicles that can capture regenerative braking energy, improving efficiency by 60% and fuel economy by 15%. Analyses include bearing life calculation, glue strength calculation, FEA analysis, and control system design.
2. An air filtration system for asthma patients, including calculations of air pressure drop and flow rate, selection of fan and filter products, CAD modeling, and analyses of air velocity and pressure distribution in the mask.
3. A gearbox design for connecting a motor to a pump, including gear
IRJET- Weight Optimization of API 6D 12”-150 Class Plug Valve Body by Finite ...IRJET Journal
This document summarizes research conducted to optimize the weight of an API 6D 12”-150 class plug valve body through finite element analysis and experimental testing. A 3D model of the existing valve body was created in CATIA and meshed in ANSYS Workbench. Stress analysis was performed at working pressures of 290 PSI and test pressures of 325 PSI. Modifications including reducing wall and flange thicknesses and adding fillets resulted in approximately 6.4% weight reduction while maintaining safety factors above 1. Experimental strain gauge testing validated the FEA stress results.
The standard disc brake of a 4-wheeler model was done using Autodesk Mechanical Simulation through which the properties like deflection, heat flux and temperature of disc brake model were calculated. It is important to understand action force and friction force on the disc brake new material, how disc brake works more efficiently, which can help to reduce the accident that may happen at anytime.
1. Motion Simulation and FEA
Benjamin Labrosse
BSc (Hons) Automotive Engineering
January 9, 2015
2. In the automotive world it is beneficial to understand the forces experienced by valves
in an engine. If a valve experiences too little stress it is considered to be over engineered
and be too heavy, reducing the potential performance of the engine. On the other hand,
if a valve experiences too large a stress the valve could bend excessively and fracture,
potentially causing damage to the engine. This leads to the aim of this paper where a
valvetrain has been measured and modelled in a CAD package and analysed through
FEA. The valve was modified according to the results of the FEA process to potentially
increase the performance of the engine.
4. List of Figures
2.0.1.The links and joints in the valvetrain model . . . . . . . . . . . . . . . . 6
2.0.2.Results of the spring dyno test . . . . . . . . . . . . . . . . . . . . . . . . 7
2.1.3.Degrees of freedom of a body, [Wang and Clarke, n,d] . . . . . . . . . . . 8
3.1.1.The maximum stress experienced by the valve . . . . . . . . . . . . . . . 10
3.1.2.The maximum stress experienced by the valve from a side view . . . . . . 11
3.2.3.The displacement of the valve under stress . . . . . . . . . . . . . . . . . 12
4.1.1.Maximum stress experienced by the valve . . . . . . . . . . . . . . . . . . 13
4.1.2.Second view of the maximum stress experienced by the valve . . . . . . . 14
4.1.3.The nodal displacement of the redesigned valve . . . . . . . . . . . . . . 14
4.2.4.The stress experienced by a titanium alloy valve . . . . . . . . . . . . . . 15
4.2.5.Nodal displacement of a titanium valve . . . . . . . . . . . . . . . . . . . 16
A.0.1.Applying a material property to the valve . . . . . . . . . . . . . . . . . 19
A.0.2.Applying a mesh collector . . . . . . . . . . . . . . . . . . . . . . . . . . 20
A.0.3.The application of the 3D Tetrahedral mesh . . . . . . . . . . . . . . . . 20
A.0.4.The mesh applied to the valve . . . . . . . . . . . . . . . . . . . . . . . . 21
A.0.5.The effect of the nodes on the valve . . . . . . . . . . . . . . . . . . . . . 21
4
5. 1. Introduction
Computer Aided Design (CAD) and Finite Element Analysis (FEA) play major roles in
the design of new components or the analysis of already existing components. Through
the use of these tools, an engineer can conclude whether a component is overly engi-
neered, that is, has been made with too much material or under engineered where a
component can be seen to fail. In both instances, the engineer can make modifications
to the component without making prototypes and completing live testing. This leads to
a reduced long term cost to the company in terms of finance and time.
The aim of this assignment is to measure and weigh real components from a system,
such as a valvetrain or suspension assembly, and create a CAD model of this system.
A motion simulation of this CAD model will be created and then a singular component
from the model will be put through an FEA. This will allow the author to modify the
CAD model as they believe fit, for example, modifying the dimensions of the component
in the model if too little or too much strain can be seen. The author has come to a
decision to model a valvetrain, consisting of a camshaft, bucket, collets, valve, spring,
spring retainer and a valve seat signifying the head of the engine. The CAD package
being used is Siemens NX8.5, created and sold by Siemens.
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6. 2. Methodology
The initial step to completing the aims of this assignment was to measure and weigh
the system chosen. The valvetrain components were measured using a vernier caliper
and weighed using scales. As there are small components in a valvetrain, high accuracy
low weight scales were used to measure the smaller components. Once the dimensions
of the valvetrain were obtained, the CAD model was created and assembled.
Figure 2.0.1.: The links and joints in the valvetrain model
As all parts were obtained from a matching head, the correct spring was available.
The spring was placed in the spring dyno to obtain the spring rate. A graph was made
showing the results from the test, see Figure 2.0.2. The spring rate was obtained from
the gradient of the graph and came out to be 13.13898N/mm.
The use of a vernier caliper is acceptable in the measurement of the majority of the
parts although this method is not suited to the measurement of the lobes. Had the
author known at the time, the measurement of the lobe would have been done by using
DTI gauges to get accurate measurements of the slope of the lobe. Using a vernier
caliper does not provide a true representation of the lobe profile. This unrealistic lobe
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7. Figure 2.0.2.: Results of the spring dyno test
profile does not allow the bucket to follow the lube therefore creating a phenomenon
called valve jump. This will lead to inaccuracies in the motion simulation but may not
effect the FEA results.
2.1. Motion simulation
The motion simulation was then completed by applying joints and links to the model,
seen in Figure 2.0.1. Links are used to group separate components that move together,
for example, in a valvetrain the collets, spring retainer, valve and spring all move together
when the camshaft pushes the bucket down. Joints are applied to the links to remove
the degrees of freedom (DOM) of the links therefore acting as constraints in the system.
Links are defined as a “rigid body with at least two points for attaching other links
(nodes)” and joints as a “connection between at least two links” by [Howe, 2006]. When
the motion simulation process commences, each component has six degrees of freedom.
The degrees of freedom in a model signify the parameters in which a body can move.
The body can move translationally in the planes x, y and z and rotationally in a, b and
g shown in Figure 2.1.3. In NX8.5, the degrees of freedom are denoted by the Grübler
count.
Table 2.1.1 shows the links created as well as the joints applied. Each joint has a base
link, the base link is the one about which each joint moves. In this case, the base link
of the revolute and slider joints is the valve seat as they move about the valve seat.
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8. Figure 2.1.3.: Degrees of freedom of a body, [Wang and Clarke, n,d]
Link Joints Reasoning
Cam Revolute The revolute joint allows the cam to
revolve and a driver was applied to it
Bucket/spring
retainer/collets/valve
Slider The slider joint allows a link to move
in one plane
Valve seat Fixed A fixed joint fixes the selected link in
space
Table 2.1.1.: The links and joints in the model
2.2. FEA
Material properties
The initial step to creating an FEA model is to apply material properties to the com-
ponents being analysed. In this case it is simple as there is only one component being
analysed meaning that only one material is present. As it is unknown what engine this
valvetrain has originated from, it has been assumed that the valve has been made from
4340 steel. Figure A.0.1 shows the window in which the user applies a material property.
Application of a mesh
The forces generated are applied to the mesh on the valve. Meshes are made up of nodes
and elements. The elements are the triangles visualized on screen and can be seen in
Figure A.0.4.
The first step to applying a mesh is to create a mesh collector. The mesh collector
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9. allows the user to apply different meshes to different materials. As there is only one
material in this FEA only one mesh collector needs to be added. The window used to
create a mesh collector is shown in Figure A.0.2.
The mesh is applied by selecting the 3D Tetrahedral mesh function. This applies a
mesh with elements taking the form of triangles. When creating a 3D mesh the user
must define in which mesh collector the mesh will be added. The element size must also
be selected. Element size varies depending on the parameters desired which is chosen by
the use of the component. Larger components typically have a larger elements, although
zones of smaller elements can be applied to more force sensitive areas. Siemens NX8.5
has a capability to automatically choose the element size which is derived from the area
of the component. The window for mesh creation is shown in Figure A.0.3 and shows
the desired mesh collector and element size which has been denoted automatically by
the software.
Once a mesh has been created, it will appear on screen as seen in Figure A.0.4. From
here, the load transfer data of the valve can be imported from the values obtained
previously in the spreadsheet.
Generation of nodes
After importing the load transfer of the valve, NX8.5 will generate two nodes in the
positions from which the forces are experienced. In this case, a node at the top of the
valve and at the bottom of the valve were generated. From the nodes, the user must
input the type of force being applied as well as the surfaces on which they are acting. The
surfaces on which the forces are applied at the top of the valve is shown in Figure A.0.5.
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10. 3. Analysis
CAD packages are made to visually exaggerate the effects of the forces produced in FEA.
As such, results obtained appear to show a greatly deformed valve but upon examination
are not very significant. The analysis has been completed assuming a cam speed of
4500RPM, meaning that the crank would be revolving at 9000RPM. This exceeds the
engine speed of the majority of road cars so knowing that the valve can tolerate this
speed ensures that the valve will not break under any speed.
3.1. Valve stress
The package has shown that the valve experiences a maximum force of 255.11N/mm2
. It
has been assumed that the valve is made of 4340 Alloy Steel. According to [AZO Mate-
rials, 2012], 4340 steel has a yield strength of 470MPa which is converted to 470N/mm2
.
The yield strength is the point at which the object begins to deform permanently. The
valve is therefore able to tolerate approximately twice that it is currently experiencing.
Figure 3.1.1.: The maximum stress experienced by the valve
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11. The bending that is experienced is seen near the bottom of the valve on the outer
extremity of the shaft, see Figure 3.1.2. The maximum stress is seen at this point as the
valve is bending at this point.
Figure 3.1.2.: The maximum stress experienced by the valve from a side view
3.2. Valve displacement
The valve experiences maximum bending when the maximum stress is seen. The max-
imum displacement is seen to be at the top of the valve where the collets sit meaning
that the tip of the valve is being bent away from the center line. This bending has a
maximum magnitude of 0.446mm. The tolerance of valves in the engine that this valve
originates is unknown but the author assumes that a valve has a larger tolerance to float.
This means that the valve would be able to bend more.
3.3. Valve rotation
The software provides information on the rotation of objects being FEA’d. This feature
is useful in components such as driveshafts as they are twisted under force. A valve
doesn’t rotate so the system has given a maximum angle of 0°.
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12. Figure 3.2.3.: The displacement of the valve under stress
3.4. Valve reaction force
The package has given a result for the reaction force on the valve as 5 × 10−10
N which
is negligible and can be ignored when designing the valve.
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13. 4. Modifications to improve the valve
design
4.1. Dimensions
In order to improve the valve, the author has decided to decrease the diameter of the
valve shank. The top of the valve has remained unmodified so that the interaction
between the bucket and the valve is unaltered. This reduces the weight of the valve
which means that the engine designer can include lighter springs in the valvetrain which
further reduces the weight. Reduced weight can increase the performance of the engine
as the valve is opened more quickly. A quicker opening of the valve will mean that the
Figure 4.1.1.: Maximum stress experienced by the valve
valve will be open longer than the original valve. This would allow more air/fuel to
be added to the cylinder. Less wear will be experienced so the longevity of the engine
will be increased as well as the performance. The increased longevity will reduce the
quantity of valves needed over the life cycle of the engine so less resources are needed.
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14. As predicted, the thinner shank has increased the stress experienced by the valve to
248MPa, see Figures 4.1.1 and 4.1.2. This stress remains within the tolerance of the
material, see Section 3.1, so the modification is acceptable.
Figure 4.1.2.: Second view of the maximum stress experienced by the valve
The maximum displacement of the nodes seen is 0.5mm which appears to be acceptable
as the tolerance of float of the valve in the head is larger than 0.5mm. This can be seen
in Figure 4.1.3.
Figure 4.1.3.: The nodal displacement of the redesigned valve
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15. Figure 4.2.4.: The stress experienced by a titanium alloy valve
4.2. Material
The author decided to make another modification to the original valve. The material
was changed from 4340 steel to a titanium alloy. Titanium is a lighter material than
steel and has a tensile strength of 880MPa, [Aerospace Specification Metals, Inc., n,d],
compared to 470MPa of 4340 steel. This means that the valve could be made thinner
than a steel valve and would have similar benefits to reducing the diameter of the valve.
Titanium is more expensive than steel however so is not usually used in road vehicles.
The titanium valve experiences the same maximum stress as a steel valve but a larger
bending is seen, see Figure 4.2.5. A nodal displacement increase of 0.3mm is seen so the
change of material is not beneficial in this application.
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17. 5. Conclusion
The aim of this assignment was to measure, model and FEA an existing system with
moving parts. The second aim was to then modify the component that was FEA’d to
improve it. A valvetrain has been modelled and the valve FEA’d. The valve was then
modified by changing the diameter of the valve shank and by changing the material of
the valve. The change in dimensions brought about that experienced a larger stress
but was within the capabilities of the material. The greater stress would increase the
performance of the engine without sacrificing the integrity of the valve. The change in
material provided conflicting results. Titanium has a greater yield strength according
to the FEA performed less favourably than steel as a greater bending is experienced by
a valve made of titanium than one made of steel.
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18. References
Aerospace Specification Metals, Inc. Titanium ti-6al-4v (grade 5), annealed, n,d. URL
http://asm.matweb.com/search/SpecificMaterial.asp?bassnum=MTP641.
AZO Materials. Aisi 4340 alloy steel (uns g43400), September 2012. URL http://www.
azom.com/article.aspx?ArticleID=6772#3.
Robert Howe. Linkages engineering sciences 51, 2006. URL http://isites.harvard.
edu/fs/docs/icb.topic192304.files/lectures/ES51-Lecture-34-04-links-1.
pdf.
Dr. X Wang and Dr. T A Clarke. Determination of the six dof parameters of cad-based
objects. Technical report, City University London, n,d.
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19. A. Figures for the FEA and motion
simulation processes
Figure A.0.1.: Applying a material property to the valve
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20. Figure A.0.2.: Applying a mesh collector
Figure A.0.3.: The application of the 3D Tetrahedral mesh
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21. Figure A.0.4.: The mesh applied to the valve
Figure A.0.5.: The effect of the nodes on the valve
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