The hybrid car is one which uses Two or more energy.
The electric power engine works at lower speed and gasoline engine at higher speed
The hybrid engine automatically off while car is stopped and restart while you accelerate
Optimum design of braking system for a formula 3 race cars with numeric compu...IRJET Journal
The document describes the design and analysis of the braking system for a Formula 3 race car. Key points:
- A bike's disc rotor and calipers were selected to reduce weight. Calculations showed the clamping force was sufficient and thermal analysis validated the safety of using the bike's rotor.
- Calculations determined braking forces, torques, bias, and performance. A tandem master cylinder provided independent circuits.
- Steady state and dynamic thermal-structural analyses in ANSYS and ABAQUS showed temperature distributions, stresses, and deformations met requirements.
- The implemented system achieved a weight reduction of around 11kg compared to a standard system, improving performance.
Computational and experimental investigation of aerodynamics of flapping aero...Lahiru Dilshan
Renewal interest on the exploitation of flapping flight motions to attain high propulsion efficiency of air vehicles is inspired by the aerodynamics of birds’ and insects’ flights. The flapping characteristics can be majorly used to develop micro aerial vehicles (MAV) as this is a lucrative method to generate lift and thrust simultaneously. In this project, the variation of the flow properties and the thrust generation of an airfoil in a flapping (plunging) motion, is evaluated using both computational and experimental methods. The NACA 2412 airfoil was selected for the study and, the computational method was carried out using an inviscid flow model and computational fluid dynamics (CFD) simulations, simultaneously to obtain and compare the variation of properties.
The inviscid model was developed using conformal mapping and potential flow theories, and it is capable of producing results for any arbitrary aerofoil. Steady-state results were compared and validated in both CFD and inviscid flow modelling as the computational framework along with flow visualisation and force sensing as the experimental framework. The validated CFD and inviscid models have been developed to produce a plunging motion to the aerofoil and obtain the variation of drag and lift coefficients with time. The experimental setup was designed to obtain the forces acting on the airfoil, and the flow characteristics were visually observed using a flow visualization technique. The force calculations were done through a developed and optimized load cell arrangement. The developed smoke flow visualisation technique is capable of successfully capturing streamline patterns, flow separation regions. These results were compared along with wake development between computational and experimental models. The Level of agreement and limitations of each method have been discussed in this report.
Characteristics of separately excited generatorSaif al-din ali
The object of this experiment is to verify the
factors , which affect Me building voltage In separately - cited generator
, the external Characteristics and load saturation characteristics ,
regulating characteristics of the generator
Characteristics of separately excited generator
SAIF ALDIN ALI MADIN
سيف الدين علي ماضي
S96aif@gmail.com
This document describes an intelligent braking system that automatically applies the brakes when a vehicle is in reverse. The key components are an ultrasonic sensor to detect obstacles, a solenoid valve to control air flow, a pneumatic cylinder to apply the brakes, and a pneumatic braking system. When the sensor detects an obstacle behind the vehicle, it sends a signal to open the solenoid valve, allowing air to flow to the cylinder and engage the brakes. Mathematical models are presented to analyze load distribution, weight transfer, clamping force, and required deceleration. The system provides automatic and safe braking when reversing, reducing risk of collisions. Potential applications include automatic parking systems and vehicles generally.
Transient three dimensional cfd modelling of ceilng fanLahiru Dilshan
Ceiling fans are used to get thermal comfort, especially in tropical countries. With the increment of the usage of air conditioners, the emission of CO2 is increased. But ceiling fans are a limited solution, that saves much energy compared to air conditioners. Ceiling fans generate a non-uniform velocity profile, so that, there is a non-uniform thermal environment. That non-uniform environment does not imply lower thermal comfort, that will give enough thermal comfort with low energy cost by air velocity. Hence, there will be difficulties of analysing with simple modelling techniques in that environment. So, to predict the performance of the ceiling fan required more accurate models.
The accurate model of a ceiling fan will generate complex geometry that makes difficulties for the simulation process and requires higher computational power. Because of that, there are several methods used to predict the performance of the ceiling fan using mathematical techniques but that will give an estimated value of properties in the surrounding.
Finite Element Analysys of Axial Flow Turbine BladeIJMER
In this paper the finite element analysis of a Axial flow turbine bladefor a high tuned
design was carried out. The geometry was modelled in CATI A V5 R21 and finite element analysis had
been performed in AN SYS12 WB. FE analysis is was used to determine stress analysis at 15000rpm
modal analysis is at slung as well a s operating condition at 700F and low cycle fatigue analysis. After
performing the analysis, the safe working conditions for the axial flow turbine blade were also stated.
This document outlines test procedures for measuring the net power and 30-minute power of electric drive trains. It describes using either a bench dynamometer or chassis dynamometer. Key steps include:
1. Performing tests at various motor/vehicle speeds within the manufacturer's recommended range to generate a power curve.
2. Measuring net power by running at full power for 5 minutes, maintaining specified temperatures.
3. Measuring 30-minute power by a 30-minute run while maintaining power within ±5% of initial value.
4. Results must be within ±2% tolerance for maximum power and ±4% for other points.
The document provides design specifications for a mechanical system that uses pulleys, gears, a shaft, and bearings. It includes details on the power input and output requirements for different components, material properties, and design considerations. The author is tasked with designing: 1) Pulleys B and K with a belt to transmit power from pulley K to B; 2) Spur gears C and G to transmit 65% of power; 3) Helical gears E and H to transmit the remaining power; 4) The shaft connecting the components; 5) Bearings A and D to support the shaft. Calculations and checks are required to validate the design meets stress, wear, and reliability requirements.
Optimum design of braking system for a formula 3 race cars with numeric compu...IRJET Journal
The document describes the design and analysis of the braking system for a Formula 3 race car. Key points:
- A bike's disc rotor and calipers were selected to reduce weight. Calculations showed the clamping force was sufficient and thermal analysis validated the safety of using the bike's rotor.
- Calculations determined braking forces, torques, bias, and performance. A tandem master cylinder provided independent circuits.
- Steady state and dynamic thermal-structural analyses in ANSYS and ABAQUS showed temperature distributions, stresses, and deformations met requirements.
- The implemented system achieved a weight reduction of around 11kg compared to a standard system, improving performance.
Computational and experimental investigation of aerodynamics of flapping aero...Lahiru Dilshan
Renewal interest on the exploitation of flapping flight motions to attain high propulsion efficiency of air vehicles is inspired by the aerodynamics of birds’ and insects’ flights. The flapping characteristics can be majorly used to develop micro aerial vehicles (MAV) as this is a lucrative method to generate lift and thrust simultaneously. In this project, the variation of the flow properties and the thrust generation of an airfoil in a flapping (plunging) motion, is evaluated using both computational and experimental methods. The NACA 2412 airfoil was selected for the study and, the computational method was carried out using an inviscid flow model and computational fluid dynamics (CFD) simulations, simultaneously to obtain and compare the variation of properties.
The inviscid model was developed using conformal mapping and potential flow theories, and it is capable of producing results for any arbitrary aerofoil. Steady-state results were compared and validated in both CFD and inviscid flow modelling as the computational framework along with flow visualisation and force sensing as the experimental framework. The validated CFD and inviscid models have been developed to produce a plunging motion to the aerofoil and obtain the variation of drag and lift coefficients with time. The experimental setup was designed to obtain the forces acting on the airfoil, and the flow characteristics were visually observed using a flow visualization technique. The force calculations were done through a developed and optimized load cell arrangement. The developed smoke flow visualisation technique is capable of successfully capturing streamline patterns, flow separation regions. These results were compared along with wake development between computational and experimental models. The Level of agreement and limitations of each method have been discussed in this report.
Characteristics of separately excited generatorSaif al-din ali
The object of this experiment is to verify the
factors , which affect Me building voltage In separately - cited generator
, the external Characteristics and load saturation characteristics ,
regulating characteristics of the generator
Characteristics of separately excited generator
SAIF ALDIN ALI MADIN
سيف الدين علي ماضي
S96aif@gmail.com
This document describes an intelligent braking system that automatically applies the brakes when a vehicle is in reverse. The key components are an ultrasonic sensor to detect obstacles, a solenoid valve to control air flow, a pneumatic cylinder to apply the brakes, and a pneumatic braking system. When the sensor detects an obstacle behind the vehicle, it sends a signal to open the solenoid valve, allowing air to flow to the cylinder and engage the brakes. Mathematical models are presented to analyze load distribution, weight transfer, clamping force, and required deceleration. The system provides automatic and safe braking when reversing, reducing risk of collisions. Potential applications include automatic parking systems and vehicles generally.
Transient three dimensional cfd modelling of ceilng fanLahiru Dilshan
Ceiling fans are used to get thermal comfort, especially in tropical countries. With the increment of the usage of air conditioners, the emission of CO2 is increased. But ceiling fans are a limited solution, that saves much energy compared to air conditioners. Ceiling fans generate a non-uniform velocity profile, so that, there is a non-uniform thermal environment. That non-uniform environment does not imply lower thermal comfort, that will give enough thermal comfort with low energy cost by air velocity. Hence, there will be difficulties of analysing with simple modelling techniques in that environment. So, to predict the performance of the ceiling fan required more accurate models.
The accurate model of a ceiling fan will generate complex geometry that makes difficulties for the simulation process and requires higher computational power. Because of that, there are several methods used to predict the performance of the ceiling fan using mathematical techniques but that will give an estimated value of properties in the surrounding.
Finite Element Analysys of Axial Flow Turbine BladeIJMER
In this paper the finite element analysis of a Axial flow turbine bladefor a high tuned
design was carried out. The geometry was modelled in CATI A V5 R21 and finite element analysis had
been performed in AN SYS12 WB. FE analysis is was used to determine stress analysis at 15000rpm
modal analysis is at slung as well a s operating condition at 700F and low cycle fatigue analysis. After
performing the analysis, the safe working conditions for the axial flow turbine blade were also stated.
This document outlines test procedures for measuring the net power and 30-minute power of electric drive trains. It describes using either a bench dynamometer or chassis dynamometer. Key steps include:
1. Performing tests at various motor/vehicle speeds within the manufacturer's recommended range to generate a power curve.
2. Measuring net power by running at full power for 5 minutes, maintaining specified temperatures.
3. Measuring 30-minute power by a 30-minute run while maintaining power within ±5% of initial value.
4. Results must be within ±2% tolerance for maximum power and ±4% for other points.
The document provides design specifications for a mechanical system that uses pulleys, gears, a shaft, and bearings. It includes details on the power input and output requirements for different components, material properties, and design considerations. The author is tasked with designing: 1) Pulleys B and K with a belt to transmit power from pulley K to B; 2) Spur gears C and G to transmit 65% of power; 3) Helical gears E and H to transmit the remaining power; 4) The shaft connecting the components; 5) Bearings A and D to support the shaft. Calculations and checks are required to validate the design meets stress, wear, and reliability requirements.
This document outlines the test method for measuring the range of electric power train vehicles in categories L, M, and N. It specifies using the IDC driving cycle for category L vehicles. The method involves fully charging the REESS overnight, applying the IDC cycle at a steady speed of 70% maximum 30 minute speed, and stopping when the vehicle can no longer maintain 65% maximum 30 minute speed or after 100km, whichever comes first. The final measured distance traveled is the calculated range in km for the electric vehicle.
This document specifies the test method for measuring the electrical energy consumption of electric power train vehicles. It outlines the test procedure which involves fully charging the REESS, running the vehicle through 34 cycles of the Indian Driving Cycle within 4 hours, recording the distance traveled, and calculating the energy consumption in Wh/km. Parameters like time, distance, temperature, speed, and energy are measured with defined accuracies and resolutions. The vehicle must pass requirements specified by the manufacturer for energy consumption.
Dynamometers are machines used to measure the torque and power of rotating devices like engines and motors. There are different types including electrical, hydraulic, and mechanical dynamometers. A dynamometer consists of an absorption unit with a rotor that is coupled to the device under test. It allows the device to rotate while applying a braking torque through various means to measure its performance characteristics.
1) The document discusses potential and kinetic energy, with a focus on using potential energy experiments involving trolleys rolling down slopes and pendulums to understand how potential energy is converted to kinetic energy.
2) It provides formulas for calculating potential energy (PE = mgh), kinetic energy (KE = 1/2 mv^2), and velocity (v = √2gh) and discusses their application to roller coaster design.
3) The steps outlined for a roller coaster design experiment involve calculating the potential and kinetic energy at various points and using that to determine the track design and roller coaster speed and energy requirements.
This document provides information about an experiment to determine the torsional vibration characteristics of single and double rotor systems. It includes the objectives, equipment description, procedures, sample calculations and observations. The experiment aims to determine the period and frequency of torsional vibration experimentally and compare to theoretical values. Key steps involve twisting and releasing rotors to measure oscillation times and calculating moments of inertia, torsional stiffness and natural frequencies.
This document discusses the design of an active electromagnetic suspension system for automotive applications. Key points:
- An active suspension system is proposed using a brushless tubular permanent magnet actuator in parallel with a passive spring. This provides additional stability during maneuvers like cornering and braking.
- Specifications for the actuator are derived based on measurements of forces during test drives. The actuator needs to produce peak forces of 4 kN and continuous forces of 1 kN to eliminate roll and pitch. It also needs to absorb road vibrations up to 2.05 kN.
- A quarter-car test setup is used to validate the improved performance of the active suspension system. Measurements show the roll angle is
This document summarizes an experiment on the impact of jets using a hydraulic bench. The experiment aims to demonstrate that the force on a vane is proportional to the rate of delivery of momentum from a jet. Students collect data on the distance moved by a jockey weight under different flow rates. The results show the force on the vane increases linearly with the rate of delivery of momentum from the jet, consistent with theoretical expectations, although actual forces measured are slightly lower than predicted.
Experimental Investigation of Multi Aerofoil Configurations Using Propeller T...ijceronline
This paper briefs about the performance test on multi aero foil configuration on propeller test rig. The airfoils used are a conventional airfoil , a airfoil with stepped configuration and a Clark y airfoil .They were tested for various speed and blade angles using propeller test rig. The result are compared and studied with the conventional airfoil configurations. In future Such Aerofoils can be used for wind Mills for producing the high Voltage Power.
The flow across an airfoil is studied for different angle of attack. The CFD analysis results are documented and studied for different angle of attack using fluent & gambit.
- Researchers at the University of Maryland tested a small-scale helicopter rotor in conditions simulating the Martian atmosphere to determine if a micro aerial vehicle could hover on Mars.
- Testing of a rectangular rotor planform in a vacuum chamber showed it could produce enough thrust to hover but with low figure of merit below 0.4. Predicted endurance was around 13 minutes.
- Additional testing showed performance significantly improved with higher Reynolds numbers, with figure of merit reaching a typical MAV value of 0.62.
- Further studies will parametrically evaluate different rotor designs including airfoil, planform shape, twist and solidity to optimize performance in the thin Martian atmosphere.
Development Of Tipper Unloading MechanismIRJET Journal
1. The document describes the development of a tipper unloading mechanism to allow a tipper truck to unload material in multiple directions rather than just the rear.
2. Currently, tipper trucks can only unload material out the back, which reduces efficiency when precise unloading locations are required. It also requires the truck be parked in certain positions.
3. The proposed design involves adding two additional hydraulic cylinders on the sides of the tipper bed, allowing material to be unloaded to the left or right as well as the rear. This would provide more flexibility in unloading location without repositioning the truck.
4. Calculations are provided for the existing rear unloading mechanism involving the hydraulic cylinder, motor,
PERFORMANCE AND ANALYSIS OF MILLING TOOLS DYNAMOMETERsathish sak
A Milling is the machining process of using rotary cutters to remove material from a work piece by advancing (or feeding) in a direction at an angle with the axis of the tool.
A dynamometer or "dyno" for short, is a device for measuring force, torque, or power. For example, the power produced by an engine, motor or other rotating prime mover can be calculated by simultaneously measuring torque and rotational speed (RPM).
Couette flow is the flow of a viscous fluid between two surfaces, one of which is
moving tangentially relative and another is fixed. The relative motion of the surfaces
imposes a shear stress that make flow possible.
Watch Video of this presentation on Link: https://youtu.be/bHKaPBgDk6g
For notes/articles, Visit my blog (link is given below).
For Video, Visit our YouTube Channel (link is given below).
Any Suggestions/doubts/reactions, please leave in the comment box.
Follow Us on
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Preliminary Design of 100 Seater AircraftROSHAN SAH
This presentation explains the different design phases of aircraft and some detailed descriptions of each phase. Then, it explains the preliminary design procedure of the aircraft which consists of weight estimation, wing design, fuselage design, drag polar, maximum speed, thrust requirement and selection of engine, landing gear selection, tail surface design, and different performance calculations.
1. The document discusses various methods for measuring force, torque, and strain. It describes load cells, cantilever beams, proving rings, and differential transformers that can be used to measure force.
2. Methods for measuring torque and power are also presented, including absorption dynamometers, prony brake dynamometers, hydraulic dynamometers, and eddy current dynamometers.
3. The concept of strain and strain gauges for measuring strain are briefly covered at the end.
Watch Video of this presentation on Link: https://youtu.be/g8eJsznmsaY
For notes/articles, Visit my blog (link is given below).
For Video, Visit our YouTube Channel (link is given below).
Any Suggestions/doubts/reactions, please leave in the comment box.
Follow Us on
YouTube: https://www.youtube.com/channel/UCVPftVoKZoIxVH_gh09bMkw/
Blog: https://e-gyaankosh.blogspot.com/
Facebook: https://www.facebook.com/egyaankosh/
This document provides information on various methods for measuring force, torque, power, flow and temperature. It discusses direct and indirect methods for measuring force, including using spring balances, accelerometers, hydraulic load cells, pneumatic load cells and strain gauge load cells. It also describes techniques for measuring torque using rope brakes, hydraulic dynamometers and strain gauge transducers. Flow measurement is discussed for devices like venturi meters, orifice meters and rotameters. Temperature measurement techniques include bimetallic strips, thermocouples and resistance thermometers.
Measurement of force and torque and pressure standardsMech-4u
Measurement of Force and Torque and pressure Standards,
Measuring Methods,
study of different types of forces and torque Measuring systems.
Description and working Principle of different types of Transducers for Measuring Pressure.
Since the beginning of modern civilization,we are always dependent on fossil fuels as the source of energy for our daily requirements.over the past decade due to population expansion,we can notice the deplition of these fossile fules . therefore to reduce this deplition,energy harvesting has become one of the prime topic for this generation.the process of acquiring the energy surrounding the system and converting it into usefull electrical source is called energy harvesting.Piezoelectric materials have gained popularity in this section of energy harvesting,which can be used to store waste energy for future use.
In our project,Since we are using electric engine which is charged with the help of piezos and solar panels,it reduces pollution.Also it reduces usage of electricity since we are using piezo electricity and solar panels
Design, Analysis & Balancing of 5 Cylinder Engine CrankshaftIJMER
This document summarizes the design, analysis, and balancing of a 5 cylinder engine crankshaft. It discusses modeling the crankshaft in Solidworks and analyzing it in ANSYS using finite element analysis. Calculations are shown for designing the crankshaft and crankpin based on engine specifications. Loading and boundary conditions are applied for static structural analysis to determine stresses and deflection. Von Mises and shear stresses from the analysis match theoretical calculations. The conclusions are that finite element analysis is effective for determining permissible stresses and that the 5 cylinder design provides weight optimization and lower cost compared to a 6 cylinder configuration.
This document outlines the test method for measuring the range of electric power train vehicles in categories L, M, and N. It specifies using the IDC driving cycle for category L vehicles. The method involves fully charging the REESS overnight, applying the IDC cycle at a steady speed of 70% maximum 30 minute speed, and stopping when the vehicle can no longer maintain 65% maximum 30 minute speed or after 100km, whichever comes first. The final measured distance traveled is the calculated range in km for the electric vehicle.
This document specifies the test method for measuring the electrical energy consumption of electric power train vehicles. It outlines the test procedure which involves fully charging the REESS, running the vehicle through 34 cycles of the Indian Driving Cycle within 4 hours, recording the distance traveled, and calculating the energy consumption in Wh/km. Parameters like time, distance, temperature, speed, and energy are measured with defined accuracies and resolutions. The vehicle must pass requirements specified by the manufacturer for energy consumption.
Dynamometers are machines used to measure the torque and power of rotating devices like engines and motors. There are different types including electrical, hydraulic, and mechanical dynamometers. A dynamometer consists of an absorption unit with a rotor that is coupled to the device under test. It allows the device to rotate while applying a braking torque through various means to measure its performance characteristics.
1) The document discusses potential and kinetic energy, with a focus on using potential energy experiments involving trolleys rolling down slopes and pendulums to understand how potential energy is converted to kinetic energy.
2) It provides formulas for calculating potential energy (PE = mgh), kinetic energy (KE = 1/2 mv^2), and velocity (v = √2gh) and discusses their application to roller coaster design.
3) The steps outlined for a roller coaster design experiment involve calculating the potential and kinetic energy at various points and using that to determine the track design and roller coaster speed and energy requirements.
This document provides information about an experiment to determine the torsional vibration characteristics of single and double rotor systems. It includes the objectives, equipment description, procedures, sample calculations and observations. The experiment aims to determine the period and frequency of torsional vibration experimentally and compare to theoretical values. Key steps involve twisting and releasing rotors to measure oscillation times and calculating moments of inertia, torsional stiffness and natural frequencies.
This document discusses the design of an active electromagnetic suspension system for automotive applications. Key points:
- An active suspension system is proposed using a brushless tubular permanent magnet actuator in parallel with a passive spring. This provides additional stability during maneuvers like cornering and braking.
- Specifications for the actuator are derived based on measurements of forces during test drives. The actuator needs to produce peak forces of 4 kN and continuous forces of 1 kN to eliminate roll and pitch. It also needs to absorb road vibrations up to 2.05 kN.
- A quarter-car test setup is used to validate the improved performance of the active suspension system. Measurements show the roll angle is
This document summarizes an experiment on the impact of jets using a hydraulic bench. The experiment aims to demonstrate that the force on a vane is proportional to the rate of delivery of momentum from a jet. Students collect data on the distance moved by a jockey weight under different flow rates. The results show the force on the vane increases linearly with the rate of delivery of momentum from the jet, consistent with theoretical expectations, although actual forces measured are slightly lower than predicted.
Experimental Investigation of Multi Aerofoil Configurations Using Propeller T...ijceronline
This paper briefs about the performance test on multi aero foil configuration on propeller test rig. The airfoils used are a conventional airfoil , a airfoil with stepped configuration and a Clark y airfoil .They were tested for various speed and blade angles using propeller test rig. The result are compared and studied with the conventional airfoil configurations. In future Such Aerofoils can be used for wind Mills for producing the high Voltage Power.
The flow across an airfoil is studied for different angle of attack. The CFD analysis results are documented and studied for different angle of attack using fluent & gambit.
- Researchers at the University of Maryland tested a small-scale helicopter rotor in conditions simulating the Martian atmosphere to determine if a micro aerial vehicle could hover on Mars.
- Testing of a rectangular rotor planform in a vacuum chamber showed it could produce enough thrust to hover but with low figure of merit below 0.4. Predicted endurance was around 13 minutes.
- Additional testing showed performance significantly improved with higher Reynolds numbers, with figure of merit reaching a typical MAV value of 0.62.
- Further studies will parametrically evaluate different rotor designs including airfoil, planform shape, twist and solidity to optimize performance in the thin Martian atmosphere.
Development Of Tipper Unloading MechanismIRJET Journal
1. The document describes the development of a tipper unloading mechanism to allow a tipper truck to unload material in multiple directions rather than just the rear.
2. Currently, tipper trucks can only unload material out the back, which reduces efficiency when precise unloading locations are required. It also requires the truck be parked in certain positions.
3. The proposed design involves adding two additional hydraulic cylinders on the sides of the tipper bed, allowing material to be unloaded to the left or right as well as the rear. This would provide more flexibility in unloading location without repositioning the truck.
4. Calculations are provided for the existing rear unloading mechanism involving the hydraulic cylinder, motor,
PERFORMANCE AND ANALYSIS OF MILLING TOOLS DYNAMOMETERsathish sak
A Milling is the machining process of using rotary cutters to remove material from a work piece by advancing (or feeding) in a direction at an angle with the axis of the tool.
A dynamometer or "dyno" for short, is a device for measuring force, torque, or power. For example, the power produced by an engine, motor or other rotating prime mover can be calculated by simultaneously measuring torque and rotational speed (RPM).
Couette flow is the flow of a viscous fluid between two surfaces, one of which is
moving tangentially relative and another is fixed. The relative motion of the surfaces
imposes a shear stress that make flow possible.
Watch Video of this presentation on Link: https://youtu.be/bHKaPBgDk6g
For notes/articles, Visit my blog (link is given below).
For Video, Visit our YouTube Channel (link is given below).
Any Suggestions/doubts/reactions, please leave in the comment box.
Follow Us on
YouTube: https://www.youtube.com/channel/UCVPftVoKZoIxVH_gh09bMkw/
Blog: https://e-gyaankosh.blogspot.com/
Facebook: https://www.facebook.com/egyaankosh/
Preliminary Design of 100 Seater AircraftROSHAN SAH
This presentation explains the different design phases of aircraft and some detailed descriptions of each phase. Then, it explains the preliminary design procedure of the aircraft which consists of weight estimation, wing design, fuselage design, drag polar, maximum speed, thrust requirement and selection of engine, landing gear selection, tail surface design, and different performance calculations.
1. The document discusses various methods for measuring force, torque, and strain. It describes load cells, cantilever beams, proving rings, and differential transformers that can be used to measure force.
2. Methods for measuring torque and power are also presented, including absorption dynamometers, prony brake dynamometers, hydraulic dynamometers, and eddy current dynamometers.
3. The concept of strain and strain gauges for measuring strain are briefly covered at the end.
Watch Video of this presentation on Link: https://youtu.be/g8eJsznmsaY
For notes/articles, Visit my blog (link is given below).
For Video, Visit our YouTube Channel (link is given below).
Any Suggestions/doubts/reactions, please leave in the comment box.
Follow Us on
YouTube: https://www.youtube.com/channel/UCVPftVoKZoIxVH_gh09bMkw/
Blog: https://e-gyaankosh.blogspot.com/
Facebook: https://www.facebook.com/egyaankosh/
This document provides information on various methods for measuring force, torque, power, flow and temperature. It discusses direct and indirect methods for measuring force, including using spring balances, accelerometers, hydraulic load cells, pneumatic load cells and strain gauge load cells. It also describes techniques for measuring torque using rope brakes, hydraulic dynamometers and strain gauge transducers. Flow measurement is discussed for devices like venturi meters, orifice meters and rotameters. Temperature measurement techniques include bimetallic strips, thermocouples and resistance thermometers.
Measurement of force and torque and pressure standardsMech-4u
Measurement of Force and Torque and pressure Standards,
Measuring Methods,
study of different types of forces and torque Measuring systems.
Description and working Principle of different types of Transducers for Measuring Pressure.
Since the beginning of modern civilization,we are always dependent on fossil fuels as the source of energy for our daily requirements.over the past decade due to population expansion,we can notice the deplition of these fossile fules . therefore to reduce this deplition,energy harvesting has become one of the prime topic for this generation.the process of acquiring the energy surrounding the system and converting it into usefull electrical source is called energy harvesting.Piezoelectric materials have gained popularity in this section of energy harvesting,which can be used to store waste energy for future use.
In our project,Since we are using electric engine which is charged with the help of piezos and solar panels,it reduces pollution.Also it reduces usage of electricity since we are using piezo electricity and solar panels
Design, Analysis & Balancing of 5 Cylinder Engine CrankshaftIJMER
This document summarizes the design, analysis, and balancing of a 5 cylinder engine crankshaft. It discusses modeling the crankshaft in Solidworks and analyzing it in ANSYS using finite element analysis. Calculations are shown for designing the crankshaft and crankpin based on engine specifications. Loading and boundary conditions are applied for static structural analysis to determine stresses and deflection. Von Mises and shear stresses from the analysis match theoretical calculations. The conclusions are that finite element analysis is effective for determining permissible stresses and that the 5 cylinder design provides weight optimization and lower cost compared to a 6 cylinder configuration.
Detailed design calculations & analysis of go kart vehicleAvinash Barve
Go-kart is a compact four-wheeler racing vehicle. Go-kart having very low ground clearance and can be work on the only flat racing track. We will create a model using 3D CAD software such as CREO PARAMETRIC, SOLIDWORKS and ANSYS WORKBENCH after completing the modeling the design is tested against all types of failure, stresses, and deformation by using analysis software. Based on design calculation and analysis result can be changed as per further modifications in dimensions.
This presentation discusses the design of a solar car, including its technical specifications, suspension, and braking systems. It provides details on the motor, gearing, and torque requirements. A double wishbone suspension is proposed for the front with calculations provided for spring rates and roll centers. Disc brakes are planned for the front and drum brakes for the rear, with analyses of braking forces and torque. Ball joints and rod ends must withstand loads from the suspension and drivetrain.
Design and Fem Analysis of Car Alloy WheelIJERA Editor
The requirements for improved stiffness, reliability, fatigue life and increased efficiency involves challenges of developing innovative design solutions. The present work mainly focus on the design of car alloy wheel, where the analytical and FEM analysis approach was implemented to analyze baseline design. Initially static analysis was performed to obtain total deformation, strain and the stress of car alloy wheel. Three Dimensional model was created using CATIA and FE software ANSYS was used for discretization and analysis to obtain expected solution. The results were obtained through linear static analysis in terms of Total deformation while Minimum principal stress, Max Principal stress were found to be nearly equal for both 6 arms wheel and 4 arms wheel and 22.16 % of reduction in weight was observed and hence overall weight of the car alloy wheel was optimized.
Design and Fabrication of a Tricycle for Municipal Waste Collectioninventionjournals
ABSTRACT: The use of inappropriate technology for the primary collection of municipal wastes in general is a common problem. A tricycle was designed and fabricated with a carriage to be used for doorstep collection of waste. The tricycle was designed to be human powered for the purpose of primary collection of municipal solid waste in locations and communities where the existing collection trucks could not cover due to narrow, poor quality roads and a high density population and congested areas. The final result shows that the tricycle is stable, strong, durable, and the dynamic test conducted has confirmed the stability, easy maneuvering, and the effectiveness of the braking system. This research work is applicable to the reduction in the inefficiency with the existing methods and equipment used in the collection of municipal waste.
1) The document simulates testing of an ATV roll cage in ANSYS to evaluate its performance against crashes.
2) A model of the roll cage and vehicle is created using pipe, mass, and spring elements. The roll cage is tested under front impact, rear impact, side impact, torsional stiffness, front wheel bump, and rollover conditions.
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Design calculation & different analysis of hybrid vehicle
1. Design Calculation & Different
Analysis of Hybrid Vehicle
Presented by Avinash Barve
Authors,
Avinash Barve, Bhagyesh Talekar, Sanket Lakhe, Vaishnavi Ratanparaj, Rahul Jangam,
Hemant Bansod
Scholar(4th year) Mechanical Engineering
Scholar(4th year) Electronics and Telecommunication Engineering
Assistant professor, Mechanical Engineering
S. B. Jain Institute of Technology Management and Research Nagpur, India
2. Hybrid car is one which uses Two or more energy.
The electric power engine works at lower speed and gasoline engine at
higher speed
Hybrid engine automatically off while car is stopped and restart while
you accelerate
What is hybrid car?
3. DESIGN METHODOLOGY
Selection of material
and basic design of
chassis.
Calculations of impact
forces and impact time.
Analysis of chassis in
ANSYS software
Optimization and
repeat process until
satisfactory result.
Stresses and
deformation results.
4. Design Calculation and Analysis
CHASSIS • Material Selected for Chassis is AISI4130 & Body is Aluminum alloy.
• Design of chassis & body has been done on using SOLIDWORK V2016 and analysis is
done by using ANSYS WORKBENCH 16.2
Analysis: The following results are obtained when maximum forces applied on the chassis & Body.
1) Front Impact
Impact Total
Deformation
Equivalent-stress Safety Factor
Front 6.8966 mm 89.761Mpa 3.1194 mm
5. 2) Rear Impact
Impact Total
Deformation
Equivalent-stress Safety Factor
Rear 3.8131 mm 45.547Mpa 6.1475 mm
6. 3) Side Impact:
Impact Total
Deformation
Equivalent-stress Safety Factor
Side 6.1028 mm 156.94Mpa 1.7841 mm
7. 4) Model Analysis
The following result is found by applying the
possible maximum frequency.
Sr. no. Frequency Total deformation
1. 57.51 Hz 3.211 mm
8. BRAKE:
• The Type of brake used in this vehicle is disc brake of APACHE RTR 160.
• The CAD model of the brake is made in SOLIDWORKS 2016 and its
analysis and its thermal analysis is performed on ANSYS WORKBENCH
Brake Disc Calculation
Mass of the vehicle = 230kg
Initial velocity (u) = 11.11 m/s
Final velocity (v) = 0 m/s
Brake rotor diameter = 0.13m
Coefficient of friction between pad and rotors (γ) =0.3
Percentage of kinetic energy that disc absorbs (90%) = K =0.9
Coefficient of friction for dry pavement µ = 0.9
Stopping distance S = u2 /2gµ = (11.11)2 /2*9.81*0.9
S = 6.99 m
Deceleration of vehicle a = v2 -u 2 /2*S
a= 02 -(11.11)2 /2*6.99
a = 8.82 m/s
Stopping time V =u + at
0 =11.11+8.82*t
t=1.25 sec
a. Energy generated during braking
b. K.E. =γ K* m (u-v)2 /2
c. K.E. =3832.56 J
d. b. Brake power
e. Pb=K.E. /t
f. Pb=3066.04 W
g. c. calculate the heat flux (Q)
h. Q =Pb/A
i. Q =235849.2 W/m2
9. Brake Analysis:
The following results are obtained from
Brake Thermal Analysis
Sr.
no.
Temperature Total Heat flux
1. 180.63 °C 2.914 x 105 W/m2
10. STEERING:
• The main function of the steering system is to guide the vehicle in desired direction as per the
requirement.
Steering Calculation
Wheel Base (L) = 64 inch= 1625.6 mm Front
Track Width (a) = 1220 mm
Rear Track width (b) = 1280 mm
Inner steering angle = ⍬
Outer steering angle =φ
Slip angle α = tan-1 (0.5*front track width
(a)/wheel base (L))
Slip angle α = 20.56º
According to Ackermann’s steering method,
Now, assuming⍬⍬ = 35º and α = 20.56º Hence,
cotφ – cot⍬⍬ = (b/L)
cot (φ) – cot (35) = 1280/1625.6
φ = 24.29º
Maximum Turning Radius
Sinα = w/R = a/R
Therefore R = a/sinα
= 1220/sin(20.56)
Maximum Turning Radius =3473.92mm
=3.473m
Minimum Turning Radius
Tanα = w/R = a/R
Therefore R = a/tanφ
= 1220/tan (20.56)
Minimum Turning Radius = 3252.65mm
= 3.252m
11. Structural analysis of stub axle of wheel: Analysis at Lateral Force ( During turning):
The maximum force is applied on the wheel
stub axle and calculated the result as shown
below.
The maximum force is applied during the turning of
the wheel and tested which gave result as follows.
Force Total
deformation
Equivalent-
stress
353.16
N
0.010062
mm
6786.Mpa
Force Total
deformation
Equivalent-
stress
416.88N 0.0042911m
m
4.2625Mpa
12. Analysis of wheel hub:Structural Analysis of stub arm:
The Tie-rod force is applied on stub arm and tested to get the following result.
Force Total
deformatio
n
Equivalent-
stress
416.88N 0.0086103
mm
13.067Mpa
13. Suspension:
• Suspension is one of the important part of the vehicle it allows relative motion
between the wheels and the vehicle the type of suspension used depends upon
low forces are transferred form the wheels to the chassis
• The points at which the wishbone is connected to the chassis is located by using
LOTUS V5 called as suspensions point.
14. Conclusion
By the concept of hybrid technology, the problem of energy crises and pollution of
environment can be minimized.
The model of chassis and body, hub , suspension, knuckle and disc plate is
designed by using solid works 2016 and cero parametric 2.0
Analysis of chassis & body , hub , knuckle and temp analysis of disc brake had
been done by using ANSYS 16.2
Suspension analysis had been performed by using LOTUS Software
Based on result obtained dimension can be modified as per further requirement.