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Design of mechanical systems mumbai university cbgs syllabus
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Dynamics of Machinery formulas
Mumbai University.
Mechanical Engineering
SEM V
Dynamics of Machinery
Governors and Gyroscopes:
1.1 Governors: Introduction to Centrifugal and Inertia governors, Force analysis of governors-
Porter and Hartnell governors, Performance characteristics of governors, Governors effort
and power
1.2 Gyroscope: Introduction, Gyroscopic couple and its effect on spinning bodies, naval ships
during steering, pitching, rolling and their stabilization. Effect of gyroscopic and centrifugal
couples, permissible speeds on curve paths, gyroscopic effect due to lateral misalignment of
rigid disc mounted on shaft.
09
2
2.1 Static and Dynamic force analysis, in slider crank mechanism (neglecting mass of
connecting rod and crank), Engine force analysis, Turning moment on crank shaft
2.2 Dynamically equivalent systems, to convert rigid body in to two mass with and without
correction couple
06
3
3.1 Basic Concepts of Vibration:
Vibration and oscillation, causes and effects of vibrations, Vibration parameters - springs,
mass, damper, damper models, Motion- periodic, non-periodic, degree of freedom, static
equilibrium position, vibration classification, steps involved in vibration analysis
3.2 Free Undamped Single Degree of Freedom Vibration System:
Longitudinal, transverse, torsional, vibration system, methods for formulation of differential
equations by Newton, Energy, Lagrangian and Rayleigh's method
08
4
4.1 Free Damped Single Degree of Freedom Vibration System:
Viscous damped system - under damped, critically damped, over damped; Logarithmic
decrement; Coulomb's damping
4.2 Equivalent Single Degree of Freedom Vibration System:
Conversion of multi-springs, multi masses, multi-dampers into a single spring and damper
with linear or rotational co-ordinate system, Introduction to free multi-degree of freedom
vibration systems
07
5
5.1 Forced Single Degree of Freedom Vibratory System:
Analysis of linear and torsional systems subjected to harmonic force excitation and harmonic
motion excitation (excluding elastic damper)
5.2 Vibration Isolation and Transmissibility:
Force Transmissibility, motion transmissibility, typical isolators & mounts.
5.3 Vibration Measuring instruments: Principle of seismic instruments, vibrometer,
accelerometer - undamped and damped, Introduction to conditioning monitoring and fault
diagnosis
6
6.1 Rotor Dynamics:
Critical speed of single rotor, undamped and damped
6.2 Balancing: Static and Dynamic balancing of multi rotor system, balancing of reciprocating
masses in In-line engines, V-engines (excluding other radial engines)
solution to Problem 8.13,8.14,8.15,8.16 from power plant technology by MM.EL....
solution to Problem 8.13,8.14,8.15,8.16 from power plant technology by MM.EL.WAKIL
Design of Petrol Engine
It covers the following points:-
Calculation of bore & stroke dimension
Design of cylinder, cylinder head and wet liner
Design of stud
نمونه سوال 5 فصل اول کنترل بهینه کتاب کرک
سوالات از تمرینات و مثال های کتاب کرک ترجمه پرفسور نیکروش انتخاب شده است
Design and Construction of a Connecting rod
An overview on different manufacturing processes of connecting rod.
Design,Analysis & Fabrication of suspension of all terrain vehicle
Design,Analysis & Fabrication of suspension of all terrain vehicle
Recommended
Dynamics of Machinery formulas
Mumbai University.
Mechanical Engineering
SEM V
Dynamics of Machinery
Governors and Gyroscopes:
1.1 Governors: Introduction to Centrifugal and Inertia governors, Force analysis of governors-
Porter and Hartnell governors, Performance characteristics of governors, Governors effort
and power
1.2 Gyroscope: Introduction, Gyroscopic couple and its effect on spinning bodies, naval ships
during steering, pitching, rolling and their stabilization. Effect of gyroscopic and centrifugal
couples, permissible speeds on curve paths, gyroscopic effect due to lateral misalignment of
rigid disc mounted on shaft.
09
2
2.1 Static and Dynamic force analysis, in slider crank mechanism (neglecting mass of
connecting rod and crank), Engine force analysis, Turning moment on crank shaft
2.2 Dynamically equivalent systems, to convert rigid body in to two mass with and without
correction couple
06
3
3.1 Basic Concepts of Vibration:
Vibration and oscillation, causes and effects of vibrations, Vibration parameters - springs,
mass, damper, damper models, Motion- periodic, non-periodic, degree of freedom, static
equilibrium position, vibration classification, steps involved in vibration analysis
3.2 Free Undamped Single Degree of Freedom Vibration System:
Longitudinal, transverse, torsional, vibration system, methods for formulation of differential
equations by Newton, Energy, Lagrangian and Rayleigh's method
08
4
4.1 Free Damped Single Degree of Freedom Vibration System:
Viscous damped system - under damped, critically damped, over damped; Logarithmic
decrement; Coulomb's damping
4.2 Equivalent Single Degree of Freedom Vibration System:
Conversion of multi-springs, multi masses, multi-dampers into a single spring and damper
with linear or rotational co-ordinate system, Introduction to free multi-degree of freedom
vibration systems
07
5
5.1 Forced Single Degree of Freedom Vibratory System:
Analysis of linear and torsional systems subjected to harmonic force excitation and harmonic
motion excitation (excluding elastic damper)
5.2 Vibration Isolation and Transmissibility:
Force Transmissibility, motion transmissibility, typical isolators & mounts.
5.3 Vibration Measuring instruments: Principle of seismic instruments, vibrometer,
accelerometer - undamped and damped, Introduction to conditioning monitoring and fault
diagnosis
6
6.1 Rotor Dynamics:
Critical speed of single rotor, undamped and damped
6.2 Balancing: Static and Dynamic balancing of multi rotor system, balancing of reciprocating
masses in In-line engines, V-engines (excluding other radial engines)
solution to Problem 8.13,8.14,8.15,8.16 from power plant technology by MM.EL....
solution to Problem 8.13,8.14,8.15,8.16 from power plant technology by MM.EL.WAKIL
Design of Petrol Engine
It covers the following points:-
Calculation of bore & stroke dimension
Design of cylinder, cylinder head and wet liner
Design of stud
نمونه سوال 5 فصل اول کنترل بهینه کتاب کرک
سوالات از تمرینات و مثال های کتاب کرک ترجمه پرفسور نیکروش انتخاب شده است
Design and Construction of a Connecting rod
An overview on different manufacturing processes of connecting rod.
Design,Analysis & Fabrication of suspension of all terrain vehicle
Design,Analysis & Fabrication of suspension of all terrain vehicle
Design of Diesel Engine by Prof. Sagar Dhotare
Design of Diesel Engine covers following component design:-
Design of Piston
Design of Cylinder and stud
Design of Cylinder head and wet Liner
Design of Piston Ring and Piston Pin
Design of Connecting Rod with I cross-section
Design Both eye, CAP and CAP bolts
Design of Gear Pump
The design of the Gear pump covers the following points:
Motor Selection
Design of Gear
Design of suction and delivery pipe
Design of Casing and casing bolts
Design of shaft and bearing
Static and dynamic analysis of automobile car chassis
Designing the space frame chassis of student formula racing vehicle and analyzing its strength using FEA.
UNIT 3 Software Testing Notes (TOPIC WISE)
Main topics of this document are Reducing the number of test cases & object oriented testing
Reducing the number of test cases
Sub topics are :- Prioritization guidelines, Priority category, Scheme, Risk Analysis,
Regression Testing, and Slice based testing.
Object Oriented Testing
Sub topic are :-Issues in Object Oriented Testing, Class Testing, GUI Testing, Object Oriented
Integration and System Testing
EOT Crane Design Problem No.- 1
In this, all components designed by considering various failure modes. The main Parts designed are Wire Rope, Sheave, Bearing for Sheave axle, Hook with bearing, Hook assembly.
ME6503 - DESIGN OF MACHINE ELEMENTS UNIT - I NOTES
ME6503 - DESIGN OF MACHINE ELEMENTS UNIT - I NOTES
THE QUESTION NUMBER WILL MATCH TO THE QUESTION BANK ATTACHED AT THE END
Car Dynamics using Quarter Model and Passive Suspension, Part VI: Sprung-mass...
IOSR Journal of Computer Engineering (IOSR-JCE) vol.17 issue.2 version.1
12 Speed Gear Box Theory Notes by Prof. Sagar Dhotare
It contains the following points:-
Requirements of speed gearboxes
Methods for changing speed in gearboxes
Preferred Numbers
Step ratio (or series ratio or progression ratio) (∅)
RAY DIAGRAM (OR SPEED DIAGRAM)
KINEMATIC LAYOUT (OR KINEMATIC ARRANGEMENT)
BASIC RULES FOR OPTIMUM GEARBOX DESIGN
solution of introductoin to fluid mechanics and machines(Prof. Som and Prof. ...
This book is pioneer in the field of fluid mechanics. Each student of mechanical engineering must buy it as it builds your concepts well and its problems can come in ESE of GATE exams because of its good difficulty level. Some students find it difficult to solve it so I am providing you my class notes on its solutions .
chapter 1(Introduction and fundamental concept) of second edition.
Unit I - Fluid statics Hand written notes
Basic Concepts and Definitions – Distinction between a fluid and a solid, Density, Specific weight, Specific gravity, Kinematic and Dynamic viscosity, variation of viscosity with temperature, Newton law of viscosity, surface tension, capillarity.
Fluid Statics - Fluid Pressure: Pressure at a point, Pascal’s law, Hydrostatic law. Piezometer, U-Tube Manometer, Single Column Manometer, U-Tube Differential Manometer, Micromanometers and problems. Pressure gauges, Hydrostatic pressure and force: on horizontal, vertical and inclined surfaces and problems.
Experimental and numerical stress analysis of a rectangular wing structure
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.
DESIGN ANALYSIS OF UNIVERSAL JOINT SHAFT FOR ROLLING MILLS
The properties of steels made by rolling of billets
are mainly dependent on the process of forming. The
performance of the rolling mill depends on the Universal
joint shaft through which the power is transmitted to the
rollers of a mill. This report mainly focuses on the
analysis of universal joint shaft for rolling mills because this
shaft is subjected to vibrations caused due to the jerk
produced during the passing of billet through the rollers.
Architectural Portfolio Sean Lockwood
This portfolio contains selected projects I completed during my undergraduate studies. 2018 - 2023
Hybrid optimization of pumped hydro system and solar- Engr. Abdul-Azeez.pdf
Advancements in technology unveil a myriad of electrical and electronic breakthroughs geared towards efficiently harnessing limited resources to meet human energy demands. The optimization of hybrid solar PV panels and pumped hydro energy supply systems plays a pivotal role in utilizing natural resources effectively. This initiative not only benefits humanity but also fosters environmental sustainability. The study investigated the design optimization of these hybrid systems, focusing on understanding solar radiation patterns, identifying geographical influences on solar radiation, formulating a mathematical model for system optimization, and determining the optimal configuration of PV panels and pumped hydro storage. Through a comparative analysis approach and eight weeks of data collection, the study addressed key research questions related to solar radiation patterns and optimal system design. The findings highlighted regions with heightened solar radiation levels, showcasing substantial potential for power generation and emphasizing the system's efficiency. Optimizing system design significantly boosted power generation, promoted renewable energy utilization, and enhanced energy storage capacity. The study underscored the benefits of optimizing hybrid solar PV panels and pumped hydro energy supply systems for sustainable energy usage. Optimizing the design of solar PV panels and pumped hydro energy supply systems as examined across diverse climatic conditions in a developing country, not only enhances power generation but also improves the integration of renewable energy sources and boosts energy storage capacities, particularly beneficial for less economically prosperous regions. Additionally, the study provides valuable insights for advancing energy research in economically viable areas. Recommendations included conducting site-specific assessments, utilizing advanced modeling tools, implementing regular maintenance protocols, and enhancing communication among system components.
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Design of Diesel Engine by Prof. Sagar Dhotare
Design of Diesel Engine covers following component design:-
Design of Piston
Design of Cylinder and stud
Design of Cylinder head and wet Liner
Design of Piston Ring and Piston Pin
Design of Connecting Rod with I cross-section
Design Both eye, CAP and CAP bolts
Design of Gear Pump
The design of the Gear pump covers the following points:
Motor Selection
Design of Gear
Design of suction and delivery pipe
Design of Casing and casing bolts
Design of shaft and bearing
Static and dynamic analysis of automobile car chassis
Designing the space frame chassis of student formula racing vehicle and analyzing its strength using FEA.
UNIT 3 Software Testing Notes (TOPIC WISE)
Main topics of this document are Reducing the number of test cases & object oriented testing
Reducing the number of test cases
Sub topics are :- Prioritization guidelines, Priority category, Scheme, Risk Analysis,
Regression Testing, and Slice based testing.
Object Oriented Testing
Sub topic are :-Issues in Object Oriented Testing, Class Testing, GUI Testing, Object Oriented
Integration and System Testing
EOT Crane Design Problem No.- 1
In this, all components designed by considering various failure modes. The main Parts designed are Wire Rope, Sheave, Bearing for Sheave axle, Hook with bearing, Hook assembly.
ME6503 - DESIGN OF MACHINE ELEMENTS UNIT - I NOTES
ME6503 - DESIGN OF MACHINE ELEMENTS UNIT - I NOTES
THE QUESTION NUMBER WILL MATCH TO THE QUESTION BANK ATTACHED AT THE END
Car Dynamics using Quarter Model and Passive Suspension, Part VI: Sprung-mass...
IOSR Journal of Computer Engineering (IOSR-JCE) vol.17 issue.2 version.1
12 Speed Gear Box Theory Notes by Prof. Sagar Dhotare
It contains the following points:-
Requirements of speed gearboxes
Methods for changing speed in gearboxes
Preferred Numbers
Step ratio (or series ratio or progression ratio) (∅)
RAY DIAGRAM (OR SPEED DIAGRAM)
KINEMATIC LAYOUT (OR KINEMATIC ARRANGEMENT)
BASIC RULES FOR OPTIMUM GEARBOX DESIGN
solution of introductoin to fluid mechanics and machines(Prof. Som and Prof. ...
This book is pioneer in the field of fluid mechanics. Each student of mechanical engineering must buy it as it builds your concepts well and its problems can come in ESE of GATE exams because of its good difficulty level. Some students find it difficult to solve it so I am providing you my class notes on its solutions .
chapter 1(Introduction and fundamental concept) of second edition.
Unit I - Fluid statics Hand written notes
Basic Concepts and Definitions – Distinction between a fluid and a solid, Density, Specific weight, Specific gravity, Kinematic and Dynamic viscosity, variation of viscosity with temperature, Newton law of viscosity, surface tension, capillarity.
Fluid Statics - Fluid Pressure: Pressure at a point, Pascal’s law, Hydrostatic law. Piezometer, U-Tube Manometer, Single Column Manometer, U-Tube Differential Manometer, Micromanometers and problems. Pressure gauges, Hydrostatic pressure and force: on horizontal, vertical and inclined surfaces and problems.
Experimental and numerical stress analysis of a rectangular wing structure
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.
DESIGN ANALYSIS OF UNIVERSAL JOINT SHAFT FOR ROLLING MILLS
The properties of steels made by rolling of billets
are mainly dependent on the process of forming. The
performance of the rolling mill depends on the Universal
joint shaft through which the power is transmitted to the
rollers of a mill. This report mainly focuses on the
analysis of universal joint shaft for rolling mills because this
shaft is subjected to vibrations caused due to the jerk
produced during the passing of billet through the rollers.
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About
Indigenized remote control interface card suitable for MAFI system CCR equipment. Compatible for IDM8000 CCR. Backplane mounted serial and TCP/Ethernet communication module for CCR remote access. IDM 8000 CCR remote control on serial and TCP protocol.
• Remote control: Parallel or serial interface.
• Compatible with MAFI CCR system.
• Compatible with IDM8000 CCR.
• Compatible with Backplane mount serial communication.
• Compatible with commercial and Defence aviation CCR system.
• Remote control system for accessing CCR and allied system over serial or TCP.
• Indigenized local Support/presence in India.
• Easy in configuration using DIP switches.
Technical Specifications
Indigenized remote control interface card suitable for MAFI system CCR equipment. Compatible for IDM8000 CCR. Backplane mounted serial and TCP/Ethernet communication module for CCR remote access. IDM 8000 CCR remote control on serial and TCP protocol.
Key Features
Indigenized remote control interface card suitable for MAFI system CCR equipment. Compatible for IDM8000 CCR. Backplane mounted serial and TCP/Ethernet communication module for CCR remote access. IDM 8000 CCR remote control on serial and TCP protocol.
• Remote control: Parallel or serial interface
• Compatible with MAFI CCR system
• Copatiable with IDM8000 CCR
• Compatible with Backplane mount serial communication.
• Compatible with commercial and Defence aviation CCR system.
• Remote control system for accessing CCR and allied system over serial or TCP.
• Indigenized local Support/presence in India.
Application
• Remote control: Parallel or serial interface.
• Compatible with MAFI CCR system.
• Compatible with IDM8000 CCR.
• Compatible with Backplane mount serial communication.
• Compatible with commercial and Defence aviation CCR system.
• Remote control system for accessing CCR and allied system over serial or TCP.
• Indigenized local Support/presence in India.
• Easy in configuration using DIP switches.
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