Showing posts with label Assignments. Show all posts
Showing posts with label Assignments. Show all posts

Thursday, 16 January 2014

Fused Deposition Modeling: Summary + Process

After analyzing the steps involved in rapid prototyping, let us move to an important rapid prototyping process: Fused Deposition Modeling (FDM).

Actually FDM is the second most widely used rapid prototyping technology. In it a plasitc filament is melted down and this melted plastic is sent to a nozzle. This nozzle extrudes the melted plasitc by moving in a plane. Due to simultaneous action of movement and extrusion a thin layer is formed. This melted plastic solidifies immediately. ABS is the most suitable plastic for this process. Sometimes a companion material is introduced to support the layer of melted plastic. This companion material also enhances the temperature bearing capacity and strength of the solidified layer. We can implement this method for the manufacture of small products also. Here is a brief review of procedural steps of FDM:

A CAD file is converted into .stl format. This file is sliced into layers. At the same time, tool path is programmed using SML language. Molten plastic is extruded out of a nozzle which is moving along the path programmed earlier. Another nozzle is used to extrude the companion material. Layers formed according to the inputted sliced model. These layers fused together to build up the 3D model of the design. After that companion material is removed, and the model is ready after removal from the fabrication platform.

Material Used in FDM process: Acrylonitrile Butadiene Styrene (ABS)

The chemical formula of this material is : C8H8 . C4H6 . C3H3N. This material is light and rigid. It is a synthetic monomer. The main advantage of ABS is that it combines the strength and rigidity of acrylonitrile and styrene with toughness of polybutadiene. Here are some advantages of FDM:

This process is speedy, safe, environment friendly, clean, simple, easy and cost effective. Also no material removal is required. On the other hand the disadvantage of this process is: poor strength in vertical direction, slow for big part and accuracy is low.

The major problem to FDM is that the 3-D files we found are not always transferable to sliced model.

FDM begins with a software process which processes an STL file (stereolithography file format), mathematically slicing and orienting the model for the build process. If required, support structures may be generated. The machine may dispense multiple materials to achieve different goals: For example, one may use one material to build up the model and use another as a soluble support structure, or one could use multiple colors of the same type of thermoplastic on the same model.

The model or part is produced by extruding small beads of thermoplastic material to form layers as the material hardens immediately after extrusion from the nozzle.

A plastic filament or metal wire is unwound from a coil and supplies material to an extrusion nozzle which can turn the flow on and off. There is typically a worm-drive that pushes the filament into the nozzle at a controlled rate.

The nozzle is heated to melt the material. The thermoplastics are heated past their glass transition temperature and are then deposited by an extrusion head.

The nozzle can be moved in both horizontal and vertical directions by a numerically controlled mechanism. The nozzle follows a tool-path controlled by a computer-aided manufacturing (CAM) software package, and the part is built from the bottom up, one layer at a time. Stepper motors or servo motors are typically employed to move the extrusion head. The mechanism used is often an X-Y-Z rectilinear design, although other mechanical designs such as deltabot have been employed.

Although as a printing technology FDM is very flexible, and it is capable of dealing with small overhangs by the support from lower layers, FDM generally has some restrictions on the slope of the overhang, and cannot produce unsupported stalactites.

Myriad materials are available, such as ABS, PLA, polycarbonate, polyamides, polystyrene, lignin, among many others, with different trade-offs between strength and temperature properties

Wednesday, 15 January 2014

What is Reynolds Number? Do you think that Reynolds Number has most important impact on incoming jet? Can it be changed in any design compatible to orifice parameters?

Reynolds Number:

It is a dimensionless number which represents the ratio between inertial forces and viscous forces. Actually it tells us the relative effect of inertial forces and viscous forces acting on the moving fluid. Before further elaborating the idea of Reynolds number let us see that what are inertial force and viscous force?

Inertial Force:

It is the force exerted by any fluid by virtue of its state of motion. Suppose a fluid is moving at high velocity then, due to inertia, we are in need of a force to stop that moving fluid at an instant. More is the mass of fluid, more is the force needed to stop it. This is the force that is exactly equal to inertial force in magnitude but will not be the inertial force. So the force which backups or supports the flow of that corresponding fluid is known as inertial force. Here is another important point to note that as the force is given by the product of mass and acceleration, so if velocity of the moving fluid is constant than no inertial force acts on that fluid because acceleration in zero. It only depends upon the rate at which velocity is changing with respect to time.

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Fig (1): fluid particles moving with constant velocity experience no inertial force.

Now let us see that what is viscous force?

Viscous Force:

It is the force which acts on the fluid due to the friction between the layers of the fluid. It can also be defined as the measure of the resistance to gradual deformation by shear stresses or tensile stresses. Actually these forces tend to nullify the relative movement of one layer of the fluid with respect to other layer due to friction between the layers. So we can deduce that more is the viscous force, less is the chance for the flow to become turbulent or chaotic.

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Fig (2): Friction between layers of fluid restricts the relative movement of layers.

Now let us analyze that either Reynolds number has most important impact on incoming jet or not.

Reynolds number’s impact on incoming jet:

Before going into detail let us first see that about which incoming jet we are talking here.

A jet is actually an efflux of fluid that is restricted to move through a medium i.e. nozzle or orifice. A jet is also characterized as a high speed flow with a very little loss in regularity even after covering a considerable amount of distance. So we can say that the flow which is going to become jet is incoming jet. Now we discuss the impact of Reynolds number on incoming jet. When a simple flow is converted into jet a very large change in velocity occurs. This ‘large change’ increases the inertial forces within the fluid and hence the chance for the flow to become turbulent arises. But as we know that jet flow is very similar to streamline flow due to its ability to sustain its original shape, so it is unavoidable to deduce that viscous forces also increase at this instant to balance the inertial forces to keep the fluid streamline. After conversion from simple flow to jet flow inertial forces approach zero because now fluid velocity is not changing too rapidly. After all this discussion we infer that it is not the Reynolds number which influences the incoming jet but actually it is the fluid itself and the condition of boundary through which it is passing which decides a particular type of flow of fluid in that particular scenario. We can say that Reynolds number is not governing the flow of fluid. On the other hand Reynolds number is self-governed by the conditions of the flowing liquid.

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Fig (3): jet flow of water

Keep in mind that Reynolds number can be used as a criterion to decide that, at a particular value of acceleration, whether the flow is turbulent or streamline. For example, low value of Reynolds number indicates that the corresponding flow is dominated by viscous force which results in streamline flow. On the other hand if the value of Reynolds number is sufficiently large then the corresponding flow is dominated by inertial force which results in turbulent flow. So understanding this predicting capability of Reynolds number we may conclude that Reynolds number influences the incoming jet of a fluid.

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Fig (4): Schematic of turbulent and laminar flow

Can Reynolds number be changed in any design compatible to orifice parameters?

Actually orifice is any opening through which something may pass. So that opening must have some particular geometric shape i.e. circular or rectangular. If it is circular, then the diameter of the orifice opening is an important design parameter. Also length plays important role as a design parameter. If the diameter of orifice is very small, then fluid passing through it must attain high magnitude of speed according to equation of continuity. This sudden increase in speed, increase the inertial forces within the fluid so that flow becomes turbulent. As Reynolds number is directly proportional to inertial force so the magnitude of Reynolds number also increases. We may prefer to select the Reynolds number as flow predicting criteria for the flow of corresponding liquid. So the Reynolds number impels us to choose appropriate dimensions for the orifice opening because just speed is not important. For example, in case of water turbine you may prefer a mechanism which produces high speed water jets to rotate the turbine blades but at the same time the prevalence of turbulence on fluid flow forces you to choose appropriate speeds to keep the flow streamline to avoid the phenomenon like back pressure etc... But if you want high speeds then you must decrease the density of that fluid or decrease the characteristic length of orifice or increase the viscosity of the fluid by proper amount. Decreasing the density is often practically impossible; also it is hard to change the viscosity of a fluid under specific conditions. The only thing which we can use to handle the flow is the diameter and characteristic length of orifice. By making a smart combination of orifice parameters with speed, viscosity and density of fluid we can achieve our goal.

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Fig (5): flow of fluid through the opening of orifice

Determination of the right method to calculate the velocity and pressure profile for installation of a water turbine

Actually water is a fluid and we know that a fluid cannot resists the deformation force i.e., it flows under the action of force. So we might expect that its shape will change continuously as long as the force is applied.

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Let us first see that what is a water turbine and what is its use. So that we can deduce that what are the possible modifications whose introduction can play positive role in our investigation process of measuring and analyzing the velocity and pressure for installation of water turbine.

The most basic purpose of a water turbine is to convert the potential energy of water (as well as kinetic energy of water) into electrical energy through a series of steps.

Before further proceeding, it is also important to know that what is meant by potential and kinetic energy of water.

We know that it is the intrinsic property of every massive body to attract each other by a force whose magnitude is governs by a particular law. Similarly the earth also attracts every other massive body (like water) through certain amount of force. So when water attains some height we might expect that this is done by working against the force of gravity. This work on the water in height attaining process develops a potential within the raised water to work on its surrounding by losing its height. This property is known as gravitational potential energy.

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Now let us move to kinetic energy. We know that it is the intrinsic property of every massive body to resist in its change of state; either it is state of rest or state of uniform motion with respect to a particular frame of reference. So when a massive body is moving with some speed then it resists anything which tries to resist its motion. The amount of resistance offered by moving water is also corresponds to kinetic energy. So when water is flowing with some speed then the kinetic energy of that flowing water impels it to work on anything which resists its flow.

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So now we are clear that what is the basic idea of potential energy and kinetic energy of water.

In simple words we can say that energy possessed due to height is known as potential energy of water and energy possessed due to speed is known as kinetic energy of the water.

So these properties help us to use the water for the production of electrical energy through water turbine.

As we are going to explore the pressure profile for installation of water turbine it is necessary to know that what is meant by pressure of water. We know that the molecules of a fluid behave dynamically i.e. the molecules are free to move relative to each other. We might expect that due to this dynamic behavior, molecules may collide with each other and also with the confining boundary. Due to collision of molecules with the confining boundary a force equal to rate of change of momentum of that molecule is exerted upon the boundary. This force per unit area of confining boundary is known as the pressure of the water. This pressure may be dynamic or static depending upon whether water is moving or not respectively.

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After knowing about the meaning of pressure of water, let us move to another concept known as pressure head. As we are dealing with the installation of a water turbine so this concept is very important for us. To know about pressure head let us investigate a situation in which a liquid of density ‘ℓ’ is poured into a vertical tube of x-sectional area ‘A’, until the tube is filled to a height ‘h’.

So, volume of liquid is given by

Volume = h A

It implies mass of liquid is

Mass = volume × density = h A ℓ

As we discussed earlier that earth, being a massive body, attracts all other massive bodies in his gravitational field. This force with which the earth attracts the other body is known as the weight of that body. So here the weight of the liquid exert a force ‘F’ on the base of the tube which is given by

F = mass × gravitational acceleration = m g = h A ℓ g

So pressure of the liquid is given by

P = F / A = h A ℓ g / A = h ℓ g

As we know that water is commonly treated as incompressible substance. So we can assume that the density of water is not changing during its interaction with the water turbine machinery and from above formula it becomes clear that the pressure may be quoted in terms of height ‘h’, the head of the liquid. This concept is referred as pressure head and it plays the key role in defining the efficiency and other parameters during the installation of a water turbine.

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From above discussion we are inferred that more is the head of the water more is the pressure exerted by the water at the base. So it impels us to choose a location for the installation of water turbine where a reasonable head is available.

After knowing that what we are going to do, let us move to the mechanism on which water turbine works so that we can analyze the role of pressure and velocity of water to make the installation of turbine perfect.

As we know that water moves from high altitude to low altitude in the form of rivers under the action of gravitational force of earth. There are two ways to utilize the energy of that water. First one is to directly put a mechanism in front of streams of flowing water so that water can work on that mechanism by losing its kinetic energy, and second one is to block that flow by some constraint to gain the pressure head, so that water can work on the mechanism by losing its potential energy.

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Commonly it is the second case which is preferable for the installation of water turbine. From previous discussion we see that pressure at the bottom of the water is directly proportional to the height of the head available there. You may conclude that it is very easy job to calculate the pressure by just measuring the head available there according to the formula, which we derived earlier

P = F / A = h A ℓ g / A = h ℓ g

Where

‘h’ represents the head available there

‘ℓ’ represents density of water and

‘g’ represents acceleration due to gravity.

You may be forced to suppose that as the water is an incompressible fluid so pressure only depends upon the height or head available there. But the measurement of the head is one of the most challenging tasks during the installation of water turbine. Review that the head is actually the water pressure, created by the difference in elevation between the intake of your pipeline and your water turbine. This difference in elevation can be measured as the vertical distance between the intake of your pipeline and your water turbine by using an altimeter. But this method is not too much accurate. For accuracy the method of “Direct height measurement” is used.

This method of measuring head requires an assistant. Take a tall poll with graduated measurements. For example a measuring tape affixed with a 6 to 7 meters long PVC pipe works well. The method is illustrated in the following figure.

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After each measurement, move the transit, or person with the sight level, to where the pole was, and begin again by moving the pole further downhill toward the generator site. Keep each transit or sight level setup exactly level, and make sure that the measuring pole is vertical. Take detailed notes of each measurement and the height of the level. Then, add up the series of measurements and subtract all of the level heights to find total head.

Another accurate method is the “water pressure measurement method”. Take one or more garden hoses or lengths of flexible plastic tubing to measure head. Run the hose (or tubing) from your proposed intake site to your proposed turbine location. If you attach multiple hoses together, make sure that each connection is tight and leak free. Attach an accurate pressure gauge to the bottom end of the hose, and completely fill the hose with water. Make sure that there are no high spots in the hose that could trap air. You can flush water through the hose before the gauge is connected to force out any air bubbles.

If necessary, you can measure total head over longer distances by moving the hose and taking multiple readings. Keep in mind, however, that there is less than 1/2 psi difference for every vertical foot. Except for very steep hillsides, even a 100-foot hose may drop only a few vertical feet. The chance for error significantly increases with a series of low-head readings. Use the longest possible hose, along with a highly accurate pressure gauge.

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After determining the head by using any of these methods another aspect highlights in front of us. Actually during the flow of water through intake of pipeline to turbine the friction plays an important role in reducing the pressure of the water more than usual as we calculated through our methods. It is also important to note that longer pipelines, smaller diameters, and higher flows create greater friction. So we must take into account the frictional loses, due to friction of water with the pipelines and the machinery of turbine, during the estimation of pressure head.

There is another aspect which highlights in front of us and that is when water flows from intake of the pipeline to turbine it still feels some additional resistance other than the resistance due to friction between pipeline and other components of turbine. Actually when some quantity of water is added to intake of pipeline, there is a resistance due to the pressure of the fluid that already exists in the pipe. Hence we must exert a force on water to overcome that resisting pressure. So it is very important to keep this factor also in mind during the calculation of pressure.

The life is not easy still. Actually when water strikes the turbine blades then another phenomenon highlights itself. This phenomenon is known as back pressure. Actually when water strikes with the blades of turbine then it exerts a pressure on the turbine as a result of which turbine also exerts an opposite and equal pressure on the water which greatly reduce net pressure across the turbine. So keep this in mind during the calculation of pressure head otherwise measurements are uncertain.

Keep in mind that as the time passes away or due to change in environmental conditions, the head of a water turbine may loses its height. So keeping this aspect in mind the pressure is analyzed at three heads which are classified as; high, low and medium heads. So another modification to pressure measuring technique is to take the weighted average of all the three pressures described above.

After the determination of correct way to measure the pressure across the water turbine and analyzing its role in mechanism of water turbine let us divert our intentions to velocity profile of water for the installation of water turbine.

Actually the water in dam retained the gravitational potential energy. When the water enters from intake of pipeline and moves to turbine its gravitational energy is gradually changed into kinetics energy and flow work. Depending upon the geometry of the pipeline and the velocity with which water is moving through the pipeline the flow may be steady or turbulent. It is the part of turbine designing process to design the pipelines of a water turbine such that the flow remains steady. But when water strikes with the blades of the turbine the flow becomes turbulent or chaotic. So if we have to measure the flow rate of water through the pipelines then it is not recommended that after taking the initial velocity as zero, take the final velocity at the point of collision between water and turbine blades because it is nearly impossible to analyze the turbulent flow by using ordinary techniques. There is one method to do so. This method comprises of dividing the whole flow into a large number of streamlines and then simulating them by using super computers.

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It is customary to define the efficiency of turbine in terms of following four parameters:

1- Flow rate

2- Head

3- Power output

4- Specific weight of water

Actually it is very important to measure the flow rate. But as we see earlier that it is very difficult to analyze the flow at turbine exit because of the conversion of flow from steady state to turbulent state. Also another important point is that after working on turbine the water exits from a tube known as draft tube. Here another problem occurs. The flow of water is converted into a very complex type of flow known as vortex flow. This flow is very difficult to analyze so if possible then design draft tube such that this type of flow doesn’t occurs, otherwise simulate this flow on super computers to get nearly accurate results.

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Keep in mind the friction between the water and pipeline during the estimation of flow rate otherwise calculations are uncertain to great extent.

The best method to estimate the change in velocity of flowing water is by using law of conservation of energy.

According to it the total mechanical energy of fluid with mass ‘m’ and pressure ‘P’, moving with velocity ‘v’, at a height ‘h’ from our reference point, and having density equal to ‘ℓ’ is given by:

Mechanical energy = kinetic + potential + flow work

= mv2/2 + mgh + mP/ℓ

By rearranging and considering water as incompressible liquid the above expression becomes

m (v2/2 + hg + P/ℓ) = constant

Expressing the above expression for two states, we get

(v12 – v22)/2 + (h1 – h2)g + (P1-P2)/ℓ = 0

This expression is known as Bernoulli’s equation

According to law of conservation of energy the sum off all these terms remain constant throughout the pipeline. But unfortunately the friction between the pipeline and water results in loss of energy. So keep the frictional effect in mind during applying law of conservation of energy for the calculation of velocity.

There is another factor which plays an important role during the calculation of flow of water through the pipelines. This factor is ‘viscosity’. Actually when water is moving, its constituent layers move over one another. This movement results in friction between the layers. Each layer tends to pull its slower neighbor along with him but the slower layer tends to act as a brake on the higher velocity layer. This frictional interaction between layers is characterized by viscosity. Actually law of conservation of energy assumes that the flowing water is ideal i.e., there is no frictional loses between the layers. But that is not true for practical situations. So keep this in mind during the calculation of flow from law of conservation of energy to avoid uncertainty.

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So now Bernoulli’s equation may be written as

V12/2 + h1g + P1/ℓ = v22/2 + h2g + P2/ ℓ + F12

Where F12 is the losses due to friction

Calculations of the energy in flowing water rely upon the Bernoulli equation, which represents the total energy as the sum of the velocity head, the pressure head, and an elevation relative to some fixed datum. The change in energy is equal to the change in this sum. Bernoulli derived one of the three familiar expressions of energy as:

Hv = V2/2g

Where:

– Hv is velocity head
– V is velocity
– g is the acceleration of gravity

But there is one problem. Use of average velocity yielded an incorrect estimate of total kinetic energy of water.

So another scientist named Gaspard Gustavo de Carioles formulated the expression by introducing a correction factor to Bernoulli’s equation as follows:

Hv = aVavg2/2g

Introduction of this correction factor reduces the uncertainty in calculation of velocity profile.

4 stroke diesel engine

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A diesel engine (also known as a compression-ignition engine) is an internal combustion engine that uses the heat of compression to initiate ignition to burn the fuel, which is injected into the combustion chamber.

Difference between diesel and petrol engine:

The only difference between Diesel Engine and Petrol Engine is the way through which combustion of fuel take place. In Petrol Engine combustion of fuel takes place by first compressing it and then igniting it from a spark plug. In Diesel Engine combustion of fuel starts automatically when it take it into contact with highly compressed air.

4- Stroke diesel engine cycle:

1-2 Isentropic Compression                                                                                                         2-3 Constant P Heat Add                                                                                                             3-4 Isentropic Expansion                                                                                                             4-1 Constant V Heat Reject

…………   P-V diagram   ………….

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…………. T-S diagram   …………..

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Efficiency of diesel engine:

Thermal efficiency of 4 Stroke diesel engine can be calculated as follows.

If

qin = net heat input

qout = net heat output

Then

Thermal Efficiency = (qin - qout ) / qin

Superiority of diesel engine over petrol engine:

Diesel engine is superior than petrol engine because Cost of diesel is low, Compression ratio is too much high, Diesel cycle is more realistic than Otto cycle etc.

Strokes of 4 stroke diesel engine:

1- Intake Stroke

2- Compression Stroke

3- Power Stroke

4- Exhaust Stroke

Intake Stroke:

This is the first movement of the piston. This is a downward motion of the piston that develops a vacuum in the cylinder. This vacuum pulls the air and fuel mixture into the cylinder through the open intake valve.

Compression Stroke:

During this second stroke, all valves are closed. This allows all of the piston's force to be used to compress the air and fuel mixture. As it is compressed, the mixture becomes more dense creating a more potent mixture for detonation.

Power Stroke:

Just before the piston reaches top dead center, the mixture is ignited due to high compression. The third stroke, the power stroke harnesses the energy of the explosion by allowing the piston to be forced downward from top dead center. This linear motion is changed to rotational motion by the crankshaft.

Exhaust Stroke:

The last stroke is the exhaust stroke. During this last upward movement of the piston the exhaust valve is open. The piston forces all of the burned gasses from the previous explosion out of the cylinder. The cycle is completed and can begin again.

Parts of 4 stroke diesel engine:

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Base

That is the lower portion of 4 stroke diesel engine and is used to envelope the sump.

Sump

That is used for the lubrication management of the engine. It is the limited space that is used to collect the lubrication liquid.

Fins

These are used to manage the temperature inside the engine.

Water hollow space

That is the space around the cylinder in which cooling fluid circulates, which cools the burnt air-fuel mixture inside the cylinder.

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              SUMP                                FINS

Driving Shaft

The shaft which is driven by expansion of piston is known as driving shaft

Fly Wheel

That is a rotating mechanical device which stores the energy.

Connecting Rod

It changes reciprocatory motion of piston into rotating motion of flywheel.

Cylinder

The potion in which diesel cycle executes is known as cylinder.

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Driving Shaft                Flywheel                        Connecting Rod

Piston

The device which compress the air-fuel mixture inside the cylinder is known as piston.

Intake Valve

The valve through which fuel enters the cylinder is known as intake valve.

Exhaust Valve

The valve through which fuel leaves the cylinder is known as exhaust valve.

Valve Springs

The springs which impel the valves to retain their original positions after their displacement directed by timing gears.

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        Piston                                       Valve                                       Spring

Cap

The cap with which valve springs are fixed.

Rocker Arm Nut

The nut with which a lever is attached, which transmits the motion

of cam to valve.

Air Filter

It filters the air which enters the cylinder of engine.

Intake Manifold

The path through which air – fuel mixture enters the cylinder.

Exhaust Manifold

The path through which air – fuel mixture exhausts to surrounding

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       Cap                 Nut                            Filter                      Manifold

Glow Plug

A glow plug is a device, used to pre ignite the fuel in engine.

Injector

That is a device which injects fuel inside the cylinder of engine.

Timing Gears

The gears which control the timing of intake and exhaust valve.

Pre-Combustion Chamber

The chamber in which air and fuel mix with each other just before combustion.

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     Plug                             Gears

Injection Pump Body

Part of the engine which controls the injection of fuel into the cylinder.

Cam Shaft

it controls the movement of valves by taking driving force from crankshaft.

Tappet

A lever or projecting arm that moves or is moved by contact with another part, usually to transmit motion, as between a driving mechanism and a valve.

Barrel

Hollow cylinder of engine

Piston Spring

The spring which moves piston to and fro.

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            Cam                                    tappet                      spring

Sector Gear

The gear system which deals with proper fuel ignition process.

Flow Rod

The rod whose movement cause gears to rotate.

Pressure Valve

The valve which adjusts the pressure of air – fuel mixture is known as pressure valve

Pressure Valve Spring

The springs which impel the pressure valve to retain their original positions after their displacement.

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    flow rod

Fuel Piping

The piping through which fuel is directed to cylinder

Exhaust Piping

The pipe through which burnt air-fuel mixture exhausts.

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    Fuel piping                                     Exhaust pipe

Experiments For Engineers …..

 

Experiment # 01

Objective:

1-To find the efforts required to raise a range of loads at a particular velocity ratio

2-To find the efficiency at each load

3-To find the effect of friction at each load

Background:

Consider two pulleys coupled by a belt, as shown below. Let the radii of one pulley is ‘a’ and the radii of other pulley is ‘b’. A flexible non-slip belt is used for the transmission of power from one pulley to other. The distance moved by the belt on circumference of each pulley is same.

Apparatus:

1- Pulleys                2- Belt

3- Vernier Calipers                  4- Loads

What is a pulley?

Basically a pulley is a mechanical device which is used to; lift a load by applying some effort. The basic aim is to keep the magnitude of applied effort as small as possible through clever design of pulley. Belts are used to transmit the power in all pulley mechanisms.

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Procedure:

First of all, fix a white paper on wall in alignment with the pulley mechanism. Apply a particular amount of load on loading hangers. Now apply weights, to ‘effort hangers’ until the loading hangers displaced slightly upward from their location. Note this distance and the corresponding effort to lift this load. Repeat this procedure for different values of load. Here again note the upward deflection and corresponding applied effort.

Observations and Calculations:

Distance moved when 0.7 N load is applied = 4mm

Distance moved when 1.0 N load is applied = 5mm

Distance moved when 1.5 N load is applied = 8mm

Efficiency = (work output/work input) × 100

Sr. No.

Load

 

Effort

Work Input

Work Output

Effort of Friction

 

Efficiency

1

           
2            
3            

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Error Analysis:

The slipping of belt on pulleys must be avoided. Also the movement of pulleys must be smooth to avoid the jerks and hence the uncertainty in measurement. Carefully note the displaced distance for accurate measurement. Weights must be applied gently on the hangers.

Comments:

It is a good experiment which tells us that how the clever arrangement of pulleys can be used for lifting maximum loads with minimum inputs.

---------------------------------------------------------------------------

Experiment # 02

Objective:

To investigate the belt drive and find the efficiency at each load

Background:

Consider two pulleys coupled by a belt, as shown below. Let the radii of one pulley is ‘a’ and the radii of other pulley is ‘b’. A flexible non-slip belt is used for the transmission of power from one pulley to other. The distance moved by the belt on circumference of each pulley is same.

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Apparatus:

1- Pulleys               2- Belt

3- Vernier Calipers       4- Loads

What is a pulley?

Basically a pulley is a mechanical device which is used to; lift a load by applying some effort. The basic aim is to keep the magnitude of applied effort as small as possible through clever design of pulley. Belts are used to transmit the power in all pulley mechanisms.

Procedure:

First of all, fix a white paper on wall in alignment with the pulley mechanism. Apply a particular amount of load on loading hangers. Now apply weights, to ‘effort hangers’ until the loading hangers displaced slightly upward from their location. Note this distance and the corresponding effort to lift this load. Repeat this procedure for different values of load. Here again note the upward deflection and corresponding applied effort.

Observations and Calculations:

· Distance Moved = 10mm, Load = 1N (Medium Pulley), Effort = 0.5 N (Rear Pulley)

· Distance Moved = 4mm, Load = 3N (Rear Pulley), Effort = 2.5N (Rear Pulley)

· Distance Moved = 10mm, Load = 4N (Front Pulley), Effort = 1N (Rear Pulley)

· Distance Moved = 10mm, Load = 3.5N, Effort = 2N

· Distance Moved = 5mm, Load = 2N, Effort = 1N

Efficiency = (work output/work input) × 100

Sr. No.

Load

 

Effort

Work Input

Work Output

Effort of Friction

 

Efficiency

Pulley Arrangement

               
               
               
             
               

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Error Analysis:

The slipping of belt on pulleys must be avoided. Also the movement of pulleys must be smooth to avoid the jerks and hence the uncertainty in measurement. Carefully note the displaced distance for accurate measurement. Weights must be applied gently on the hangers.

Comments:

It is a good experiment which tells us that how the clever arrangement of pulleys can be used for lifting maximum loads with minimum inputs.

Experiment # 03

Objective:

To find out pressure with a Bourdon Tube (pressure gauge) and compare this pressure with theoretical results

Background:

Actually pressure is defined as the ratio of applied force and corresponding area. Here we determine the applied pressure by subjecting a fluid (oil) to a pressure and balancing it with the applied pressure until the fluid attains equilibrium. At this instant, the applied pressure equals to the pressure of the oil and hence determined through the apparatus.

Apparatus:

1- Dead weight calibrator

2- Oil

3- Weights

4- Vernier calipers

What is a Pressure?

Pressure is defined as force per unit area. In other words, it tells us that if a particular amount of force is applied on a particular area then the concentration of force there is characterized as pressure.

image

Procedure:

Apply weights at the top of the area as shown in figure. Keep valve closed at this instant. After applying the mass open the valve such the piston moves downward under the action of weight on it until a point reaches where the pressure generated due to the applied weights is exactly equal to the pressure of the fluid in the other cylinder. This pressure is noted by the dial gauge. This gauge is calibrated in ‘bars’. So convert it into metric units. Compare these practically calculated values of pressure with theoretically calculated values.

Observations and Calculations:

Zero error of dial gauge = 0.05 bar

Mass of piston = 0.5 kg

Piston Diameter = 18 mm

Now to calculate the theoretical pressure acting on the piston, we use the definition of pressure

P = F/A

Force ‘F’ is given by

F = mass of applied weight × g

Area ‘A’ is given by

A = π × (piston diameter)2 / 4

Sr. No

Applied mass (Kg)

Applied Load (Applied mass × g)

Area

(m2)

Theoretical Pressure (N/m2)

Practical Pressure (bar)

Practical Pressure (N/m2)

Difference

               
               
               
               

Error Analysis:

Open the valve at appropriate time to avoid uncertainty. Estimate the error in dial gauge. Apply weights on piston gently. As the gauge is calibrated in ‘bar’, so keep in mind to convert the noted values into metric units.

Comments:

It is an accurate method of determining the pressure due to precise design of the apparatus.

Experiment # 04

Objective:

Determination of the operation and characteristics of three basic types of flow meter

Background:

Actually here we are going to analyze the flow rate of water by using three different types of flow meters which are as follows:

i- Venturi Meter

ii- Orifice Plate

iii- Rota Meter

Water enters the apparatus through the lower left-hand end and flows horizontally through a sudden enlargement into a transparent Venturi meter, and into an orifice plate, a 90º elbow changes the flow direction to vertical and connects to a variable area flow meter (Rota Meter). The static head at various points in the flow path may be measured on a manometer panel. The water flow through the apparatus is controlled by the delivery valve of the Hydraulics Bench and the flow rate may be confirmed by using the volumetric measuring tank of the Hydraulics Bench

image

Apparatus:

1- Hydraulics Test Bench

2- Stop Watch

Procedure:

Direct the flow of water from sump tank to volumetric tank by using discharge valve. Ensure the absence of bubbles from the flow of water. Now note the time taken by water to occupy a particular volume in volumetric tank by using stop watch. Also note the height of fluid, raised in the tubes of manometer by using the scale which is fixed behind them. Note the reading of orifice plate as well as Rota meter. Repeat this procedure for different volumes occupied by discharged water.

Observations and Calculations:

As we know that Bernoulli’s equation is given by

Continuity equation is given by

For Ideal Flow

For Actual Flow

Here

Cd = Coefficient of discharge = 0.98

D2 = Throat Diameter = 16mm ; D1 = Inlet Diameter = 26mm

At = Throat Area = 2.011 × 10-4m2 ; A1 = Inlet Area = 5.309 × 10-4m2

Ρ = density of water = 1000kgm-3

For Orifice plate coefficient of discharge = 0.63

Sr. No

Manometer Reading

A

B

G

H

Rota-meter Reading (L/min)

Volume Occupied (Liters)

Time taken (Sec)

         
         
         

After putting values flow rate for ideal flow comes out to be ‘18.13 L/min’ ………………………………………. While flow rate for actual flow from formula comes out to be ’17.77 L/min’………………………………………

Error Analysis:

Ensure the absence of air bubbles. Handle discharge valve appropriately.

Experiment # 05

Objective:

Determination of the coefficient of discharge of Venturi meter

Background:

Water enters the apparatus through the lower left-hand end and flows horizontally through a sudden enlargement into a transparent Venturi meter. The static head at various points in the flow path may be measured on a manometer panel. The water flow through the apparatus is controlled by the delivery valve of the Hydraulics Bench and the flow rate may be confirmed by using the volumetric measuring tank of the Hydraulics Bench

Apparatus:

3- Hydraulics Test Bench

4- Stop Watch

Procedure:

Direct the flow of water from sump tank to volumetric tank by using discharge valve. Ensure the absence of bubbles from the flow of water. Now note the time taken by water to occupy a particular volume in volumetric tank by using stop watch. Also note the height of fluid, raised in the tubes of manometer by using the scale which is fixed behind them. Repeat this procedure for different volumes occupied by discharged water.

image

Observations and Calculations:

As we know that Bernoulli’s equation is given by

Continuity equation is given by

For Ideal Flow

For Actual Flow

Here

Cd = Coefficient of discharge = 0.98

D2 = Throat Diameter = 16mm ; D1 = Inlet Diameter = 26mm

At = Throat Area = 2.011 × 10-4m2 ; A1 = Inlet Area = 5.309 × 10-4m2

Ρ = density of water = 1000kgm-3

For Orifice plate coefficient of discharge = 0.63

Sr. No

H1 (cm)

H3 (cm)

Volume Occupied (Liters)

Time taken (Sec)

         
         

After putting values ideal flow rate comes out to be ‘35.35 L/min’………………………

On the other hand actual flow rate is ’15.89 L/min’ ……………………….

So coefficient of discharge is ‘0.45’ …………………………….

Error Analysis:

Ensure the absence of air bubbles. Handle discharge valve appropriately.