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    INTRODUCTION

    Mobiles play an important role in peoples everyday life and lots of

    communications are relayed through a mobile. The mobile charger is important

    accessory for its trouble free and efficient usage of various mobile activities.

    General problem that arises in mobile is quick discharge. While browsing the

    features in mobile continuously, battery gets discharged quickly and in such cases

    solar powered mobile chargers can be a better alternative to electrical mobile

    chargers.

    The solar charger can be powered via sun with a USB cable or directly to

    the wall.

    The utility of this development is mainly aimed at convenience of the user at

    following limitations.

    Not having charging adaptor

    Not having electrical connections.

    Not having sufficient sunlight.

    The various advantages of using solar energy over electrical energy in chargingthe mobile are

    It saves electrical energy.

    It is pollution free, natural and free of cost.

    Solar energy is renewable.

    Solar energy is also abundant and

    It prevents global warming.

    The project outlines the manufacturing of solar charger to charge the mobile

    using solar energy instead of electrical energy.

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    1.PHOTOVOLTAIC CELL

    1.1 INTRODUCTION

    The early development of solar technologies started in the year 1860s was driven

    by an expectation that coal would soon become scarce. However development of solar

    technologies stagnated in the early 20th century in the face of the increasing availability,

    economy, and utility of coal and petroleum.

    The term "photovoltaic" comes from the Greek (photo) meaning "light", and

    "voltaic", meaning electric, from the name of the Italian physicist VOLTAafter whom

    a unit of electro-motive force, the volt is named. The term "photo-voltaic" has been in usein English since 1849.

    In 1839, nineteen-year-old Edmund Becquerel, while experimenting with an

    electrolytic cell made up of two metal electrodes found that certain materials would

    produce small amounts of electric current when exposed to light. The photovoltaic cell

    was developed in 1954 at Bell Laboratories.

    The highly efficient solar cell was first developed by Daryl Chapin,

    Calvin Souther Fuller and Gerald Pearson in 1954 using diffused silicon

    p-n junction.

    The sun is 150 million km from the earth and is 5 billion years old. The

    temperature of the sun ranges from 6000 degrees Celsius at its surface to 10 million

    degrees Celsius at its centre. It takes about 8 minutes for the light energy to touch the

    earth.

    The sun is a star made up of hydrogen and helium gas and it radiates an

    enormous amount of energy every second and it is clean. Solar poweris the conversion

    of sunlight into electricity either directly using photovoltaic (PV), or indirectly using

    concentrated solar power (CSP). CSP systems use lenses or mirrors and tracking systemsto focus a large area of sunlight into a small beam. PV converts light into electric current

    using the photoelectric effect.

    Most commercially available solar cells are capable of producing electricity for at

    least twenty years without a significant decrease in efficiency. The typical warranty given

    by panel manufacturers is for a period of 25 30 years, wherein the output shall not fall

    below a specified percentage (around 80%) of the rated capacity.

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    1.2 PRINCIPLE OF PV CELL

    Solar cell works on the principle of photovoltaic effect. Sunlight is composed of

    photons, or "packets" of energy. These photons contain various amounts of energy

    corresponding to the different wavelengths of light. When photons strike a solar cell, they

    may be reflected or absorbed, or they may pass right through. When a photon is absorbed,

    the energy of the photon is transferred to an electron in an atom of the cell (which is

    actually a semiconductor). With its new found energy, the electron is able to escape from

    its normal position associated with that atom to become part of the current in an electrical

    circuit.

    Each cell is made of two layers with a barrier in between them. The first layer(Layer A) contains electrons that are free to move to the second layer (Layer B). The

    Layer B wants these electrons more than the first layer.

    Layer A electrons will migrate to

    Layer B automatically, no sunlight

    needed. Layer B now has the extra

    electrons. However, while layer B has a

    better grip on these electrons that Layer

    A, it can still lose them. This is due to

    the pull of the nucleus on theelectrons. So when sunlight hits Layer

    B the electrons are dislodged. Their

    natural response is to try to go back to

    the positively charged Layer A; they do

    this because they can now move.

    This is where the barrier layer

    comes in. This is a one-way gate for the

    electrons to go from Layer A to Layer

    B but NOT the other way. The only way for the electrons to get back to Layer A isthrough the wire joining the two. So a photovoltaic solar cell or panel of cells will only

    generate electricity if it is connected to a circuit; otherwise it will just heat up in the sun.

    Once the electrons have done some work, they will have lost the energy that the

    sunlight provided them with and they will return, exhausted, to Layer A where they go

    back to their parent metal atoms. As soon as they get there they feel the pull of Layer B

    and off they go again, for another round.

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    Fig 1: Principle of PV Cell

    If n- and p-silicon are combined, the differently charged free charge carriers

    are attracted to each other, move into the respective neighbouring area and so charge it

    with electricity. A strong, inner electric field is created at the boundary layer, theP-n crossover. When illuminated, this field will separate the created charge carriers and a

    voltage of approx. 0.5 V is created at the outer contacts. The p-n-crossover ensures that

    the charge carriers created by the light do not join up again, but can be used as current.

    Silicon solar cells are differentiated from untreated, extremely clean semiconductor

    material by two main stages: doping and p-n-crossover.

    If small quantities of foreign atoms are introduced into the silicon: ("doping"),

    free moving charge carriers are created according to the type of atoms. Phosphorus atoms

    lead to free electrons (n-silicon), boron to free holes (p-silicon). Doping thereforeprovides free charge carriers in otherwise isolated silicon.

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    Fig 2: Principle of PV Cell

    1.3 ELECTRIC MODEL OF PHOTOVOLTAIC CELL

    Thus the simplest equivalent circuit of a solar cell is a current source in parallel with a

    diode. The output of the current source is directly proportional to the light falling on the cell

    (photocurrent Iph). During darkness, the solar cell is not an active device; it works as a

    diode, i.e. a p-n junction. It produces neither a current nor a voltage. However, if it is

    connected to an external supply (large voltage) it generates a current ID, called diode (D)

    current or dark current. The diode determines the I-V characteristics of the cell.

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    Fig 3: Electrical model of PV Cell

    Semiconductors, characterized as being perfect insulators at absolute zero,

    become increasingly conductive as temperature is increased. As temperature becomes

    greater, sufficient energy is transferred to a small fraction of electrons, causing them to

    move from the valence band to the conduction band and holes to move from the

    conduction band to the valence band. The increase in temperature responsible for this

    entire process is a direct result of external energy in the case of PV systems, it is incident

    photons due to illumination.

    Under the photoelectric effect, because photons incident upon a p-n diode can

    create electron-hole pairs at a cross material junction, an electric potential difference

    across this junction can be established. Under no illumination, electrons and holes are

    separated at n and p regions respectively due to the diode characteristic unidirectional

    current path. When illuminated, PV cells are impacted by incident photons which

    bombard cell electrons creating electron hole pairs. These electron hole pairs then

    separate in response to the electric field created by the cell junction, causing electrons to

    drift back into the n region, and holes into the p region. A bidirectional current path is

    created and energy can be harnessed.

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    Fig 4. Graphs

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    1.4 MANUFACTURING OF SOLAR CELLS

    Properties of silicon:

    Atomic number 14

    Atomic mass 28.0855 g.mol-1

    Electronegativity according to Pauling 1.8

    Density 2.33 g.cm-3

    at 20 C

    Melting point 1410 C

    Boiling point 3265 C

    Vanderwaals radius 0.132 nm

    Ionic radius 0.271 (-4) nm ; 0.041(+4)

    Isotopes 5

    There are two main reasons why silicon is used for manufacturing solar cells.One is

    that silicon is an elemental semiconductor with good stability and a well balanced set of

    electronic ,physical and chemical properties,the same set of strengths that have made

    silicon the preferred material for microelectronics. The molecular structure of single-

    crystal silicon is uniform. This uniformity is ideal for the transfer of electrons efficiently

    through the material. However, in order to make an effective photovoltaic cell, silicon

    needs to be "doped" with other elements.

    Raw Materials

    The basic component of a solar cell is pure silicon, which is not pure in its

    natural state.

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    Fig 5: Raw Materials

    To make solar cells, the raw materialssilicon dioxide of either quartzite

    gravel or crushed quartzare first placed into an electric arc furnace, where a carbon arcis applied to release the oxygen. The products are carbon dioxide and molten silicon. At

    this point, the silicon is still not pure enough to be used for solar cells and requires further

    purification.

    Pure silicon is derived from such silicon dioxides as quartzite gravel (the

    purest silica) or crushed quartz. The resulting pure silicon is then doped (treated with)

    with phosphorous and boron to produce an excess of electrons and a deficiency of

    electrons respectively to make a semiconductor capable of conducting electricity. The

    silicon disks are shiny and require an anti-reflective coating, usually titanium dioxide.

    The solar module consists of the silicon semiconductor surrounded by protective

    material in a metal frame. The protective material consists of an encapsulant of

    transparent silicon rubber or butyryl plastic (commonly used in automobile windshields)

    bonded around the cells, which are then embedded in ethylene vinyl acetate. A polyester

    film (such as Mylar or tedlar) makes up the backing. A glass cover is found on terrestrial

    arrays, a lightweight plastic cover on satellite arrays.

    Purifying the silicon

    The silicon dioxide of either quartzite gravel or crushed quartz is placed into an

    electric arc furnace. A carbon arc is then applied to release the oxygen. The

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    products are carbon dioxide and molten silicon. This simple process yields silicon

    with one percent impurity, useful in many industries but not the solar cell industry.

    The 99 percent pure silicon is purified even further using the floating zone

    technique. A rod of impure silicon is passed through a heated zone several times in

    the same direction. This procedure "drags" the impurities toward one end with

    each pass. At a specific point, the silicon is deemed pure, and the impure end is

    removed.

    Making single crystal silicon

    Solar cells are made from silicon boules, polycrystalline structures that have the

    atomic structure of a single crystal. The most commonly used process for creating

    the boule is called the Czochralski method. In this process, a seed crystal of silicon

    is dipped into melted polycrystalline silicon. As the seed crystal is withdrawn and

    rotated, a cylindrical ingot or "boule" of silicon is formed. The ingot withdrawn is

    unusually pure, because impurities tend to remain in the liquid.

    Making silicon wafers

    From the boule, silicon wafers are sliced one at a time using a circular saw whose

    inner diameter cuts into the rod, or many at once with a multiwire saw. (Adiamond saw produces cuts that are as wide as the wafer. 5 millimeter thick.)

    Only about one-half of the silicon is lost from the boule to the finished circular

    wafermore if the wafer is then cut to be rectangular or hexagonal. Rectangular

    or hexagonal wafers are sometimes used in solar cells because they can be fitted

    together perfectly, thereby utilizing all available space on the front surface of the

    solar cell.

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    After the initial purification, the silicon is further refined in a floating zone

    process. In this process, a silicon rod is passed through a heated zone several times,which serves to 'drag" the impurities toward one end of the rod. The impure end can

    then be removed.

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    Next, a silicon seed crystal is put into a Czochralski growth apparatus, where

    it is dipped into melted polycrystalline silicon. The seed crystal rotates as it is

    withdrawn, forming a cylindrical ingot of very pure silicon. Wafers are then sliced out

    of the ingot.

    The wafers are then polished to remove saw marks. (It has recently been found

    that rougher cells absorb light more effectively, therefore some manufacturers have

    chosen not to polish the wafer.)

    Doping

    The traditional way of doping (adding impurities to) silicon wafers with boron and

    phosphorous is to introduce a small amount of boron during the Czochralski process.

    Properties of Boron:

    Atomic number

    Atomic mass

    Density

    Melting point

    Boiling point

    Vanderwaals radius

    Ionic radius

    5

    10.81 g.mol-1

    2.3 g.cm-3

    at 20C

    2076 C

    3927 C

    0.098 nm

    0.027 nm

    Isotopes 2

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    The wafers are then sealed back to back and placed in a furnace to be heated to

    slightly below the melting point of silicon (2,570 degrees Fahrenheit or 1,410

    degrees Celsius) in the presence of phosphorous gas. The phosphorous atoms

    "burrow" into the silicon, which is more porous because it is close to becoming a

    liquid. The temperature and time given to the process is carefully controlled to

    ensure a uniform junction of proper depth. A more recent way of doping silicon

    with phosphorous is to use a small particle accelerator to shoot phosphorous ions

    into the ingot. By controlling the speed of the ions, it is possible to control their

    penetrating depth. This new process, however, has generally not been accepted by

    commercial manufacturers.

    Properties of Phosphorous:

    Atomic number 15

    Atomic mass 30,9738 g.mol-1

    Density 1,82 g/ml at 20C

    Melting point 44,2 C

    Boiling point 280 C

    Placing electrical contacts

    Electrical contacts connect each solar cell to another and to the receiver of

    produced current. The contacts must be very thin (at least in the front) so as not toblock sunlight to the cell. Metals such as palladium/silver, nickel, or copper are

    vacuum-evaporated.

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    Fig 6: Makeup of a typical solar cell

    This illustration shows the makeup of a typical solar cell. The cells are

    encapsulated in ethylene vinyl acetate and placed in a metal frame that has a Mylar

    back sheet and glass cover through a photo resist, silk screened, or merely

    deposited on the exposed portion of cells that have been partially covered with

    wax. All three methods involve a system in which the part of the cell on which a

    contact is not desired is protected, while the rest of the cell is exposed to the metal.

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    After the contacts are in place, thin strips ("fingers") are placed between

    cells. The most commonly used strips are tin-coated copper.

    The anti-reflective coating

    Because pure silicon is shiny, it can reflect up to 35 percent of the sunlight. To

    reduce the amount of sunlight lost, an anti-reflective coating is put on the silicon wafer.

    The most commonly used coatings are titanium dioxide and silicon oxide, though

    others are used. The material used for coating is either heated until its molecules boil off

    and travel to the silicon and condense, or the material undergoes sputtering. In this

    process, a high voltage knocks molecules off the material and deposits them onto the

    silicon at the opposite electrode.Yet another method is to allow the silicon itself to react

    with oxygen- or nitrogen-containing gases to form silicon dioxide or silicon nitride.

    Commercial solar cell manufacturers use silicon nitride.

    Encapsulating the cell

    The finished solar cells are then encapsulated; that is, sealed into silicon rubber or

    ethylene vinyl acetate. The encapsulated solar cells are then placed into an aluminum

    frame that has a Mylar or tedlar back sheet and a glass or plastic cover.

    Types of Solar cells

    Monocrystalline silicon(c-Si):often made using the Czochralski process. Single-

    crystal wafer cells tend to be expensive, and because they are cut from cylindrical

    ingots, do not completely cover a square solar cell module without a substantial

    waste of refined silicon. Hence most c-Si panels have uncovered gaps at the four

    corners of the cells.

    Poly- or multicrystalline silicon (poly-Si or mc-Si): made from cast square

    ingots large blocks of molten silicon carefully cooled and solidified. Poly-Si cells

    are less expensive to produce than single crystal silicon cells, but are less efficient.

    Ribbon silicon is a type of multicrystalline silicon: it is formed by drawing flat

    thin films from molten silicon and results in a multicrystalline structure. These

    cells have lower efficiencies than poly-Si, but save on production costs due to a

    great reduction in silicon waste, as this approach does not require sawing from

    ingots.

    http://en.wikipedia.org/wiki/Monocrystalline_siliconhttp://en.wikipedia.org/wiki/Czochralski_processhttp://en.wikipedia.org/wiki/Multicrystalline_siliconhttp://en.wikipedia.org/wiki/Ribbon_siliconhttp://en.wikipedia.org/wiki/Moltenhttp://en.wikipedia.org/wiki/Multicrystallinehttp://en.wikipedia.org/w/index.php?title=Silicon_waste&action=edit&redlink=1http://en.wikipedia.org/wiki/Sawhttp://en.wikipedia.org/wiki/Ingothttp://en.wikipedia.org/wiki/Ingothttp://en.wikipedia.org/wiki/Sawhttp://en.wikipedia.org/w/index.php?title=Silicon_waste&action=edit&redlink=1http://en.wikipedia.org/wiki/Multicrystallinehttp://en.wikipedia.org/wiki/Moltenhttp://en.wikipedia.org/wiki/Ribbon_siliconhttp://en.wikipedia.org/wiki/Multicrystalline_siliconhttp://en.wikipedia.org/wiki/Czochralski_processhttp://en.wikipedia.org/wiki/Monocrystalline_silicon
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    Fig 7: Types of solar cells

    1.5 PV CELL SPECIFICATIONS

    MULTICRYSTALLINE SOLAR CELL

    NEGATIVE POSITIVE

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    MECHANICAL SPECIFICATION

    Product Multicrystalline cell

    Format 156 mm 156 mm 0.5 mmDiameter:220 0.5 mm

    Average thickness (Si) 160 m 30 m / 180 m 30 m /200 m 30 m

    Front contacts () Three 1.5 mm wide bus bars(silver)Alkaline texturized surfaceDarkblue anti-reflecting coating (siliconnitride)

    Back contacts (+) Three 3 mm wide bus bars (silver /aluminum)Aluminum backsidemetallization

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    1.6 APPLICATIONS

    For low-power portable electronics, like calculators or small fans, a

    photovoltaic array may be a reasonable energy source rather than a battery.

    Although using photovoltaics lowers the cost (over time) of the device to the user-

    who will never need to buy batteries-the cost of manufacturing devices with

    photovoltaic arrays is generally higher than the cost of manufacturing devices to

    which batteries must be added. Therefore, the initial cost of photovoltaic devices is

    often higher than battery-operated devices.

    In other situations, such as solarbattery chargers, watches, and flashlights, the

    photovoltaic array is used to generate electricitythat is then stored in batteries foruse later.

    Fig 8: Application of PV Cell

    http://science.jrank.org/pages/2385/Electronics.htmlhttp://science.jrank.org/pages/5204/Photovoltaic-Cell-Applications.htmlhttp://science.jrank.org/pages/779/Battery.htmlhttp://science.jrank.org/pages/5204/Photovoltaic-Cell-Applications.htmlhttp://science.jrank.org/pages/5204/Photovoltaic-Cell-Applications.htmlhttp://science.jrank.org/pages/5204/Photovoltaic-Cell-Applications.htmlhttp://science.jrank.org/pages/5204/Photovoltaic-Cell-Applications.htmlhttp://science.jrank.org/pages/779/Battery.htmlhttp://science.jrank.org/pages/5204/Photovoltaic-Cell-Applications.htmlhttp://science.jrank.org/pages/2385/Electronics.html
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    1.7 MAKING OF SOLAR CELL MODULE

    FLOW CHART

    Solar Cell

    Manufacturing

    Solar cell

    Soldering

    machine.

    Komex 1

    Pick &Place

    Robot 1

    Panel layout

    EVA &Glass

    Semi

    Automatic

    Bus Bay

    soldering

    Manual Manual

    layout

    Lamination

    thermal &

    vacuum

    Panel

    TestingPick & Place

    Robo

    Panel layout

    EVA &GlassPick &PlaceRobot 2

    Solar cell

    Soldering

    machine.

    Komex 2

    Bus Bay

    soldering

    Lamination

    thermal &

    vacuum

    Bus Bay

    solderingLamination

    thermal &

    vacuum

    PANEL

    ASSEMBLY

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    PANEL

    ASSEMBLY

    Fork lift

    Manual

    Distributi

    on box

    fixing

    Soldering

    Pressing

    machine

    Panel cell

    side

    frame fix

    Gate outLoadingin trucksPacking

    MANUFACTURING PROCESS

    Solar Semiconductor employs equipment that can handle 160 micron cells, 2Busbar and 3 Busbar cells. The Tabber is used to interconnect cells in a

    string, uses vacuum suction cups to pick cells and an IR camera to check for

    any cell breakages.

    The advanced automation unit at Solar Semiconductor comes with Twin

    Robot System. These Robotic systems speed up the manufacturing processand enhance efficiency. It also helps in increasing productivity, minimizing

    errors and life cycle costs.

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    The encapsulation process involves vacuum pressing the array sandwich(glass EVA array EVA backsheet). The pressing melts the fast cure

    0.33mm EVA, which then acts as an adhesive and bonds the backsheet andthe glass sheet with the cell array to make it weather and dust proof.

    The laminate is trimmed and then taped with a double sided adhesive foamtape. The temperature is maintained at 140 degree centigrade for lamination.

    This trimmed laminate is then framed using an in-house developed

    automatic frame-fitter. This is followed by junction box fitting, which is

    done manually.

    The testing for electrical parameters is done by using the most advancedclass AAA - pulsed type Sun Simulators.

    The Reliability Testing Lab has been set up for in-house testing of prototypemodules and new materials. It enables self-certification of products and

    speeds up new process qualification and certification process.

    Quality control at Solar Semiconductor is done through checks on incomingraw material and on the manufacturing process. In order to enhance the

    effectiveness and ensure total quality control, various quality concepts likeQuality circles and Kaizen are being practiced.

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    2. SOLAR MOBILE CHARGER UNIT

    Portable Solar Mobile Charger for mobile phone can be charged with Sun

    light, and electrical power. It stores power from the sun and lets you charge mobilephone, iPod, etc at your convenience.

    PV cell converts light into electric current using the photo electric effect.

    In photo electric effect electrons emitted from the matter (metals and nonmetals,

    liquids and gases)as a consequence of their absorption of energy 4m

    electromagnetic radiation of very short wavelength such as ultraviolet or visible

    light.

    The photons of light beam have a characteristic energy determined by the

    (frequency of light).In the photon emission process if an electron with in some

    material absorbs the energy the energy of 1 photon and thus has more energy than

    the work function (the electron binding energy) of the material is ejected. If photon

    energy is low the electron is unable to escape 4m the material.

    Increasing the intensity of the light beam increases the number of photons

    in the light beam and thus increase the number of electrons emitted but doesnt

    increase the energy that each electron possesses.

    The energy of the emitted electron doesnt depend on the light intensity

    of the incoming light but only on the energy or frequency of the individual

    photons. It is an interaction between the incident photon and the outermost

    electron.

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    2.1 MATERIALS REQUIRED

    SOLAR CELLS

    12 pieces each generating 0.5 V.

    Fig 9: Solar cells

    ACRYLIC SHEET

    Cast acrylic sheet is a material with unique physical properties and performance

    characteristics. It weighs half as much as the finest optical glass yet is equal to it in clarity

    and is up to 17 times more impact resistant.

    Fig 10: Acrylic sheet

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    ETHYLENE VINYL ACETATE

    Ethylene vinyl acetate(also known as EVA) is the copolymerof ethyleneand vinyl

    acetate. The weight percent vinyl acetate usually varies from 10 to 40%, with theremainder being ethylene.

    It is a polymerthat approaches elastomericmaterials in softness and flexibility, yet

    can be processed like other thermoplastics. The material has good clarity and barrier

    properties, low-temperature toughness, stress-crack resistance, hot-melt adhesive water

    proof properties, and resistance to UV radiation. EVA has little or no odor and is

    competitive with rubberand vinylproducts in many electrical applications.

    Fig 11: EVA

    TEFLON:

    Polytetrafluoroethylene (PTFE) is a synthetic fluoropolymer of tetrafluoroethylenethat finds numerous applications. PTFE is most well-known by the DuPont brand name

    Teflon.

    PTFE is a fluorocarbon solid, as it is a high-molecular-weight compound consisting

    wholly of carbon and fluorine. PTFE is hydrophobic: neither water nor water-containing

    substances wet PTFE, as fluorocarbons demonstrate mitigated London dispersion forces

    http://en.wikipedia.org/wiki/Heteropolymerhttp://en.wikipedia.org/wiki/Ethylenehttp://en.wikipedia.org/wiki/Vinyl_acetatehttp://en.wikipedia.org/wiki/Vinyl_acetatehttp://en.wikipedia.org/wiki/Polymerhttp://en.wikipedia.org/wiki/Elastomerhttp://en.wikipedia.org/wiki/Thermoplastichttp://en.wikipedia.org/wiki/Toughnesshttp://en.wikipedia.org/wiki/Adhesivehttp://en.wikipedia.org/wiki/UV_radiationhttp://en.wikipedia.org/wiki/Rubberhttp://en.wikipedia.org/wiki/Vinylhttp://en.wikipedia.org/wiki/Vinylhttp://en.wikipedia.org/wiki/Rubberhttp://en.wikipedia.org/wiki/UV_radiationhttp://en.wikipedia.org/wiki/Adhesivehttp://en.wikipedia.org/wiki/Toughnesshttp://en.wikipedia.org/wiki/Thermoplastichttp://en.wikipedia.org/wiki/Elastomerhttp://en.wikipedia.org/wiki/Polymerhttp://en.wikipedia.org/wiki/Vinyl_acetatehttp://en.wikipedia.org/wiki/Vinyl_acetatehttp://en.wikipedia.org/wiki/Ethylenehttp://en.wikipedia.org/wiki/Heteropolymer
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    due to the high electronegativity of fluorine. PTFE has one of the lowest coefficients of

    friction against any solid.

    Fig 12: Teflon

    TABBING WIRE

    Tabbing wire is used by solar panel manufacturers to connect individual solar cells

    together in serial connections. It is copper wire coated with solder

    Typical characteristics of tabbing wire are

    GAUGE: 0.1MM

    WIDTH: 2.0 MM

    98-99% of the material weight is Copper Ribbon which serves as the base center of

    the tabbing wire. The tin coating is made from either lead based material 62 SN% (tin) /

    36 PB% (lead) / 2 AG% (silver) or 96.5% SN / 3.5% Ag (Silver) or other variations of

    lead free solder.

    Fig 13: Tabbing Wire

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    7805 REGULATOR

    It converts a varying DC input voltage into a constant 5 DC output voltage.

    Fig 15 : 7805 regulator

    MULTIPIN CABLE

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    2.2 SPECIFICATIONS OF CHARGER

    Uses high-efficiency monocrystalline silicon Solar panel: 5.5V/1000mA

    Output voltage: 5.5V

    Output current: 300-550 mA

    Time taken to charge mobile phone using the charger: about 60 for typical mobile

    Time to fully charge the built-in battery using computer or AC adapter: ~ 2 hours

    Time to fully charge the built-in battery with solar energy: ~ 8 hours

    2.3 DESIGN OF CHARGER

    A multicrystalline solar cell is taken and its cut into 12 parts.

    By taking tabbing wire and applying flux, paste soldering is done on the bus bars.

    Fig 16 : Initial Arrangement of Solar cells in Series

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    This is done from top of one cell to bottom of the other cell. They are connected in

    series. The above process is continued for remaining cells.

    A wire comes from positive side of cell and another wire comes from the negative

    side. The whole arrangement is then placed on top of an acrylic sheet, Teflon, EVA.

    On top these panels EVA is again placed and are attached with a feviquick.

    Fig 17: Cells in Series

    Thee wires are connected to the terminals of a regulator. Using multimeter we verify the voltage is brought down to 5 V.

    Regular terminals are further connected to multipin cable.

    The pin is then connected to mobile to charge it.

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    Fig 18 :Final Work

    2.4 EXPERIMENTAL WORK

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    Using Sun light:

    LIGHTAND

    HEAT

    HEAT/TEMP

    NUMBER

    OF

    CELLS

    AREAOF

    CELL

    SERIES/

    PARELLEL

    CONNECTIO

    N

    VOLTAGE CURRENTS.NO LIGHT

    INTENSITY POWER

    SOURCE

    1 SUNLIGHT

    NOON OPENSPACE

    1

    2

    3

    4

    5

    6

    7

    8

    9

    10

    11

    SERIES0.55

    1.10

    1.65

    2.20

    2.78

    3.34

    3.87

    4.42

    4.94

    5.14

    6.06

    1 0.55

    1.10

    1.65

    2.20

    2.78

    3.34

    3.87

    4.42

    4.94

    5.14

    6.06

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    Using 60 watts bulb:

    S.NO LIGHT

    AND

    HEAT

    SOURCE

    LIGHT

    INTENSITY

    HEAT/

    TEMP

    AREA

    OF

    CELL

    SERIES/NUMBE

    R

    OF

    CELLS

    CURRENTPARELLEL

    VOLTAG

    E

    POWER

    ()CONNECTION

    260

    WATTSBULB

    ROOMTEMPERATURE

    ROOMTEMP

    1

    2

    3

    4

    5

    6

    7

    8

    9

    10

    11

    1 0.42

    0.94

    1.40

    1.85

    2.20

    2.71

    3.24

    3.53

    3.84

    SERIES 0.42

    0.94

    1.40

    1.85

    2.20

    2.71

    3.24

    3.53

    3.84

    4.26 4.26

    4.50 4.50

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    Using 100 watts bulb:

    S.NO LIGHT

    AND

    HEAT

    SOURCE

    LIGHT

    INTENSITYHEAT/

    TEMPNUMBE

    R

    OF

    CELLS

    AREA

    OF

    CELL

    SERIES/

    PARELLEL VOLTAG

    E

    CURREN

    TPOWER

    CONNECTIO

    N ()

    3 100WATTSBULB

    INSIDEROOM

    ROOMTEMP

    1

    2

    3

    4

    5

    6

    7

    8

    9

    10

    11

    SERIES 0.48

    0.98

    1.40

    1.88

    2.35

    2.91

    3.36

    3.75

    4.30

    1 0.48

    0.98

    1.40

    1.88

    2.35

    2.91

    3.36

    3.75

    4.30

    4.814.81

    5.38 5.38

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    Fig 19:Charging Nokia mobile using solar cells

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    Fig 20:Charging Samsung mobile using solar cells

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    3. MOBILE BATTERY

    A lithium-ion battery(Li-ion batteryor LIB) is a family of rechargeable battery

    types in which lithiumions move from the negative electrodeto the positive electrode

    during discharge, and back when charging. Chemistry, performance, cost, and safety

    characteristics vary across LIB types. Unlike lithium primary batteries (which are

    disposable), lithium-ion electrochemical cells use an intercalated lithium compound as

    the electrode material instead of metallic lithium.

    Fig 21: Nokia Li-ion battery for powering a mobile phone

    3.1 ELECTRICAL MODEL FOR LI-ION BATTERY

    Safety circuits inside a Li-Ion battery pack:

    Inside a Li-Ion pack there is always a safety circuit that consists of four main sections:

    The controller IC that monitors each cell (or parallel cells) voltage and preventsthe cells to overcharge or over discharge controlling accordingly the cutoff

    switches. Also the voltage across the switches is monitors in order to prevent over

    current.

    The control switches that usually comprises FET structures that cutoff the chargeor discharge depending on the control signals of the controller IC.

    http://en.wikipedia.org/wiki/Rechargeable_batteryhttp://en.wikipedia.org/wiki/Lithiumhttp://en.wikipedia.org/wiki/Electrodehttp://en.wikipedia.org/wiki/Primary_batteryhttp://en.wikipedia.org/wiki/Electrochemical_cellhttp://en.wikipedia.org/wiki/Intercalation_%28chemistry%29http://en.wikipedia.org/wiki/Intercalation_%28chemistry%29http://en.wikipedia.org/wiki/Electrochemical_cellhttp://en.wikipedia.org/wiki/Primary_batteryhttp://en.wikipedia.org/wiki/Electrodehttp://en.wikipedia.org/wiki/Lithiumhttp://en.wikipedia.org/wiki/Rechargeable_battery
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    The temperature fuse that cutoff the current if the control switches experienceabnormal heating. This fuse is not recoverable.

    The thermistor (usually PTC) that measure the battery temperature inside the pack.It's terminals are connected to the charger so it can sense the temperature of the

    pack and control the charge current until the battery it's full charged.

    3.2 SPECIFICATIONS OF BATTERY

    Type : RH-105

    Make : Nokia Make: Samsung

    Model : 1208 Model: GT-B5310

    Voltage : Max-5V Voltage : Max-5V

    Min-3.7V Min-3.7V

    Capacity: 1020mahr Capacity: 960maph

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    3.3 STRUCTURE

    Li-Ion cell has a tree layer structure. A positive electrode plate (made with LithiumCobalt oxide - cathode), a negative electrode plate (made with specialty carbon - anode)

    and a separator layer.

    Inside the battery also exists a electrolyte which is a lithium salt in an organic

    solvent. I-Ion is also equipped with a variety of safety measures and protective

    electronics and/or fuses to prevent reverse polarity, over voltage and over heating and

    also have a pressure release valve and a safety vent to prevent battery from burst.

    Fig 22: Structure

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    3.4 WORKING PRINCIPLE

    Lithium battery uses lithium cobalt oxide as positive electrode - cathode - and a

    high crystallized special carbon as negative electrode - anode. Also an organic solvent

    specialized to be used with the specific carbon works like electrolytic fluid.

    The chemical reaction that takes place inside the battery is as follows, during charge

    and discharge operation:

    The main principle behind the chemical reaction is one where lithium in

    positive electrode material is ionized during charge and moves from layer to layer in the

    negative electrode.

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    3.5 FEATURES OF LITHIUM ION BATTERIES

    High energy density that reaches 400 Wh/L (volumetric energy density) or

    160Wh/Kg (mass energy density)

    High voltage. Nominal voltage of 3,6V or even 3,7V on newer Li-Ion batteries.

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    No memory effect. Can be charged any time, but they are not as durable as NiMH

    and NiCd batteries.

    High charge currents (0,5-1A) that lead to small charging times (around 2-4

    hours).

    Flat discharge voltage allowing the device to stable power throughout the

    discharge period.

    Typical charging Voltage 4,2 0,05V.

    Charging method: constant current - constant voltage (CV-CC).

    Typical operation voltage 2,8V to 4,2V

    Recommended temperature range 0-40

    3.6 CHARGING CHARECTERISTICS

    Charging method is constant current - constant voltage (CV-CC). This means

    charging with constant current until the 4.2V are reached by the cell (or 4,2V x the

    number of cells connected in series) and continuing with constant voltage until the

    current drops to zero.

    The charge time depends on the charge level of the battery and varies from 2-4

    hours for full charge. Also Li-Ion cannot fast charge as this will increase their

    temperature above limits. Charging time increases at lower temperatures.

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    3.7 WORKING PROCESS

    A battery charger is basically a DC power supply source. Here a transformer isused to step down the AC mains input voltage to the required level as per the

    rating of the transformer.

    This transformer is always a high power type and is able to produce a high current

    output as required by most lead-acid batteries.

    A bridge rectifier configuration is used to rectify the low voltage AC into DC and

    is further smoothed by a high value electrolytic capacitor.

    This DC is fed to an electronic circuit which regulates the voltage into a constant

    level and is applied to the battery under charge, where the energy is stored through

    an internal process of chemical reaction.

    In automatic battery chargers a voltage sensor circuit is incorporated to sense the

    voltage of the battery under charge. The charger is automatically switched OFF

    when the battery voltage reaches the required optimum level.

    Calculation of Charging or discharging time of a Battery

    The rated current capacity of a chargeable battery may vary according to its

    applications. Its current holding capacity is expressed in ampere-hour (AH). This

    unit of measurement may be defined as the maximum current through which the

    particular battery can be fully charged or discharged in one hour.

    If for example a 4 AH fully charged battery is discharged at 4 ampere rate, then

    ideally it should take an hour for it to get fully discharged (but practically it can be

    seen that the back up time is much less than an hour due to the existing

    inefficiency in all batteries).

    Similarly if the same battery is charged at 4 ampere rate, then it should take an

    hour to get it fully charged. But its never a good practice to charge or discharge

    batteries at their full current ratings.

    http://www.brighthub.com/engineering/electrical/articles/61881.aspxhttp://www.brighthub.com/engineering/electrical/articles/61881.aspx
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    Ideally the charging and the discharging process should be carried out gradually

    for about 10 hours. So to find out the optimum charging current of a battery, just

    divide its AH by 10, the same is true to find its correct continuous discharge rate.

    3.8 ADVANTAGE

    One great advantage of Li-Ion batteries is their low self-discharge rate of only

    approximately 5% per month, compared with over 30% per month and 20% per month in

    nickel metal hydride batteries and nickel cadmium batteries respectively.

    Comparison table of the most common batteries types

    Chemistry Type Ni-Cd Ni-MH Leadacid

    Li-ionCylindrical

    Li-ionPrismatic

    Li-Po

    Nominal Voltage (V) 1.2 1.2 2,1 3.6 3.6 / 3.7 3.6

    Specific Energy (Wh/Kg) 50 70 30 80 100-160 140

    Specific Energy (Wh/L) 150 200 - - 250-360 -

    Cycle Life (Times) 500 560 - 1000 1000 -

    Environmental hazard low medium medium high high high

    Safety High High medium low low low

    Cost low medium low high high high

    Self-Discharge Rate

    (%/month)

    25-30 30-35 - 6-9 6-9 -

    Memory Effect yes yes yes no no no

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    CONCLUSION

    In solar mobile charger ripples will not be there as we use DC power

    directly to charge the mobile.

    Battery life is more as high voltages are not developed.

    Versatility of Solar mobile charger is high.

    Life of the battery will be high as we use solar mobile charger.

    Adaptability is high.

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    REFERENCES

    Solar semiconductor Industry visit

    http://en.wikipedia.org/wiki/Solar_cell

    encyclobeamia.solarbotics.net/article...

    www.solarbuzz.com/going-solar

    www.solarserver.com/knowledge

    http://www.solarbuzz.com/going-solahttp://www.solarbuzz.com/going-solahttp://www.solarbuzz.com/going-sola