Unit 4- balancing of rotating masses, Dynamics of machines of VTU Syllabus prepared by Hareesha N Gowda, Asst. Prof, Dayananda Sagar College of Engg, Blore. Please write to hareeshang@gmail.com for suggestions and criticisms.
Unit 4- balancing of rotating masses, Dynamics of machines of VTU Syllabus prepared by Hareesha N Gowda, Asst. Prof, Dayananda Sagar College of Engg, Blore. Please write to hareeshang@gmail.com for suggestions and criticisms.
Unit 5- balancing of reciprocating masses, Dynamics of machines of VTU Syllabus prepared by Hareesha N Gowda, Asst. Prof, Dayananda Sagar College of Engg, Blore. Please write to hareeshang@gmail.com for suggestions and criticisms.
ME010 801 Design of Transmission Elements
(Common with AU010 801)
Teaching scheme Credits: 4
2 hours lecture, 2 hour tutorial and 1 hour drawing per week
Objectives
To provide basic design skill with regard to various transmission elements like clutches, brakes, bearings and
gears.
Module I (20 Hrs)
Clutches - friction clutches- design considerations-multiple disc clutches-cone clutch- centrifugal clutch -
Brakes- Block brake- band brake- band and block brake-internal expanding shoe brake.
Module II (17 Hrs)
Design of bearings - Types - Selection of a bearing type - bearing life - Rolling contact bearings - static
and dynamic load capacity - axial and radial loads - selection of bearings - dynamic equivalent load -
lubrication and lubricants - viscosity - Journal bearings - hydrodynamic theory - design considerations -
heat balance - bearing characteristic number - hydrostatic bearings.
Module III (19 Hrs)
Gears- classification- Gear nomenclature - Tooth profiles - Materials of gears - design of spur, helical,
bevel gears and worm & worm wheel - Law of gearing - virtual or formative number of teeth- gear tooth
failures- Beam strength - Lewis equation- Buckingham’s equation for dynamic load- wear loadendurance strength of tooth- surface durability- heat dissipation - lubrication of gears - Merits and
demerits of each type of gears.
Module IV (16 Hrs)
Design of Internal Combustion Engine parts- Piston, Cylinder, Connecting rod, Flywheel
Design recommendations for Forgings- castings and welded products- rolled sections- turned parts,
screw machined products- Parts produced on milling machines. Design for manufacturing - preparation
of working drawings - working drawings for manufacture of parts with complete specifications including
manufacturing details.
Note: Any one of the following data book is permitted for reference in the final University examination:
1. Machine Design Data hand book by K. Lingaiah, Suma Publishers, Bangalore/ Tata Mc Graw Hill
2. PSG Design Data, DPV Printers, Coimbatore.
Text Books
1. C.S,Sarma, Kamlesh Purohit, Design of Machine Elements Prentice Hall of India Ltd NewDelhi
2. V.B.Bhandari, Design of Machine Elements McGraw Hill Book Company
3. M. F. Spotts, T. E. Shoup, Design of Machine Elements, Pearson Education.
Reference Books
1. J. E. Shigley, Mechanical Engineering Design, McGraw Hill Book Company.
2. Juvinall R.C & Marshek K.M., Fundamentals of Machine Component Design, John Wiley
3. Doughtie V.L., & Vallance A.V., Design of Machine Elements, McGraw Hill Book Company.
4. Siegel, Maleev & Hartman, Mechanical Design of Machines, International Book Company
This is the basic lecture on introduction to gears for engineering students. It includes basics of gears, spur gear, bevel gear, etc. It also talks about a fundamental law of gearing, pressure angle and contact ratio.
Static balance occurs when the center of gravity of an object is on the axis of rotation. This allows the object to remain stationary, with the axis horizontal, without the application of any braking force. Static balance does not tend to rotate due to the force of gravity.
Static Balance is when the weight of the wheel and tire assembly is distributed equally around the axis of the wheel rotation. If static Balance exists the wheel will not tend to rotate.
Dynamic balancing definition: “Dynamic balancing is a way of balancing machines by rotating parts quickly and measuring the imbalance using electronic equipment. The imbalance measured can then be corrected by adding or subtracting weight from the rotating parts until the vibration is reduced.”
The various forces acts on the reciprocating parts of an engine.
The resultant of all the forces acting on the body of the engine due to inertia forces only is known as unbalanced force or shaking force.
Unit 5- balancing of reciprocating masses, Dynamics of machines of VTU Syllabus prepared by Hareesha N Gowda, Asst. Prof, Dayananda Sagar College of Engg, Blore. Please write to hareeshang@gmail.com for suggestions and criticisms.
ME010 801 Design of Transmission Elements
(Common with AU010 801)
Teaching scheme Credits: 4
2 hours lecture, 2 hour tutorial and 1 hour drawing per week
Objectives
To provide basic design skill with regard to various transmission elements like clutches, brakes, bearings and
gears.
Module I (20 Hrs)
Clutches - friction clutches- design considerations-multiple disc clutches-cone clutch- centrifugal clutch -
Brakes- Block brake- band brake- band and block brake-internal expanding shoe brake.
Module II (17 Hrs)
Design of bearings - Types - Selection of a bearing type - bearing life - Rolling contact bearings - static
and dynamic load capacity - axial and radial loads - selection of bearings - dynamic equivalent load -
lubrication and lubricants - viscosity - Journal bearings - hydrodynamic theory - design considerations -
heat balance - bearing characteristic number - hydrostatic bearings.
Module III (19 Hrs)
Gears- classification- Gear nomenclature - Tooth profiles - Materials of gears - design of spur, helical,
bevel gears and worm & worm wheel - Law of gearing - virtual or formative number of teeth- gear tooth
failures- Beam strength - Lewis equation- Buckingham’s equation for dynamic load- wear loadendurance strength of tooth- surface durability- heat dissipation - lubrication of gears - Merits and
demerits of each type of gears.
Module IV (16 Hrs)
Design of Internal Combustion Engine parts- Piston, Cylinder, Connecting rod, Flywheel
Design recommendations for Forgings- castings and welded products- rolled sections- turned parts,
screw machined products- Parts produced on milling machines. Design for manufacturing - preparation
of working drawings - working drawings for manufacture of parts with complete specifications including
manufacturing details.
Note: Any one of the following data book is permitted for reference in the final University examination:
1. Machine Design Data hand book by K. Lingaiah, Suma Publishers, Bangalore/ Tata Mc Graw Hill
2. PSG Design Data, DPV Printers, Coimbatore.
Text Books
1. C.S,Sarma, Kamlesh Purohit, Design of Machine Elements Prentice Hall of India Ltd NewDelhi
2. V.B.Bhandari, Design of Machine Elements McGraw Hill Book Company
3. M. F. Spotts, T. E. Shoup, Design of Machine Elements, Pearson Education.
Reference Books
1. J. E. Shigley, Mechanical Engineering Design, McGraw Hill Book Company.
2. Juvinall R.C & Marshek K.M., Fundamentals of Machine Component Design, John Wiley
3. Doughtie V.L., & Vallance A.V., Design of Machine Elements, McGraw Hill Book Company.
4. Siegel, Maleev & Hartman, Mechanical Design of Machines, International Book Company
This is the basic lecture on introduction to gears for engineering students. It includes basics of gears, spur gear, bevel gear, etc. It also talks about a fundamental law of gearing, pressure angle and contact ratio.
Static balance occurs when the center of gravity of an object is on the axis of rotation. This allows the object to remain stationary, with the axis horizontal, without the application of any braking force. Static balance does not tend to rotate due to the force of gravity.
Static Balance is when the weight of the wheel and tire assembly is distributed equally around the axis of the wheel rotation. If static Balance exists the wheel will not tend to rotate.
Dynamic balancing definition: “Dynamic balancing is a way of balancing machines by rotating parts quickly and measuring the imbalance using electronic equipment. The imbalance measured can then be corrected by adding or subtracting weight from the rotating parts until the vibration is reduced.”
The various forces acts on the reciprocating parts of an engine.
The resultant of all the forces acting on the body of the engine due to inertia forces only is known as unbalanced force or shaking force.
Cosmetic shop management system project report.pdfKamal Acharya
Buying new cosmetic products is difficult. It can even be scary for those who have sensitive skin and are prone to skin trouble. The information needed to alleviate this problem is on the back of each product, but it's thought to interpret those ingredient lists unless you have a background in chemistry.
Instead of buying and hoping for the best, we can use data science to help us predict which products may be good fits for us. It includes various function programs to do the above mentioned tasks.
Data file handling has been effectively used in the program.
The automated cosmetic shop management system should deal with the automation of general workflow and administration process of the shop. The main processes of the system focus on customer's request where the system is able to search the most appropriate products and deliver it to the customers. It should help the employees to quickly identify the list of cosmetic product that have reached the minimum quantity and also keep a track of expired date for each cosmetic product. It should help the employees to find the rack number in which the product is placed.It is also Faster and more efficient way.
CFD Simulation of By-pass Flow in a HRSG module by R&R Consult.pptxR&R Consult
CFD analysis is incredibly effective at solving mysteries and improving the performance of complex systems!
Here's a great example: At a large natural gas-fired power plant, where they use waste heat to generate steam and energy, they were puzzled that their boiler wasn't producing as much steam as expected.
R&R and Tetra Engineering Group Inc. were asked to solve the issue with reduced steam production.
An inspection had shown that a significant amount of hot flue gas was bypassing the boiler tubes, where the heat was supposed to be transferred.
R&R Consult conducted a CFD analysis, which revealed that 6.3% of the flue gas was bypassing the boiler tubes without transferring heat. The analysis also showed that the flue gas was instead being directed along the sides of the boiler and between the modules that were supposed to capture the heat. This was the cause of the reduced performance.
Based on our results, Tetra Engineering installed covering plates to reduce the bypass flow. This improved the boiler's performance and increased electricity production.
It is always satisfying when we can help solve complex challenges like this. Do your systems also need a check-up or optimization? Give us a call!
Work done in cooperation with James Malloy and David Moelling from Tetra Engineering.
More examples of our work https://www.r-r-consult.dk/en/cases-en/
Hierarchical Digital Twin of a Naval Power SystemKerry Sado
A hierarchical digital twin of a Naval DC power system has been developed and experimentally verified. Similar to other state-of-the-art digital twins, this technology creates a digital replica of the physical system executed in real-time or faster, which can modify hardware controls. However, its advantage stems from distributing computational efforts by utilizing a hierarchical structure composed of lower-level digital twin blocks and a higher-level system digital twin. Each digital twin block is associated with a physical subsystem of the hardware and communicates with a singular system digital twin, which creates a system-level response. By extracting information from each level of the hierarchy, power system controls of the hardware were reconfigured autonomously. This hierarchical digital twin development offers several advantages over other digital twins, particularly in the field of naval power systems. The hierarchical structure allows for greater computational efficiency and scalability while the ability to autonomously reconfigure hardware controls offers increased flexibility and responsiveness. The hierarchical decomposition and models utilized were well aligned with the physical twin, as indicated by the maximum deviations between the developed digital twin hierarchy and the hardware.
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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Saudi Arabia stands as a titan in the global energy landscape, renowned for its abundant oil and gas resources. It's the largest exporter of petroleum and holds some of the world's most significant reserves. Let's delve into the top 10 oil and gas projects shaping Saudi Arabia's energy future in 2024.
Overview of the fundamental roles in Hydropower generation and the components involved in wider Electrical Engineering.
This paper presents the design and construction of hydroelectric dams from the hydrologist’s survey of the valley before construction, all aspects and involved disciplines, fluid dynamics, structural engineering, generation and mains frequency regulation to the very transmission of power through the network in the United Kingdom.
Author: Robbie Edward Sayers
Collaborators and co editors: Charlie Sims and Connor Healey.
(C) 2024 Robbie E. Sayers
Hybrid optimization of pumped hydro system and solar- Engr. Abdul-Azeez.pdffxintegritypublishin
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.
Runway Orientation Based on the Wind Rose Diagram.pptx
Balancing of rotating masses
1. UNIT-VI
Balancing of Rotating Masses
Introduction
The high speed of engines and other machines is a common phenomenon now-a-
days. It is, therefore, very essential that all the rotating and reciprocating parts should be
completely balanced as far as possible. If these parts are not properly balanced, the
dynamic forces are set up. These forces not only increase the loads on bearings and
stressesin the various members, but also produce unpleasant and even dangerous
vibrations. In this chapter we shall discuss the balancing of unbalanced forces caused by
rotating masses, in order to minimise pressure on the main bearings when an engine is
running.
Balancing of Rotating Masses
We have already discussed, that whenever a certain mass is attached to a rotating
shaft, it exerts some centrifugal force, whose effect is to bend the shaft and to produce
vibrations in it. In order to prevent the effect of centrifugal force, another mass is
attached to the opposite side of the shaft, at such a position so as to balance the effect of
the centrifugal force of the first mass. This is done in such a way that the centrifugal force
of both the masses are made to be equal and opposite. The process of providing the
second mass in order to counteract the effect of the centrifugal force of the first mass,
is called balancing of rotating masses.
The following cases are important from the subject point of view:
1. Balancing of a single rotating mass by a single mass rotating in the same plane.
2. Balancing of a single rotating mass by two masses rotating in different planes.
3. Balancing of different masses rotating in the same plane.
4. Balancing of different masses rotating in different planes.
We shall now discuss these cases, in detail, in the following pages.
Balancing of a Single Rotating Mass By a Single Mass Rotating in the Same Plane
Consider a disturbing mass m1 attached to a shaft rotating at ω rad/s as shown in
Fig.
Let r1 be the radius of rotation of the mass m1 (i.e. distance between the axis of rotation
of the shaft and the centre of gravity of the mass m1).
We know that the centrifugal force exerted by the mass m1 on the shaft,
This centrifugal force acts radially outwards and thus produces bending moment
on the
shaft. In order to counteract the effect of this force, a balancing mass (m2) may be
attached in the same plane of rotation as that of disturbing mass (m1) such that the
centrifugal forces due to the two masses are equal and opposite.
Let r 2 = Radius of rotation of the balancing mass m2 (i.e. distance between the
axis of rotation of the shaft and the centre of gravity of mass m2 ).
2. Balancing of a Single Rotating Mass By Two Masses Rotating in Different Planes:
We have discussed in the previous article that by introducing a single balancing
mass in the same plane of rotation as that of disturbing mass, the centrifugal forces are
balanced. In other words, the two forces are equal in magnitude and opposite in direction.
But this type of arrangement for balancing gives rise to a couple which tends to rock the
shaft in its bearings. Therefore in order to put the system in complete balance, two
balancing masses are placed in two different planes, parallel to the plane of rotation of the
disturbing mass, in such a way that they satisfy the following two conditions of
equilibrium.
1. The net dynamic force acting on the shaft is equal to zero. This requires that the
line of action of three centrifugal forces must be the same. In other words, the
centre of the masses of the system must lie on the axis of rotation. This is the
condition for static balancing.
2. The net couple due to the dynamic forces acting on the shaft is equal to zero. In
other words, the algebraic sum of the moments about any point in the plane must
be zero.
The conditions (1) and (2) together give dynamic balancing.
The following two possibilities may arise while attaching the two balancing masses :
1. The plane of the disturbing mass may be in between the planes of the two balancing
masses, and
2. The plane of the disturbing mass may lie on the left or right of the two planes
containing the balancing masses.
Case:1
1. When the plane of the disturbing mass lies in between the planes of the two
balancing masses:
Let l1 = Distance between the planes A and L,
l2 = Distance between the planes A and M, and
l = Distance between the planes L and M.
3. 2. When the plane of the disturbing mass lies on one end of the planes of the
balancing masses
4. the following conditions must be satisfied in order to balance the system, i.e.
Now, to find the balancing force in the plane L (or the dynamic force at the bearing Q of
a shaft), take moments about P which is the point of intersection of the plane M and the
axis of rotation.
Therefore
Similarly, to find the balancing force in the plane M (or the dynamic force at the bearing
P of a shaft), take moments about Q which is the point of intersection of the plane L and
the axis of rotation.
Therefore
Balancing of Several Masses Rotating in the Same Plane
Consider any number of masses (say four) of magnitude m1, m2, m3 and m4 at distances of
r1, r2, r3 and r4 from the axis of the rotating shaft. Let θ1, θ2, θ3 and θ4be the angles of
these masses with the horizontal line OX, as shown in Fig. (a). Let these masses rotate
about an axis through O and perpendicular to the plane of paper, with a constant angular
velocity of ω rad/s.
5. The magnitude and direction of the balancing mass may be obtained, analytically, as
discussed below :
1. First of all, find out the centrifugal force (or the product of the mass and its radius of
rotation) exerted by each mass on the rotating shaft.
2. Resolve the centrifugal forces horizontally and vertically and find their sums, i.e. ΣH
and ΣV .
We know that
Balancing of Several Masses Rotating in Different Planes:
When several masses revolve in different planes, they may be transferred to a
reference plane (briefly written as R.P.), which may be defined as the plane passing
through a point on the axis of rotation and perpendicular to it. The effect of transferring a
revolving mass (in one plane) to a reference plane is to cause a force of magnitude equal
to the centrifugal force of the revolving mass to act in the reference plane, together with a
couple of magnitude equal to the product of the force and the distance between the plane
of rotation and the reference plane. In order to have a complete balance of the several
revolving masses in different planes, the following two conditions must be satisfied :
1. The forces in the reference plane must balance, i.e. the resultant force must be zero.
2. The couples about the reference plane must balance, i.e. the resultant couple must be
zero.
6. Let us now consider four masses m1, m2, m3 and m4 revolving in planes 1, 2, 3 and 4
respectively as shown in Fig. (a). The relative angular positions of these masses are
shown in the end view [Fig. (b)]. The magnitude of the balancing masses mL and mM in
planes L and M may be obtained as discussed below :
1. Take one of the planes, say L as the reference plane (R.P.). The distances of all the
other planes to the left of the reference plane may be regarded as negative, and those to
the right as positive.
2. Tabulate the data as shown in Table. The planes are tabulated in the same order in
which they occur, reading from left to right.