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Tuesday, 23 September 2014

Pelton turbine design & basics


Pelton Turbine – The Basic Working Principle

Working principle of Pelton turbine is simple. When a high speed water jet injected through a nozzle hits buckets of Pelton wheel; it induces an impulsive force. This force makes the turbine rotate. The rotating shaft runs a generator and produces electricity.
Fig.1 Pelton wheel derives rotation from impulse force produced by the water jet
In short, Pelton turbine transforms kinetic energy of water jet to rotational energy.

Governing in Pelton Wheel

Demand of power may fluctuate over time. A governing mechanism which controls position of the spear head meets this requirement. With lowering power demand the spear head at water inlet nozzle is moved in. So that water flow rate is reduced. If power demand increases spear head is moved out this will increase the flow rate. Following figure illustrates this mechanism. The first position of the spear head produces a low flow rate, while the second position produces a high flow rate.
Fig.2 Water flow rate control in Pelton wheel by monitoring position of spear head
So in Pelton turbine synchronization between power demand and power supply is met by controlling the water flow rate. The same technique is used in other types hydroelectric turbines. If the power supply is more than the demand, then the turbine will run over speed otherwise in under speed. But such a governing mechanism in turn will balance the power supply and demand and will make sure that the turbine rotates at a constant specified RPM. This speed should also conforms to the power supply frequency. So this mechanism acts as a speed governing mechanism of Pelton wheel.

Number of Buckets in Pelton Wheel

One of the most important parameter of Pelton turbine design is number of buckets on the disk. If number of buckets is inadequate, this will result in loss in water jet. That means when one bucket departs from the water jet next bucket may not get engaged with the jet. This will result in loss in water jet for a small time duration, thus sudden drop in turbine efficiency. Following figure illustrates what happens when the number of buckets are lowered. With lowering number of buckets at some point of operation, complete water jet might be lost (3rd figure). So there should be an appropriate number of buckets, which will make sure that no water is lost (1st figure).
Fig.3 Effect of number of buckets on water-bucket interaction

Pelton Bucket - Design & Features

Most vital component of Pelton wheel is its bucket. Buckets are casted as single solid piece, in order to avoid fatigue failure. You can note that force acting on the turbine bucket is not constant with time. If you follow one particular bucket, it will have high force for a small time duration (at the time of jet impingement) after that a larger idle period where no jet interaction takes place. So the force acting on the bucket is also not constant. It varies with the time but it is having a cyclic nature. If bucket were made using pieces by welding attachment such cyclic fore will easily lead to premature fatigue failure.
Fig.4 Different views of Pelton bucket
Water jet is split into 2 equal components with help of a splitter. The special shape of bucket makes the jet turn almost 180 degree. This produces an impulsive force on bucket. Force so produced can easily be derived from Newton’s 2nd law of motion. Blade outlet angle close to 180 degree is usually used in order to maximize impulsive force.
A cut is provided on bottom portion of buckets. This makes sure that water jet will not get interfered by other incoming buckets.

Pelton – An Impulse Turbine

Since the water jet is always open to atmosphere, inlet and exit pressure of water jet will be same and will be same as atmospheric pressure. However absolute velocity of fluid will have huge drop from inlet to exit of bucket. This kinetic energy drop is the maximum energy the bucket can absorb.
So it is clear that Pelton turbine gains mechanical energy purely due to change in kinetic energy of jet, not due to pressure energy change. Which means Pelton turbine is a pure impulse machine.
Fig.5 Pressure and velocity variation across Pelton bucket
Impulse force produced by water jet is high when jet is having high velocity. Water stored at high altitude can easily produce high jet velocity. This is the reason why Pelton turbine is most suitable for operation, when water is stored at high altitude. You can easily understand why there is a nozzle fitted at water jet injection portion. Nozzle will increase velocity of jet further, thus will aid in effective production of impulse force.

Extracting Maximum Power from Water Jet

Pelton turbine design is always aimed at extracting maximum power from water jet, or maximizing efficiency. Power extracted by the bucket, P is product of jet impulse force and bucket velocity.
So power extraction is maximum when product of impulsive force and bucket velocity is maximum. Let's consider 2 different operating conditions.
  • Buckets are Held Stationary

  • If Pelton wheel buckets are held stationary, there will be a huge impulse force produced. But power extraction will be zero since buckets are not moving.
  • Bucket Speed Same as Jest Speed

  • If buckets are moving with same speed of jet, water jet won't be able to hit the bucket. This will lead to zero impulse force. Again power extraction will be zero.
Fig.6 Relative magnitude of bucket and jet velocity is important in power extraction from fluid
In short, power extraction is zero both at zero bucket speed and when bucket speed is same as jet speed. So with respect to jet to bucket speed ratio, power extraction will vary with as shown below.
Fig.7 This graph shows how power extraction from fluid varies with respect to bucket to jet velocity ratio
It is clear from the above graph that optimum power extraction happens in between. It can be shown using Euler's turbo machinery equation that maximum power extraction happens when bucket speed is half the jet velocity. So it is always desirable to operate Pelton wheel at this condition. Pelton turbines can give efficiency as high as 90 %, at optimum working conditions.

Tuesday, 8 July 2014

Factors Affacting Lubrication

Circulation and Heating in the Presence of Air
Heat is generated within the bearings by friction and heat conduction along the shaft. Oil is broken into droplets while it is flowing. This allows greater exposure to air. During operation, oxidation (combination of the oil molecules with oxygen) occurs. Fine metal particles resulting, from wear or contamination and water act as a catalyst (enhance the rate) to oxidation. The viscosity of oil increases with oxidation. Insoluble oxidation products such as varnish and sludge may settle out on governor components, in bearings, heat exchangers, and strainers. Their accumulation will interfere with governor operation and oil flow to the bearings.
Contamination
Water is the most prevalent contamination in turbine lubrication systems. Three common sources of water include:
  1. Leaking turbine and pump seals
  2. Condensation of humid air
  3. Water leaks in heat exchangers
Emulsion will form when the oil is mixed with water. The emulsion will separate quickly when the oil is new and clean. The water will settle in the reservoir where it can be removed by purification equipment. Oxidation or contamination of the oil will increase the tendency of the oil to emulsify. Emulsions can mix with insoluble oxidation products and dirt to form sludges. Water can combine with air to form red and black rust, which is similar in appearance to pipe scale. Particles of rust have the following effects:
  • Act as catalysts that increase the rate of oil oxidation.
  • Scratch the journals and cause excessive wear.
  • Get entrained into the small clearances of the governing system. This will cause sluggish operation and, in extreme cases, disasters (due to slow operation of the governing valve).
Oil can become contaminated by air to form “bubbly” oil. This oil is compressible and can cause sponginess in hydraulic controls. It may reduce the load-carrying capability of oil films. Entrained air increases the rate of oxidation. An excessive amount of air can generate foaming in the reservoir or bearing housings.

Steam Turbine Lubricating oil Characteristics

Mostly turbine of steam power plant may have its rotational 3000 rpm to produce required power. Due to friction the temperature of bearing, rotor may increase which, combined with other factors, may leads to the failure of bearing hence produce a serious damage to turbine and plant. Plant stability, production depends on the turbine and turbine stability depends on bearing life as bearing will always be damage first. This causes the shutdown of power plant and hence gives a loss of money. Lubricant has vast effect on the life of bearing that’s why much care should be given while selecting it. We are going to be familiar with some of the properties, a lubricant should have.
Viscosity
The journal and thrust bearings of steam turbines require lubrication. Oils having higher viscosity provide a greater margin of safety in the bearings. However, its friction losses are high. In high-speed turbines, the heat generation becomes significant. Most oils used in this service have International Organization for Standardization (ISO) viscosity grade 32. Higher viscosity is used in some applications, ISO viscosity grade 46 (41.4 to 50.6 cSt at 40°C).
Higher-viscosity oils are used for geared turbines to provide adequate lubrication for the gears. Most of these systems use oils of ISO viscosity grade 68 (61.2 to 74.8 cSt at 40°C). Some geared turbines cool the oil in a heat exchanger before delivering it to the gears. The increase in viscosity provides better protection for the gears.
Load-Carrying Ability
Steam turbines normally use mineral oils. Boundary lubrication conditions occur in turbines not equipped with lifts. Wear will occur under these conditions unless lubricants with enhanced film strength are used. The higher viscosity of cool oil provides the increase in load-carrying ability of the oil films needed during start-up. Additives are also frequently used in turbine oil to improve the film strength.
Oxidation Stability
The ability to resist oxidation is the most important characteristic of turbine oils. This property is important from the standpoint of retention of viscosity (resistance to the formation of sludges, deposits, and corrosive oil oxyacids) and retention of the ability to separate water, resist foam, and release entrained air.
Protection Against Rusting
Rust inhibitors are required from turbine oils to improve their ability to protect against rusting of ferrous surfaces. These inhibitors “plate out” on metal surfaces to resist the penetration of water.
Water-Separating Ability
New mineral oils usually resist emulsification when there is water ingress. Any emulsion formed breaks quickly. Some additives such as rust inhibitors increase the tendency of an oil to emulsify. Thus, additives should be selected carefully to ensure that the oil has good water-separating ability.
Foam Resistance
Turbine oils usually contain defoamants to reduce the foaming tendency. Since oxidation increases the tendency to foam, good oxidation stability is essential to maintain good resistance to foaming.
Entrained-Air Release
Entrained air can cause sponginess and delayed or erratic response. Some additives are known to degrade the ability of the oil to release entrained air. Thus, the additives selected for turbine oil should not reduce its ability to release air.
Fire Resistance
Fire-resistant fluids (FRFs) are normally used in electrohydraulic governor control systems due to high pressures (up to 3000 psi). Phosphate esters or blends of phosphate esters and chlorinated hydrocarbons are normally used. These systems are extremely sensitive to the presence of solid contaminants. Considerable attention should be paid to the filtration of the oil.

Friday, 4 April 2014

Why compression ratio of petrol engine is kept low compared to diesel engine?

What is the need of high compression ratio? 
Today every machine is expected to give higher efficiency. When we talk about petrol engine and diesel engine whose thermal efficiency is directly related to 'compression ratio'. That means if we want to achieve higher thermal performance in terms of efficiency, we should provide high compression ratio for both the engine. 
What is compression ratio? 

The compression ratio is the ratio of total volume of engine cylinder to the clearance volume of the same cylinder.  As the name suggest, it relates compression of the air fuel mixture during compression stroke. When there is compression, there always be heat associated with and it increases the overall temperature of fuel air mixture.

Why compression ratio of petrol engine is kept low compared to diesel engine?

In petrol engine, petrol is used as fuel and when it is subjected to high compression ratio, the heat generated may increase the temperature of petrol+air mixture above the auto ignition temperature of petrol ( 280 °C) and the fuel mixture will automatically ignite without getting sparked.

This auto ignition produces very high pressure which may burst piston. This phenomenon is called 'detonation'. So, to reduce the detonation effect and to allow the combustion in exactly after compression stroke, high compression ratio cannot be used in petrol engine. In case of otto engines, the compression ratio is of the order of 4 to 8.

Sunday, 23 February 2014

Solar Energy Materials And Solar Cells | Types Of Solar Cells

Solar radiation received on earth in just one hour is more than what the whole world’s population consumes in one year. 3,850,000 Exajoules (EJ) amount of solar energy received by Earth Surface per year. In 2011, worldwide primary energy consumptions was 550 EJ. 7 hours of Solar Energy at Deserts can meet annual global energy requirement.
Note: 1 EJ = 10 18 J
(i.e in the order, Joule (J), Kilo Joule, Mega joule, Giga Joule, Tera Joule, Peta Joule, Exa Joule, Zeeta Joule, Yotta Joule and so on.)
01-solar cell - photovoltaic cell - Photovoltaic unit - solar energy
What is Photovoltaics (“PV”)?
  • Photovoltaic (phōs) = light (@ Greek )and “voltaic” = electric (from Volta, Italian physicist)
  • Conversion of sun light directly into electricity through semi conductor materials
  • Electricity for 2 billion people around the world
image01-different types of photovoltaic cells-solar cells-silicon cells-thin films solar cells
What is Photovoltaic (PV) systems?
A PV system consist of:
  • Photovoltaic cells connected into modules and encapsulated Modules grouped into panels.
  • Panels groups into arrays,
  • A power conditioning unit,
  • Batteries.
01-photovoltaic system- solar cell - solar module - solar array
History of Photovoltaic’s:
In 1839, a young French physicist named Edmund Bacquerel discovered the photovoltaic effect. While working with two metal electrodes in an electricity-conducting solution, he noted that the apparatus generates voltage when exposed to light.
When 1904, Albert Einstein published a paper on the photoelectric effect, that the general scientific community stopped looking at photovoltaic as some type of scientific hoax.
1839        Becquerel:             Photogalvanic effiect
1873        Smith:                    Photoconductivity of Se
1883        Fritts:                     Se films solar cells
1946        Russel Ohl             Modern Solar cell Patent
1954        Bell Lab:                 6% Si solar cells
1959        Hoffman:               2% Si cells (industrial)
1966        NASA:                    1kW array
1974        Sunshine:              Alternatives to Si
1980                                       Thin-film 10% Cu2S/CdS
1985                                       High Efficiency 20%; Conc. 25% (Si)
1999                                       1GW installed (cumulative)
2007                                       ~3GW
2008                                       Sunpower 18.5% PV panel
2009                                       Low cost (<1$/wp) module by First solar
Note: Se – Selenide, Si – Silicon, CdS- Cadmium Sulfides, Cu2S- Copper Sulfides.
What is Solar Cell?
The basic component of a PV system is solar cell.
Two fundamental functions:
1. Photo-generation of charge carriers (electrons and holes) in a light-absorbing material
2. Separation of the charge carriers to a conductive contact to transmit electricity
If light with adequate energy falls onto silicon arranged to form a p-n junction and penetrates to a point near the junction, then, because of the photo-electric effect, it will create free electrons near the junction. These electrons immediately move under the influence of the p-n junction’s electric field. The electrons continue to move through the cell to the surface of the cell. On the way towards the surface of the cell some of the electrons may be re-absorbed by the silicon atoms, but many electrons still reach the surface of the cell. These electrons can be collected by a metallic grid and an electric current will flow if the grid is connected to the metal contact on the other side of the cell by an external circuit.
01-layout of solar cells-photo electric effect-electric circuit of solar cells
Photovoltaic Materials:
  • Crystalline silicon (c-Si)
  • Amorphous silicon (s-si)
  • Cadmium Telluride (CdTe)
  • Copper Indium Diselenide (CIS)
  • III-V Family (Gallium arsenide….)
  • Dye-Sensitised Solar Cells (DSSC)
  • Organic Photovoltaics (OPV)
01-types of solar cells - types of photovoltaic cells-crystaline solar cells-Amorphous solar cell-cadmium tellutide thin films

Wednesday, 8 January 2014

Build A Quadcopter From Scratch

Build a Quadcopter

How To Build A Quadcopter – Choosing Hardware

In this article I will be talking about quadcopter components and how to choose them. This is part of the tutorial series on how to build a quadcopter. In the next post I will be talking about software, how to go about the algorithm and programming.
If you are planning on building a quadcopter but not sure how, this is the right place for you. Doing research is pretty boring, so I am trying to put together a comprehensive tutorial about quadcopter, hope it helps you as much as it helped me.
Building a quadcopter from scratch takes a lot of time and effort. If you are inpatient, afraid of programming/maths and has a good budget, you can just buy a pre-built kit. You could get it assembled within minutes before it’s flying (For example, like this one). But I have to say, you are missing the fun part of building a quadcopter. From choosing the parts, designing the circuits, to programming, you will be involved in every aspect of building a quadcopter, and it’s FUN!
If you have any questions, feel free to ask on this quadcopter message board.

This blog post is divided into a three parts
  • What is a Quadcopter and How It Work
  • Quadcopter Components Introduction
  • Conclusion

What Is A QuadCopter and How It Works

QuadCopter is a helicopter with four rotors, so it’s also known as quadrotor. Because of its unique design comparing to traditional helicopters, it allows a more stable platform, making quadcopters ideal for tasks such as surveillance and aerial photography. And it is also getting very popular in UAV research in recent years.
The Quadcopters exist in many different sizes. From as small as a CD up to something as big as one meter in width.
tiny-quadcopter   large_Quad_Copter_01
On a regular helicopter has one big rotor to provide all the lifting power and a little tail rotor to offset the aerodynamic torque generated by the big rotor (without it, the helicopter would spin almost as fast as the propeller)
Unlike a helicopter, a quadrotor has four rotors all work together to produce upward thrust and each rotor lifts only 1/4 of the weight, so we can use less powerful and therefore cheaper motors. The quadcopter’s movement is controlled by varying the relative thrusts of each rotor.
These rotors are aligned in a square, two on opposite sides of the square rotate in clockwise direction and the other two rotate in the opposite direction. If all rotors turn in the same direction, the craft would spin would spin just like the regular helicopter without tail rotor. (if you are not sure what I mean, check out this video) Yaw is induced by unbalanced aerodynamic torques. The aerodynamic torque of the first rotors pair cancelled out with the torque created by the second pair which rotates in the opposite direction, so if all four rotors apply equal thrust the quadcopter will stay in the same direction.
quadcopter-station
To maintain balance the quadcopter must be continuously taking measurements from the sensors, and making adjustments to the speed of each rotor to keep the body level. Usually these adjustments are done autonomously by a sophisticated control system on the quadcopter in order to stay perfectly balanced. A quadcopter has four controllable degrees of freedom:Yaw, Roll, Pitch, and Altitude. Each degree of freedom can be controlled by adjusting the thrusts of each rotor.

  • Yaw (turning left and right) is controlled by turning up the speed of the regular rotating motors and taking away power from the counter rotating; by taking away the same amount that you put in on the regular rotors produces no extra lift (it won’t go higher) but since the counter torque is now less, the quadrotor rotates as explained earlier.3.- control becomes a matter of which motor gets more power and which one gets less.
  • Roll (tilting left and right) is controlled by increasing speed on one motor and lowering on the opposite one.
  • Pitch (moving up and down, similar to nodding) is controlled the same way as roll, but using the second set of motors. This may be kinda confusing, but roll and pitch are determined from where the “front” of the thing is, and in a quadrotor they are basically interchangeable; but do take note that you have to decide which way is front and be consistent or your control may go out of control.
quadcopter-rotating
quadcopter-foward
For example, to roll or pitch, one rotor’s thrust is decreased and the opposite rotor’s thrust is increased by the same amount. This causes the quadcopter to tilt. When the quadcopter tilts, the force vector is split into a horizontal component and a vertical component. This causes two things to happen: First, the quadcopter will begin to travel opposite the direction of the newly created horizontal component. Second, because the force vector has been split, the vertical component will be smaller, causing the quadcopter to begin to fall. In order to keep the quadcopter from falling, the thrust of each rotor must then be increased to compensate.
This illustrates how the adjustments made for each degree of freedom must work together to achieve a desired motion. Now, building and flying a quadrotor from a remote control is simple and fun and stuff, but people noting the inherently stable flight (in theory with equal speed of the motors the thing keeps itself level) and ease of control (only three functions and they are all basically take speed from one and put in the other), people love to make them autonomous (flies itself) and semi-autonomous (at least keeps itself level by responding to disturbances and error).

Quadcopter Components Introduction

There are sensors connected to a microcontroller to make the decision as to how to control the motors. Depending on how autonomous you want it to be, one or more of these sensors are used in combination.
In this section, I will talk about these essential quadcopter components:
  • Frame – The structure that holds all the components together. They need to be designed to be strong but also lightweight.
  • Rotors – Brushless DC motors that can provide the necessary thrust to propel the craft. Each rotor needs to be controlled separately by a speed controller.
  • Propeller
  • Battery – Power Source
  • IMU – Sensors
  • Microcontroller – The Brain
  • RC Transmitter
  • Optional
Before we go into explaining how to choose each components, we can take a look some quadcopters that people have built, and the parts they used to get a rough idea. I didn’t build these planes, so I can’t guarantee their performance.
Multicopter Examples Page

Frame

Frame is the structure that holds all the components together. The Frame should be rigid, and be able to minimize the vibrations coming from the motors.
Aluminium-Frame
A QuadCopter frame consists of two to three parts which don’t necessarily have to be of the same material:
  • The center plate where the electronics are mounted
  • Four arms mounted to the center plate
  • Four motor brackets connecting the motors to the end of the arms
Most available materials for the frame are:
  • Carbon Fiber
  • Aluminium
  • Wood, such as Plywood or MDF (Medium-density fibreboard)
Carbon fiber is most rigid and vibration absorbent out of the three materials but also the most expensive.
Hollow aluminium square rails is the most popular for the QuadCopters’ arms due to its relatively light weight, rigidness and affordability. However aluminium could suffer from motor vibrations, as the damping effect is not as good as carbon fiber. In cases of severe vibration problem, it could mess up sensor readings.
Wood board such as MDF plates could be cut out for the arms as they are better at absorbing the vibrations than aluminium. Unfortunately the wood is not a very rigid material and can break easily in quadcopter crashes.
Although it is not as important as for the arms which of the three material to use for the center plate, plywood is most commonly seen because of its the light weight, easy to work with and good vibration absorbing features.
As for arm length, the term “motor-to-motor distance” is sometimes used, meaning the distance between the center of one motor to that of another motor of the same arm in the QuadCopter terminology.
QuadCopter-M2M-Distance
The motor to motor distance usually depends on the diameter of the propellers. To make you have enough space between the propellers and they don’t get caught by each other.
[Give example]

Brushless Motors

A little background of Brushless motor. They are a bit similar to normal DC motors in the way that coils and magnets are used to drive the shaft. Though the brushless motors do not have a brush on the shaft which takes care of switching the power direction in the coils, and this is why they are called brushless. Instead the brushless motors have three coils on the inner (center) of the motor, which is fixed to the mounting.
brushless_motor_1
On the outer side it contains a number of magnets mounted to a cylinder that is attached to the rotating shaft. So the coils are fixed which means wires can go directly to them and therefor there is no need for a brush.
brushless_motorBrushlessMotor
Generally brushless motors spin in much higher speed and use less power at the same speed than DC motors. Also brushless motors don’t lose power in the brush-transition like the DC motors do, so it’s more energy efficient.
Brushless motors come in many different varieties, where the size and the current consumption differ. When selecting your brushless motor you should take care of the weight, the size, which kind of propeller you are going to use, so everything matches up with the current consumption. When looking for the brushless motors you should notice the specifications, especially the “Kv-rating“.
The Kv-rating indicates how many RPMs (Revolutions per minute) the motor will do if provided with x-number of volts. The RPMs can be calculated in this way: RPM=Kv*U An easy way to calculate rating of motor you need, check out the online calculator eCalc. It’s an amazing tool that helps you decide what components to purchase depending on the payload that you want to carry.
Make sure you buy the counter-rotating to counteract the torque effect of the props.
I have written a more complete guide on how to choose Motor and propeller.

Propellers

On each of the brushless motors there are mounted a propeller.
You might not have noticed this on the pictures, but the 4 propellers are actually not identical. You will see that the front and the back propellers are tilted to the right, while the left and right propellers are tilted to the left.
Like I mentioned before, 2 rotors rotates in the opposite directions to the other two to avoid body spinning. By making the propeller pairs spin in each direction, but also having opposite tilting, all of them will provide lifting thrust without spinning in the same direction. This makes it possible for the QuadCopter to stabilize the yaw rotation, which is the rotation around itself.
images
The propellers come in different diameters and pitches (tilting). You would have to decide which one to use according to your frame size, and when that decision is made you should chose your motors according to that. Some of the standard propeller sizes used for QuadCopters are:
  • EPP1045 10 diameter and 4.5 pitch  this is the most popular one, good for mid-sized quads
  • APC 1047 10 diameter and 4.7 pitch  much similar to the one above
  • EPP0845  8 diameter and 4.5 pitch  regularly used in smaller quads
  • EPP1245  12 diameter and 4.5 pitch  used for larger quads which requires lot of thrust
  • EPP0938  9 diameter and 3.8 pitch  used in smaller quads
Aerodynamics is just way too complex for non-academic hobbyists. It’s even unlikely we can explain all that theory stuff in a few words. But in general when selecting propellers you can always follow these rules:
  1. The larger diameter and pitch the more thrust the propeller can generate. It also requires more power to drive it, but it will be able to lift more weight.
  2. When using high RPM (Revolutions per minute) motors you should go for the smaller or mid-sized propellers. When using low RPM motors you should go for the larger propellers as you can run into troubles with the small ones not being able to lift the quad at low speed.

Analysis of Propeller Pitch, Diameter, and RPM

Pitch VS Diameter: the diameter basically means area while pitch means effective area. So with the same diameter, larger pitch propeller would generate more thrust and lift more weight but also use more power.
A higher RPM of the propeller will give you more speed and maneuverability, but it is limited in the amount of weight it will be able to lift for any given power. Also, the power drawn (and rotating power required) by the motor increases as the effective area of the propeller increases, so a bigger diameter or higher pitch one will draw more power at the same RPM, but will also produce much more thrust, and it will be able to lift more weight.
In choosing a balanced motor and propeller combination, you have to figure out what you want your quadcopter to do. If you want to fly around stably with heavy subject like a camera, you would probably use a motor that manages less revolutions but can provide more torque and a longer or higher pitched propeller (which uses more torque to move more air in order to create lift).

ESC – Electronic Speed Controller

The brushless motors are multi-phased, normally 3 phases, so direct supply of DC power will not turn the motors on. Thats where the Electronic Speed Controllers (ESC) comes into play. The ESC generating three high frequency signals with different but controllable phases continually to keep the motor turning. The ESC is also able to source a lot of current as the motors can draw a lot of power.
ESC-Turnigy-Plush
The ESC is an inexpensive motor controller board that has a battery input and a three phase output for the motor. Each ESC is controlled independently by a PPM signal (similar to PWM). The frequency of the signals also vary a lot, but for a Quadcopter it is recommended the controller should support high enough frequency signal, so the motor speeds can be adjusted quick enough for optimal stability (i.e. at least 200 Hz or even better 300 Hz PPM signal). ESC can also be controlled through I2C but these controllers are much more expensive.
When selecting a suitable ESC, the most important factor is the source current. You should always choose an ESC with at least 10 A or more in sourcing current as what your motor will require. Second most important factor is the programming facilities, which means in some ESC you are allowed to use different signals frequency range other than only between 1 ms to 2 ms range, but you could change it to whatever you need. This is especially useful for custom controller board.

Battery

As for the power source of the quadcopter, I would recommend LiPo Battery because firstly it is light, and secondly its current ratings meet our requirement. NiMH is also possible. They are cheaper, but it’s also a lot heavier than LiPo Battery.
Battery-Zippy-4000

Battery Voltage

LiPo battery can be found in a single cell (3.7V) to in a pack of over 10 cells connected in series (37V). A popular choice of battery for a QuadCopter is the 3SP1 batteries which means three cells connected in series as one parallel, which should give us 11.1V.

Battery Capacity

As for the battery capacity, you need to do some calculations on:
  • How much power your motors will draw?
  • Decide how long flight time you want?
  • How much influence the battery weight should have on the total weight?
A good rule of thumb is that you with four EPP1045 propellers and four Kv=1000 rated motor will get the number of minutes of full throttle flight time as the same number of amp-hours in your battery capacity. This means that if you have a 4000mAh battery, you will get around 4 minutes of full throttle flight time though with a 1KG total weight you will get around 16 minutes of hover.

Battery Discharge Rate

Another important factor is the discharge rate which is specified by the C-value. The C-value together with the battery capacity indicates how much current can be drawn from the battery.
Maximum current that can be sourced can be calculated as:
MaxCurrent = DischargeRate x Capacity
For example if there is a battery that has a discharge rate of 30C and a capacity of 2000 mAh. With this battery you will be able to source a maximum of 30Cx2000mAh = 60A. So in this case you should make sure that the total amount of current drawn by your motors won’t exceed 60A.
This tutorial about battery I found very informative.

IMU – Inertial Measurement Unit

The Inertial Measurement Unit (IMU) is an electronic sensor device that measures the velocity, orientation and gravitational forces of the quadcopter. These measurements allow the controlling electronics to calculate the changes in the motor speeds.
The IMU is a combination of the 3-axis accelerometer and 3-axis gyroscope, together they represent a 6DOF IMU. Sometimes there is also an additional 3-axis magnetometer for better Yaw stability (in total 9DOF).

How does IMU work

The accelerometer measures acceleration and also force, so the downwards gravity will also be sensed. As the accelerometer has three axis sensors, we can work out the orientation of the device.
Accelerometer-3-axis
A gyroscope measure angular velocity, in other words the rotational speed around the three axis.
Gyroscope-3-axis

Using Only Accelerometer?

With the accelerometer alone, we should be able to measure the orientation with reference to the surface of earth. But the accelerometer tends to be very sensitive and unstable sometimes, when motor vibration is bad, it could mess up the orientation. Therefore we use a gyroscope to address this problem. With both the accelerometer and gyroscope readings we are now able to distinguish between movement and vibration.

Using Only Gyroscope?

Since the gyroscope can tell us the rotational movement, why can’t we just use the gyroscope alone?
The gyroscope tends to drift a lot, which means that if you start rotating the sensor, the gyroscope will output the angular velocity, but when you stop it doesn’t necessarily go back to 0 deg/s. If you then just used the gyroscope readings you will get an orientation that continues to move slowly (drifts) even when you stopped rotating the sensor. This is why both sensors has to be used together to calculate a good and useful orientation.

Magnetometer

The accelerometer cannot sense yaw rotation like it can with roll and pitch, and therefore a magnetometer is sometimes used.
A magnetometer measures the directions and strength of the magnetic field. This magnetic sensor can be used to determine which way is south and north. The pole locations are then used as a reference together with the Yaw angular velocity around from the gyroscope, to calculate a stable Yaw angle.
I am trying to keep the theory and maths minimal here, and I will go into more detail in the next couple of tutorials.

Buying an IMU

These three sensors are available individually on the market. But it is easier for development to get an IMU sensor board with the first two sensors (6DOF) or all three sensors (9DOF).
9DOF-Stick-Front
The raw sensor boards can communicate with the microcontroller via I2C or analogue. Digital boards that support I2C is easier and faster for development, but Analogue ones are cheaper.
There are even complete IMU units with processor available. Usually the processor is a small 8-bit microprocessor which runs computations some kind of algorithms to work out the Pitch, Roll and Yaw. The calculated data will then be put out on a serial bus or sometimes also available by I2C or SPI.
The choice of IMU is going to narrow down what type of controller board you can use. So before purchasing an IMU boards you should find out information about the controller boards. Some controller boards even comes with built-in sensors.
Some commercially available IMU sensors boards:

IMU with processor:

Flight Controller – Controlling electronics

You can either buy a controller board that is specially designed for quadcopter or buy all the parts and assemble one yourself. Some of the controller boards already contain the required sensors while other requires you to buy these on a separate board.
Here is a comprehensive list of ready to go flight controller boards:
http://robot-kingdom.com/best-flight-controller-for-quadcopter-and-multicopter/
The AeroQuad MEGA Shield The AeroQuad board is a shield for the Arduino, either the Arduino UNO or the Arduino MEGA. The AeroQuad board requires the Sparkfun 9DOF stick which is soldered to the shield.
The ArduPilot board contains an ATMEGA328, the same as on the Arduino UNO. Like the AeroQuad shield this board doesn’t contain any sensors either. You would have to buy the ArduIMU and connect it to the board to use it.
The OpenPilot is a more advanced board which contains a 72MHz ARM Cortex-M3 processor, the STM32. The board also includes a 3-axis accelerometer and 3-axis gyroscope. Together with the board comes a great piece of software for the PC to calibrate, tune and especially set waypoints for your QuadCopter if you have installed a GPS module which I will be talking more about in the next section.

Make You Own Quadcopter Controller Board

Alternatively you can also use general purpose microcontroller, such as Arduino.
[Coming soon]

RC Transmitter

QuadCopters can be programmed and controlled in many different ways but the most common ones are by RC transmitter in either Rate (acrobatic) or Stable mode. The difference is the way the controller board interprets the orientations feedback together with your RC transmitter joysticks.
In Rate mode only the Gyroscope values are used to control the quadcopter. The joysticks on your RC transmitter are then used to control and set the desired rotation speed of the 3 axes, though if you release the joysticks it does not automatically re-balance. This is useful when doing acrobatics with your quadcopter as you can tilt it a bit to the right, release your joysticks, and then your quadcopter will keep that set position.
For the beginners the Rate mode might be too difficult, and you should start with the Stable mode. All the sensors are used to determine the quadcopters orientation in the stable mode. The speed of the 4 motors will be adjusted automatically and constantly to keep the quadcopter balanced. You control and change the angle of the quadcopter with any axis using the joystick. For example to go forward, you can simply tilt one of the joysticks to change the pitch angle of the quadcopter. When releasing the joystick, the angle will be reset and the quadcopter will be balanced again.
Check here for a more detailed RC transmitter article.

Optional Components

After buying all the necessary parts, and you are still not broke, you might consider other popular optional components such as GPS modules, ultrasonic sensors, barometers etc. They can enhance the performance of your quadcopter, and bring more features.
A GPS module talks to the satellite and retrieve accurate location information. We can use this information to calculate speed and path. It is especially useful for autonomous quadcopters which needs to know its exact position and which way to fly.
An ultrasonic sensor measures the distance to the ground, i.e. altitude. This is useful if you want to keep your quadcopter a certain distance from the ground without having to adjust the height it’s flying at constantly yourself. Most of these sensors has a range between 20cm to 7m.
When you gets higher, you might want to use a barometer. This sensor measures humidity and pressure to work out the altitude, so when the quadcopter is close to the ground (where these two factors doesn’t change much), it becomes ineffective. Therefore it is also common to use both of them at the same time.

Conclusion

Hopefully this article has given you a better understanding what each part of the quadcopter does, and how to go about selecting the right product for your quadcopter.
Please do not hesitate writing a comment or giving us some feedback on this article. The next post will be about the software side of the quadcopter.
If you are into FPV and Video taking, you might find this collection of FPV videos interesting