The document provides an overview of dynamics of engine mechanisms. It discusses key topics like dynamics force analysis, inertia forces, D'Alembert's principle, velocity and acceleration analysis of reciprocating engines using graphical and analytical methods, turning moment diagrams, work done per cycle, flywheel analysis and cam dynamics. The document contains examples of force analysis on reciprocating parts of an engine, dimensions of flywheel rim, and operation of flywheel in punching press. It also provides questions for practice on related concepts.
The document discusses the fundamentals of theory of machines and its subdivisions. It covers the following key points:
1. Theory of machines deals with the study of relative motion between machine parts and forces acting on them. It is subdivided into kinematics, dynamics, kinetics, and statics.
2. Kinematics studies relative motion, dynamics studies forces and their effects on moving parts, kinetics studies inertia forces, and statics studies forces on stationary parts.
3. Fundamental concepts like space, time, matter, body, mass, and force are defined. Newton's laws of motion are also summarized.
4. Methods for analyzing reciprocating engines like graphical and analytical methods are outlined. Forces
1. The document discusses the dynamics of machines and introduces the key concepts of kinematics, dynamics, kinetics, and statics as the four main branches of the theory of machines.
2. It then discusses static and dynamic force analysis and introduces concepts like inertia forces and torques. D'Alembert's principle is explained which states that inertia and external forces together result in static equilibrium.
3. Methods for dynamic analysis of reciprocating engines like graphical and analytical methods are introduced. Key forces on reciprocating parts like piston effort, connecting rod force, thrust, crank pin effort, and crank effort are defined.
The document discusses the thermo-mechanical analysis of a crankcase for a six cylinder truck diesel engine. It outlines the process of identifying loads from combustion, inertia, thermal effects and assembly and applying them in a finite element analysis of the crankcase. The analysis seeks to determine the durability and fatigue life of the crankcase under the varying operating loads of the engine.
Mechanics was among the first of the exact sciences to be developed. Its internal beauty as a mathematical discipline and its early remarkable success in accounting in quantitative detail for the motions of the Moon, Earth, and other planetary bodies had enormous influence on philosophical thought and provided impetus for the systematic development of science.
Mechanics may be divided into three branches: statics, which deals with forces acting on and in a body at rest; kinematics, which describes the possible motions of a body or system of bodies; and kinetics, which attempts to explain or predict the motion that will occur in a given situation. Alternatively, mechanics may be divided according to the kind of system studied. The simplest mechanical system is the particle, defined as a body so small that its shape and internal structure are of no consequence in the given problem. More complicated is the motion of a system of two or more particles that exert forces on one another and possibly undergo forces exerted by bodies outside of the system.
The principles of mechanics have been applied to three general realms of phenomena. The motions of such celestial bodies as stars, planets, and satellites can be predicted with great accuracy thousands of years before they occur. (The theory of relativity predicts some deviations from the motion according to classical, or Newtonian, mechanics; however, these are so small as to be observable only with very accurate techniques, except in problems involving all or a large portion of the detectable universe.) As the second realm, ordinary objects on Earth down to microscopic size (moving at speeds much lower than that of light) are properly described by classical mechanics without significant corrections. The engineer who designs bridges or aircraft may use the Newtonian laws of classical mechanics with confidence, even though the forces may be very complicated, and the calculations lack the beautiful simplicity of celestial mechanics. The third realm of phenomena comprises the behaviour of matter and ele
Forward and Reverse Motoring of DC Hoist Motor on Container Crane (CC) OperationIJERA Editor
Container cranes (CC) become the highest electric energy consumption equipment in container terminal. Therefore it is important to study and analyze the hoist motor as the largest motor on container crane operation to look for opportunities in use energy efficiently. Lifting and lowering the container as the fixed operation of CC. Lifting the container as forward operating of hoist motor and lowering the container as reverse operating of hoist motor. The type of DC motor have used to modelling. Simulink (one of Matlab toolboxes) was used to model the forward and reverse of DC hoist motor. When lifting the container (forward motoring), the current required depends on the applied load torque. But when lowering the containers (reverse motoring), the voltage generated by the engine polarity reverse is determined by the downward movement of containers (mass and height). Reverse the polarity, and let the motor functions as a generator, produces a current and then the potential energy was calculated. Conclusions were drawn at the end of the paper.
This document provides an introduction to kinematics of machines. It defines key terms like kinematics, mechanisms, machines, degrees of freedom, and types of links and motion. It also describes different types of kinematic pairs that constrain relative motion between links, including lower pairs like sliding and revolute pairs, and higher pairs. The main topics covered are the basic concepts, definitions, and analytical tools used in the kinematic analysis of machines.
1) The document describes an experiment conducted to determine the moment of inertia of a flywheel. Measurements were taken of the time required for different masses attached to the flywheel to complete a set number of revolutions.
2) The theoretical moment of inertia was calculated based on the flywheel's dimensions and material. This was compared to values calculated from the experimental data.
3) It was found that generally the theoretical and experimental results differed somewhat. This was attributed to factors like human error in taking measurements and the age of the engine used.
The document discusses the fundamentals of theory of machines and its subdivisions. It covers the following key points:
1. Theory of machines deals with the study of relative motion between machine parts and forces acting on them. It is subdivided into kinematics, dynamics, kinetics, and statics.
2. Kinematics studies relative motion, dynamics studies forces and their effects on moving parts, kinetics studies inertia forces, and statics studies forces on stationary parts.
3. Fundamental concepts like space, time, matter, body, mass, and force are defined. Newton's laws of motion are also summarized.
4. Methods for analyzing reciprocating engines like graphical and analytical methods are outlined. Forces
1. The document discusses the dynamics of machines and introduces the key concepts of kinematics, dynamics, kinetics, and statics as the four main branches of the theory of machines.
2. It then discusses static and dynamic force analysis and introduces concepts like inertia forces and torques. D'Alembert's principle is explained which states that inertia and external forces together result in static equilibrium.
3. Methods for dynamic analysis of reciprocating engines like graphical and analytical methods are introduced. Key forces on reciprocating parts like piston effort, connecting rod force, thrust, crank pin effort, and crank effort are defined.
The document discusses the thermo-mechanical analysis of a crankcase for a six cylinder truck diesel engine. It outlines the process of identifying loads from combustion, inertia, thermal effects and assembly and applying them in a finite element analysis of the crankcase. The analysis seeks to determine the durability and fatigue life of the crankcase under the varying operating loads of the engine.
Mechanics was among the first of the exact sciences to be developed. Its internal beauty as a mathematical discipline and its early remarkable success in accounting in quantitative detail for the motions of the Moon, Earth, and other planetary bodies had enormous influence on philosophical thought and provided impetus for the systematic development of science.
Mechanics may be divided into three branches: statics, which deals with forces acting on and in a body at rest; kinematics, which describes the possible motions of a body or system of bodies; and kinetics, which attempts to explain or predict the motion that will occur in a given situation. Alternatively, mechanics may be divided according to the kind of system studied. The simplest mechanical system is the particle, defined as a body so small that its shape and internal structure are of no consequence in the given problem. More complicated is the motion of a system of two or more particles that exert forces on one another and possibly undergo forces exerted by bodies outside of the system.
The principles of mechanics have been applied to three general realms of phenomena. The motions of such celestial bodies as stars, planets, and satellites can be predicted with great accuracy thousands of years before they occur. (The theory of relativity predicts some deviations from the motion according to classical, or Newtonian, mechanics; however, these are so small as to be observable only with very accurate techniques, except in problems involving all or a large portion of the detectable universe.) As the second realm, ordinary objects on Earth down to microscopic size (moving at speeds much lower than that of light) are properly described by classical mechanics without significant corrections. The engineer who designs bridges or aircraft may use the Newtonian laws of classical mechanics with confidence, even though the forces may be very complicated, and the calculations lack the beautiful simplicity of celestial mechanics. The third realm of phenomena comprises the behaviour of matter and ele
Forward and Reverse Motoring of DC Hoist Motor on Container Crane (CC) OperationIJERA Editor
Container cranes (CC) become the highest electric energy consumption equipment in container terminal. Therefore it is important to study and analyze the hoist motor as the largest motor on container crane operation to look for opportunities in use energy efficiently. Lifting and lowering the container as the fixed operation of CC. Lifting the container as forward operating of hoist motor and lowering the container as reverse operating of hoist motor. The type of DC motor have used to modelling. Simulink (one of Matlab toolboxes) was used to model the forward and reverse of DC hoist motor. When lifting the container (forward motoring), the current required depends on the applied load torque. But when lowering the containers (reverse motoring), the voltage generated by the engine polarity reverse is determined by the downward movement of containers (mass and height). Reverse the polarity, and let the motor functions as a generator, produces a current and then the potential energy was calculated. Conclusions were drawn at the end of the paper.
This document provides an introduction to kinematics of machines. It defines key terms like kinematics, mechanisms, machines, degrees of freedom, and types of links and motion. It also describes different types of kinematic pairs that constrain relative motion between links, including lower pairs like sliding and revolute pairs, and higher pairs. The main topics covered are the basic concepts, definitions, and analytical tools used in the kinematic analysis of machines.
1) The document describes an experiment conducted to determine the moment of inertia of a flywheel. Measurements were taken of the time required for different masses attached to the flywheel to complete a set number of revolutions.
2) The theoretical moment of inertia was calculated based on the flywheel's dimensions and material. This was compared to values calculated from the experimental data.
3) It was found that generally the theoretical and experimental results differed somewhat. This was attributed to factors like human error in taking measurements and the age of the engine used.
The effect of rotor disc clearance on the lift performance of contra rotating...eSAT Publishing House
IJRET : International Journal of Research in Engineering and Technology is an international peer reviewed, online journal published by eSAT Publishing House for the enhancement of research in various disciplines of Engineering and Technology. The aim and scope of the journal is to provide an academic medium and an important reference for the advancement and dissemination of research results that support high-level learning, teaching and research in the fields of Engineering and Technology. We bring together Scientists, Academician, Field Engineers, Scholars and Students of related fields of Engineering and Technology
Week 10 part 3 pe 6282 mecchanical liquid and electricalCharlton Inao
The document discusses mechanical modeling of systems. It provides instructional objectives of reviewing fundamentals, constructing mathematical models, and solving practical examples. It then defines systems modeling and discusses modeling dynamic systems using lumped parameters like springs, dampers, and masses. Analogous quantities between mechanical, electrical, pneumatic and hydraulic systems are also presented to model different system types.
The document provides a project report on the design and fabrication of a power hammer. It includes sections on the introduction, history and development of power hammers, experimental work conducted, design calculations, operation sheets, cost estimation, drawings, and conclusions. The project was carried out by 5 students under the guidance of Mr. Pavan M. Bhatt to design a simple mechanically operated power hammer applying principles of kinematic arrangement and machine design.
The document contains definitions and concepts related to kinematics and machine elements. It defines terms like kinematic link, structure, higher pair, kinematic chain, kinematic pair, mechanism, inversion, and types of kinematic chains. It also discusses concepts related to velocity and acceleration analysis, gears, belts, clutches, brakes, bearings, cams, vibration, and balancing of rotating masses.
This document describes a design for a piezoelectric shock absorber that can generate electricity from vehicle vibrations. It discusses two initial designs - electromagnetic and hydraulic - and proposes using a piezoelectric crystal installed within the shock absorber. When compressed, the crystal generates electric energy from the force. The design aims to limit the force on the crystal for safety while still producing optimal voltage. Analysis shows the design could generate over 25V from manual impacts. The piezoelectric shock absorber could increase fuel efficiency in hybrids or power accessories in other vehicles.
A landing gear assembly consists of various components viz. Lower side stay, Upperside stay, Locking actuators, Extension actuators, Tyres, and Locking pins to name a few. Each unit having a specific operation to deal with, in this project the main unit being studied is the lower brace. The primary objective is to analyse stresses in the element of the lower brace unit using strength of materials or RDM method and Finite Element Method (FEM) and compare both. Using the obtained data a suitable material is proposed for the component. The approach used here is to study the overall behaviour of the element by taking up each aspect, finally summing up the total effect of all the aspects in the functioning of the element.
15723120156. Measurement of Force and Torque.pdfKhalil Alhatab
This document discusses various methods of measuring force and torque. It describes several common force and torque measurement devices. Scales, spring scales, cantilever beams, load cells, and dynamometers are some of the main instruments covered. Load cells can operate hydraulically, pneumatically, or with strain gauges to translate an applied force into a pressure or electrical resistance measurement. Dynamometers discussed include Prony brakes, rope brakes, hydraulic dynamometers, and eddy current dynamometers, which all work to absorb the power output of an engine being tested.
Detailed design procedure for solar panel mounting structure with dual axis tracking capability for Sub urban West Bengal(Wind load calculation have been done for this region only).
This document presents an investigation of the behavior of 3 degree of freedom spring mass damper systems subjected to transient loads. Two models of the spring mass damper system are modeled and their governing equations are derived. The velocities of the oscillators are estimated by solving the governing equations for a loss factor of 0.15. The kinetic and potential energies are calculated using the mass, velocity and stiffness of the oscillators to estimate the total energy. It is found that when the load changes from full to partial over time, there is a significant increase in displacement and velocity, dissipating more energy.
This document discusses investigating the behavior of a 3 degree of freedom spring mass damper system subjected to transient loads. It presents two models of the system with different damper configurations and derives the governing equations. The velocities and energies (kinetic and potential) of the oscillators are estimated by solving the equations for an exponential decaying, constant, and partial load over time. The results show the contribution of kinetic energy is minimal for oscillator 2 in all cases, while potential energy and contributions from oscillators 1 and 3 depend on the load type.
Design and Analysis of Auger in KAMCO Power Tillerinventy
Research Inventy : International Journal of Engineering and Science is published by the group of young academic and industrial researchers with 12 Issues per year. It is an online as well as print version open access journal that provides rapid publication (monthly) of articles in all areas of the subject such as: civil, mechanical, chemical, electronic and computer engineering as well as production and information technology. The Journal welcomes the submission of manuscripts that meet the general criteria of significance and scientific excellence. Papers will be published by rapid process within 20 days after acceptance and peer review process takes only 7 days. All articles published in Research Inventy will be peer-reviewed.
lec3 Direct Stiffness Approach for Beams and Frames.pptShaheerRizwan1
This document outlines the procedure for analyzing beams and frames using the direct stiffness method. It discusses:
1) Dividing the structure into finite elements and defining nodes with degrees of freedom. Forces and deformations are defined at nodes.
2) Calculating the structure stiffness matrix of each element based on its properties.
3) Assembling the overall structure stiffness matrix. Equations are set up relating known/unknown loads and displacements to solve for unknowns.
4) Computing element forces from the determined displacements using appropriate transformation matrices for each element type. Bending moment and shear force diagrams can then be plotted.
COMPARISON OF RESPONSE TO UNBALANCE OF OVERHUNG ROTOR SYSTEM FOR DIFFERENT SU...IAEME Publication
Rotor unbalance is most common fault found in the rotating machines. Methods
are adopted to analyze the position of unbalance and to bring its effect into acceptablelimit. Vibration analysis is the most common technique used to analyze the rotor
system. Research have been performed on rotor supported atboth ends, however lessstudy has been done for overhung rotor. In this paper the response of overhung rotoron isotropic support and anisotropic support subject tounbalance has been presented.and equations aresolved using MATLAB programming. The effect of unbalancehas been studied on thebode plot. Forward and Reverse whirl are observed through Campbell diagram andmode shapes are plotted.
International Journal of Computational Engineering Research(IJCER) is an intentional online Journal in English monthly publishing journal. This Journal publish original research work that contributes significantly to further the scientific knowledge in engineering and Technology
Slider Crank Mechanism for Four bar linkageijsrd.com
the slider crank mechanism is a particular four bar linkage configuration that exhibits both linear and rotational motion simultaneously. This mechanism is frequently utilized in undergraduate engineering courses to investigate machine kinematics and resulting dynamic forces. The position, velocity, acceleration and shaking forces generated by a slider crank mechanism during operation can be determined analytically. Certain factors are often neglected from analytical calculations, causing results to differ from experimental data. The study of these slight variances produces useful insight. The following report details the successful design, fabrication and testing of a pneumatically powered slider crank mechanism for the purpose of classroom demonstration and experimentation. Transducers mounted to the mechanism record kinematic and dynamic force data during operation, which can then be compared to analytical values. The mechanism is capable of operating in balanced and unbalanced configurations so that the magnitude of shaking forces can be compared. The engine was successfully manufactured and operates as intended. Data recorded by the device's accelerometers is comparable to calculated values of acceleration and shaking force.
This document presents a detailed modelling and analysis of parasitic effects in the dynamics of multi-rotor hovercrafts. It focuses on modelling these effects for a T-configuration tri-rotor hovercraft called a T-Copter. The parasitic effects modelled include air drag moments, tilt reaction moments, precession moments, and various angular acceleration effects like Coriolis and centripetal accelerations. Equations are developed to model these effects based on the hardware configuration and dynamics of the T-Copter system. Experimental data is also used to generate polynomial functions modelling the air drag moments.
The effect of rotor disc clearance on the lift performance of contra rotating...eSAT Publishing House
IJRET : International Journal of Research in Engineering and Technology is an international peer reviewed, online journal published by eSAT Publishing House for the enhancement of research in various disciplines of Engineering and Technology. The aim and scope of the journal is to provide an academic medium and an important reference for the advancement and dissemination of research results that support high-level learning, teaching and research in the fields of Engineering and Technology. We bring together Scientists, Academician, Field Engineers, Scholars and Students of related fields of Engineering and Technology
Week 10 part 3 pe 6282 mecchanical liquid and electricalCharlton Inao
The document discusses mechanical modeling of systems. It provides instructional objectives of reviewing fundamentals, constructing mathematical models, and solving practical examples. It then defines systems modeling and discusses modeling dynamic systems using lumped parameters like springs, dampers, and masses. Analogous quantities between mechanical, electrical, pneumatic and hydraulic systems are also presented to model different system types.
The document provides a project report on the design and fabrication of a power hammer. It includes sections on the introduction, history and development of power hammers, experimental work conducted, design calculations, operation sheets, cost estimation, drawings, and conclusions. The project was carried out by 5 students under the guidance of Mr. Pavan M. Bhatt to design a simple mechanically operated power hammer applying principles of kinematic arrangement and machine design.
The document contains definitions and concepts related to kinematics and machine elements. It defines terms like kinematic link, structure, higher pair, kinematic chain, kinematic pair, mechanism, inversion, and types of kinematic chains. It also discusses concepts related to velocity and acceleration analysis, gears, belts, clutches, brakes, bearings, cams, vibration, and balancing of rotating masses.
This document describes a design for a piezoelectric shock absorber that can generate electricity from vehicle vibrations. It discusses two initial designs - electromagnetic and hydraulic - and proposes using a piezoelectric crystal installed within the shock absorber. When compressed, the crystal generates electric energy from the force. The design aims to limit the force on the crystal for safety while still producing optimal voltage. Analysis shows the design could generate over 25V from manual impacts. The piezoelectric shock absorber could increase fuel efficiency in hybrids or power accessories in other vehicles.
A landing gear assembly consists of various components viz. Lower side stay, Upperside stay, Locking actuators, Extension actuators, Tyres, and Locking pins to name a few. Each unit having a specific operation to deal with, in this project the main unit being studied is the lower brace. The primary objective is to analyse stresses in the element of the lower brace unit using strength of materials or RDM method and Finite Element Method (FEM) and compare both. Using the obtained data a suitable material is proposed for the component. The approach used here is to study the overall behaviour of the element by taking up each aspect, finally summing up the total effect of all the aspects in the functioning of the element.
15723120156. Measurement of Force and Torque.pdfKhalil Alhatab
This document discusses various methods of measuring force and torque. It describes several common force and torque measurement devices. Scales, spring scales, cantilever beams, load cells, and dynamometers are some of the main instruments covered. Load cells can operate hydraulically, pneumatically, or with strain gauges to translate an applied force into a pressure or electrical resistance measurement. Dynamometers discussed include Prony brakes, rope brakes, hydraulic dynamometers, and eddy current dynamometers, which all work to absorb the power output of an engine being tested.
Detailed design procedure for solar panel mounting structure with dual axis tracking capability for Sub urban West Bengal(Wind load calculation have been done for this region only).
This document presents an investigation of the behavior of 3 degree of freedom spring mass damper systems subjected to transient loads. Two models of the spring mass damper system are modeled and their governing equations are derived. The velocities of the oscillators are estimated by solving the governing equations for a loss factor of 0.15. The kinetic and potential energies are calculated using the mass, velocity and stiffness of the oscillators to estimate the total energy. It is found that when the load changes from full to partial over time, there is a significant increase in displacement and velocity, dissipating more energy.
This document discusses investigating the behavior of a 3 degree of freedom spring mass damper system subjected to transient loads. It presents two models of the system with different damper configurations and derives the governing equations. The velocities and energies (kinetic and potential) of the oscillators are estimated by solving the equations for an exponential decaying, constant, and partial load over time. The results show the contribution of kinetic energy is minimal for oscillator 2 in all cases, while potential energy and contributions from oscillators 1 and 3 depend on the load type.
Design and Analysis of Auger in KAMCO Power Tillerinventy
Research Inventy : International Journal of Engineering and Science is published by the group of young academic and industrial researchers with 12 Issues per year. It is an online as well as print version open access journal that provides rapid publication (monthly) of articles in all areas of the subject such as: civil, mechanical, chemical, electronic and computer engineering as well as production and information technology. The Journal welcomes the submission of manuscripts that meet the general criteria of significance and scientific excellence. Papers will be published by rapid process within 20 days after acceptance and peer review process takes only 7 days. All articles published in Research Inventy will be peer-reviewed.
lec3 Direct Stiffness Approach for Beams and Frames.pptShaheerRizwan1
This document outlines the procedure for analyzing beams and frames using the direct stiffness method. It discusses:
1) Dividing the structure into finite elements and defining nodes with degrees of freedom. Forces and deformations are defined at nodes.
2) Calculating the structure stiffness matrix of each element based on its properties.
3) Assembling the overall structure stiffness matrix. Equations are set up relating known/unknown loads and displacements to solve for unknowns.
4) Computing element forces from the determined displacements using appropriate transformation matrices for each element type. Bending moment and shear force diagrams can then be plotted.
COMPARISON OF RESPONSE TO UNBALANCE OF OVERHUNG ROTOR SYSTEM FOR DIFFERENT SU...IAEME Publication
Rotor unbalance is most common fault found in the rotating machines. Methods
are adopted to analyze the position of unbalance and to bring its effect into acceptablelimit. Vibration analysis is the most common technique used to analyze the rotor
system. Research have been performed on rotor supported atboth ends, however lessstudy has been done for overhung rotor. In this paper the response of overhung rotoron isotropic support and anisotropic support subject tounbalance has been presented.and equations aresolved using MATLAB programming. The effect of unbalancehas been studied on thebode plot. Forward and Reverse whirl are observed through Campbell diagram andmode shapes are plotted.
International Journal of Computational Engineering Research(IJCER) is an intentional online Journal in English monthly publishing journal. This Journal publish original research work that contributes significantly to further the scientific knowledge in engineering and Technology
Slider Crank Mechanism for Four bar linkageijsrd.com
the slider crank mechanism is a particular four bar linkage configuration that exhibits both linear and rotational motion simultaneously. This mechanism is frequently utilized in undergraduate engineering courses to investigate machine kinematics and resulting dynamic forces. The position, velocity, acceleration and shaking forces generated by a slider crank mechanism during operation can be determined analytically. Certain factors are often neglected from analytical calculations, causing results to differ from experimental data. The study of these slight variances produces useful insight. The following report details the successful design, fabrication and testing of a pneumatically powered slider crank mechanism for the purpose of classroom demonstration and experimentation. Transducers mounted to the mechanism record kinematic and dynamic force data during operation, which can then be compared to analytical values. The mechanism is capable of operating in balanced and unbalanced configurations so that the magnitude of shaking forces can be compared. The engine was successfully manufactured and operates as intended. Data recorded by the device's accelerometers is comparable to calculated values of acceleration and shaking force.
This document presents a detailed modelling and analysis of parasitic effects in the dynamics of multi-rotor hovercrafts. It focuses on modelling these effects for a T-configuration tri-rotor hovercraft called a T-Copter. The parasitic effects modelled include air drag moments, tilt reaction moments, precession moments, and various angular acceleration effects like Coriolis and centripetal accelerations. Equations are developed to model these effects based on the hardware configuration and dynamics of the T-Copter system. Experimental data is also used to generate polynomial functions modelling the air drag moments.
Similar to Dynamics of Machines_Module I.pptx (20)
Literature Review Basics and Understanding Reference Management.pptxDr Ramhari Poudyal
Three-day training on academic research focuses on analytical tools at United Technical College, supported by the University Grant Commission, Nepal. 24-26 May 2024
International Conference on NLP, Artificial Intelligence, Machine Learning an...gerogepatton
International Conference on NLP, Artificial Intelligence, Machine Learning and Applications (NLAIM 2024) offers a premier global platform for exchanging insights and findings in the theory, methodology, and applications of NLP, Artificial Intelligence, Machine Learning, and their applications. The conference seeks substantial contributions across all key domains of NLP, Artificial Intelligence, Machine Learning, and their practical applications, aiming to foster both theoretical advancements and real-world implementations. With a focus on facilitating collaboration between researchers and practitioners from academia and industry, the conference serves as a nexus for sharing the latest developments in the field.
A review on techniques and modelling methodologies used for checking electrom...nooriasukmaningtyas
The proper function of the integrated circuit (IC) in an inhibiting electromagnetic environment has always been a serious concern throughout the decades of revolution in the world of electronics, from disjunct devices to today’s integrated circuit technology, where billions of transistors are combined on a single chip. The automotive industry and smart vehicles in particular, are confronting design issues such as being prone to electromagnetic interference (EMI). Electronic control devices calculate incorrect outputs because of EMI and sensors give misleading values which can prove fatal in case of automotives. In this paper, the authors have non exhaustively tried to review research work concerned with the investigation of EMI in ICs and prediction of this EMI using various modelling methodologies and measurement setups.
Harnessing WebAssembly for Real-time Stateless Streaming PipelinesChristina Lin
Traditionally, dealing with real-time data pipelines has involved significant overhead, even for straightforward tasks like data transformation or masking. However, in this talk, we’ll venture into the dynamic realm of WebAssembly (WASM) and discover how it can revolutionize the creation of stateless streaming pipelines within a Kafka (Redpanda) broker. These pipelines are adept at managing low-latency, high-data-volume scenarios.
Advanced control scheme of doubly fed induction generator for wind turbine us...IJECEIAES
This paper describes a speed control device for generating electrical energy on an electricity network based on the doubly fed induction generator (DFIG) used for wind power conversion systems. At first, a double-fed induction generator model was constructed. A control law is formulated to govern the flow of energy between the stator of a DFIG and the energy network using three types of controllers: proportional integral (PI), sliding mode controller (SMC) and second order sliding mode controller (SOSMC). Their different results in terms of power reference tracking, reaction to unexpected speed fluctuations, sensitivity to perturbations, and resilience against machine parameter alterations are compared. MATLAB/Simulink was used to conduct the simulations for the preceding study. Multiple simulations have shown very satisfying results, and the investigations demonstrate the efficacy and power-enhancing capabilities of the suggested control system.
We have compiled the most important slides from each speaker's presentation. This year’s compilation, available for free, captures the key insights and contributions shared during the DfMAy 2024 conference.
1. BME 502 1
By
Dr. Manvandra Kumar Singh
(Ph.D., M.Tech. & B.Tech.)
Assistant Professor
Department of Mechanical Engineering
Amity School of Engineering & Technology
Amity University, Madhya Pradesh
12/23/2022
MODULE – I
DYNAMICS OF ENGINE MECHANISMS
3. BME 502 3
Introduction
The subject Theory of Machines may be
defined as that branch of Engineering science,
which deals with the study of relative motion
between the various parts of a machine, and
forces which act on them.
The knowledge of this
essential for an engineer in designing
subject is very
the
various parts of a machine.
12/23/2022
4. BME 502 4
Sub-divisions of Theory of
Machines
The Theory of Machines may be sub-
divided into the following four branches :
1. Kinematics
2. Dynamics
3. Kinetics
4. Statics
12/23/2022
5. BME 502 5
1. Kinematics
It is that branch of Theory of Machines
which deals with the relative motion between
the various parts of the machines.
2. Dynamics
It is that branch of Theory of Machines
which deals with the forces and their effects,
while acting upon the machine parts in motion.
Sub-divisions of Theory of
Machines
12/23/2022
6. BME 502 6
Sub-divisions of Theory of
Machines
3. Kinetics
It is that branch of Theory of Machines
which deals with the inertia forces which arise
from the combined effect of the mass and
motion of the machine parts.
12/23/2022
7. BME 502 7
4. Statics
It is that branch of Theory of Machines
which deals with the forces and their effects
while the machine parts are at rest. The mass
of the parts is assumed to be negligible.
Sub-divisions of Theory of
Machines
12/23/2022
8. BME 502 8
Fundamental Concepts
Space: Is a region which extends in all directions
and contains everything in it. The position of a
body in space is determined w.r.t. a reference
system
Time: to define the succession of events, it is not
sufficient to indicate their position. The time of
events is required, So time is as measure of the
succession of events.
Matter: Any substance, which occupies space. It is
made up of atoms and molecules
12/23/2022
9. BME 502 9
Body: Any matter that is bounded by a closed
surface
Rigid body: Is that which does not change its shape
or size when subjected to external forces
Deformable body: is that which changes its shape
or size when subjected to external forces
Mass: Quantity of matter it contains. It does not
vary with the location and orientation of the body
Particle: Body of negligible dimension . It occupies
no space. i.e. no size, but has a definite mass
concentrated at a point
12/23/2022
10. BME 502 10
Inertia: Resistance offered by a matter to any
change of its state of motion
Solid: Asubstance possessing a definite shape and a
definite volume
Force: It is a pull or push which acting on a body
changes or tends to change, the state of rest or
uniform motion of the body.
It is completely characterized by its point of
application, its magnitude and direction.
Forced System or system of forces: When a
number of forces act on a body
12/23/2022
11. BME 502 11
Weight: Weight of a body is the force with which
the earth attracts the body towards its centre.
W = m.g
Equilibrium: A body acted upon by a system of
forces is said to be in equilibrium, if it either
remains in a state of rest or continues to move in a
straight line with uniform velocity.
Motion: A body is said to be in motion, when it
changes its position w.r.t. other bodies. Thus the
relative change in position is called motion.
Motion involves both space and time.
12/23/2022
12. BME 502 12
NEWTON’S LAW OF MOTION
1st Law: Every body continues in its state of rest
or uniform motion in a straight line unless an
external resultant forces acts on it.
2nd Law: The rate of change of momentum of a
body is directly proportional to the force acting
on it and takes place in the direction of force.
3rd Law: To every action there is an equal and
opposite reaction
12/23/2022
14. BME 502 14
Static force analysis: When the inertia effect
due to the mass of the machine components are
neglected in the analysis of the mechanism
Dynamic force analysis: When the inertia
forces are considered in the analysis of the
mechanism
12/23/2022
15. BME 502 15
Inertia force
A force equal in magnitude but opposite in
direction and collinear with the impressed
force producing the acceleration, is known as
inertia force.
Inertia force = – m x a
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16. BME 502 16
Inertia torque
The inertia torque is an imaginary torque,
which when applied upon the rigid body,
brings it in equilibrium position. It is equal to
the accelerating couple in magnitude but
opposite in direction.
Inertia Torque = -I x α
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17. BME 502 17
D-Alembert’s principle
D-Alembert’s principle states that the
resultant force acting on a body together with
the reversed effective force (or inertia force),
are in equilibrium.
٤F = 0
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18. BME 502 18
Dynamic Analysis in reciprocating
engines
The velocity and acceleration of the reciprocating parts of
the steam engine or internal combustion engine may be
determined by graphical method or analytical method.
The velocity and acceleration, by graphical method, may
be determined by one of the following constructions:
1. Klien’s construction,
2. Ritterhaus’s construction, and
3. Bennett’s construction.
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19. Dynamic Analysis in reciprocating
engines - Analytical Method
Consider the motion of a crank and connecting rod of
a reciprocating steam engine as shown in Figure.
BME 502 19
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20. BME 502 20
Conti…
Let OC be the crank and PC the connecting rod. Let
the crank rotates with angular velocity of rad/s and
the crank turns through an angle θ from the inner
dead centre (briefly written as I.D.C).
Let x be the displacement of a reciprocating body P
from I.D.C. after time t seconds, during which the
crank has turned through an angle θ.
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21. BME 502 21
Let
l = Length of connecting rod between the centres,
r = Radius of crank or crank pin circle,
θ = Inclination of crank to the line of stroke PO
n = Ratio of length of connecting rod to the radius of crank
= l/r.
Conti…
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27. BME 502 27
Forces on the Reciprocating Parts of an
Engine
1. Piston effort
It is the net force acting on the piston or
crosshead pin, along the line of stroke. It is denoted
by FP.
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33. BME 502 33
Conti…
6. Crank effort or turning moment or torque on the
crank shaft.
The product of the crankpin effort (FT) and the crank
pin radius (r) is known as crank effort or turning moment
or torque on the crank shaft.
T = F × r
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34. BME 502 34
Turning moment diagram
• The turning moment diagram (also known as
crank effort diagram) is the graphical
representation of the turning moment or crank-
effort for various positions of the crank. It is
plotted on cartesian co-ordinates, in which the
turning moment is taken as the ordinate and
crank angle as abscissa.
• It is also known as T-M diagram.
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35. The variation of torque (T) during one revolution of
the crankshaft of a steam engine or an I C Engine
is:
T = Ft ˟ r
= F* x r x [sin θ + (sin 2θ/2√n² - sin² θ)]
Where,
Ft -tangential force or force normal to crank
r-crank radius
F* - net force acting on the piston
BME 502
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Conti…
41. BME 502 41
Fluctuation of Energy
• The variations of energy above and below the mean
resisting torque line are called fluctuations of energy.
• The difference between the maximum and the
minimum energies is known as maximum fluctuation of
energy.
Maximum fluctuation of energy,
E = Maximum energy – Minimum energy
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42. BME 502 42
Coefficient of
Fluctuation of Energy
• It may be defined as the ratio of the maximum
fluctuation of energy to the work done per cycle.
CE = Maximum fluctuation of energy / Work done per cycle
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43. BME 502 43
Flywheel
• A flywheel used in machines serves as a
reservoir, which stores energy during the
period when the supply of energy is more than
the requirement, and releases it during the
period when the requirement of energy is more
than the supply.
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45. Coefficient of
Fluctuation of Speed
The
minimum
difference between the maximum and
speeds during a cycle is called the
maximum fluctuation of speed. The ratio of the
maximum fluctuation of speed to the mean speed is
called the coefficient of fluctuation of speed.
BME 502 45
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46. BME 502 46
Energy Stored in a
Flywheel
Energy stored, E = mk2ω2CS = mv2CS
Where,
m = Mass of the flywheel in kg,
k = Radius of gyration of the flywheel in metres
ω = angular speed in rad/s2
Cs = Coefficient of Fluctuation of Speed
v = Mean linear velocity
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47. Question.1. The maximum and minimum speed of flywheel is 242 rpm
and 238 rpm respectively. The mass of flywheel is 2600 kg and
radius of gyration is 1.8 m. Find the mean speed of the flywheel,
maximum fluctuation of energy and coefficient of fluctuation of
speed.
Question.2. Find the maximum and minimum speeds of a flywheel of
mass 5200 kg and radius of gyration 1.8 m when the fluctuation of
energy is 100800 Nm. The mean speed of engine is 180 r.p.m.
BME 502
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50. Question. 4. The areas above and below the mean torque line for
an IC engine are -25, +200, -100, +150, -300, +150 and -75 mm²
taken in order. The scale for the turning moment diagram is 1 mm
vertical scale = 10 Nm and 1mm horizontal scale = 1.5°.the mass
of the rotating parts are 45 kg with a radius of gyration of 150
mm. if the engine speed is 1500 rpm, find the cof of speed.
BME 502
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51.
52. BME 502 52
Dimensions of the
Flywheel Rim
Tensile stress or hoop stress,σ = ρR2ω2 = ρv2
Where,
ρ = Density of rim material in kg/m3,
N = Speed of the flywheel in r.p.m.,
ω =Angular velocity of the flywheel in rad/s,
v = Linear velocity at the mean radius in m/s
= ω R = DN/60
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53. BME 502 53
Mass of the rim, m = Volume × density = πDA ρ
If the cross-section of the rim is a
rectangular, then
A = b × t
where b = Width of the rim, and
t = Thickness of the rim.
Conti…
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54. Question 5. The turning moment diagram as shown in figure, for a multi-cylinder
engine has been drawn to a scale of 1 mm to 500 N-m torque and 1 mm to 6° of
crank displacement. The intercepted area between o/p torque curve and mean
resistance line taken in order from one end, in sq. mm are: -30, +410, -280, +320, -
330, +250, -360, +280, -260 sq. mm when the engine is running at 800 rpm. The
engine has a stroke of 300 mm and fluctuation of speed is not to exceed 2% of the
mean speed.
Determine a suitable diameter and cross-section of the flywheel rim for a limiting
value of the some centrifugal stress of 7 N/mm³. the density of the material may be
assumed as 7200 kg/mm³. The width of the rim is to be 5 times the thickness.
BME 502
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55. BME 502 55
Operation of a Flywheel
in Punching Press
1. The function of a flywheel in an engine is to reduce
the fluctuations of speed, when the load on the crankshaft is
constant and the input torque varies during the cycle.
2. The flywheel can also be used to perform the same
function when the torque is constant and the load varies
during the cycle.
3. Such an application is found in punching press or in
a riveting machine.
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56. BME 502 56
Dynamics of Cam
follower mechanism
Cam Dynamics
Cam dynamics is the study of cam follower systems
with considering the dynamic forces and torques developed
in it.
Types of cam systems
1. Rigid body cam systems
2. Elastic body cam systems
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57. BME 502 57
Rigid cam system
If the members of the cam system are fairly rigid
and their speed is moderate, then the analysis of such
a cam system is known as analysis of rigid cam
system.
Elastic cam system
If the members of the cam system are elastic and
their speed is very high, then the analysis of such a
cam system is known as analysis of elastic cam
system
Conti…
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