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Introduction
 Earlier Solar cells were used in spacecrafts.
 In 1973,interest increased in renewable energy post
oil crisis because of war between Arab and Israel.
 Production of solar cell started for terrestrial
use.
 A standard technology is used for manufacturing of
solar cells.
Steps for making solar cells
1. Sand to metallurgical grade silicon.
2. Metallurgical grade to semiconductor grade .
3. Semiconductor grade to Si wafer.
4.Conversion of Si wafer to solar cell.
5. Solar cell to solar module.
6.Solar module installation.
Why Si for making solar
cell?
 Silicon is 2nd most
abundant element in the
earth crust (about 28% by
mass ) after oxygen.
 Stable: in terms of
temperature.
 Available in the form of
sand(SiO2).
Sand to metallurgical grade Si
 Si in the form of crystal(quartzite) is used.
 It is then reduced in an arc furnace with some
reducing agent like coal ,wooden chips and
coke at a high temperature of about .
 Molten Si thus obtained is called
metallurgical grade Si.
Arc furnace with chemical
reactions involved
 Si is periodically poured from the furnace and
blown with oxygen to further purify it
 It is then poured into shallow troughs , where
it solidifies and is subsequently broken into
chunks.
 MGS of the order of 1 million metric tons is
produced globally each year.
Impurity concentration in
MGS
Element Concentration(ppm) Element Concentration(ppm)
Aluminum 1000 – 4350 Manganese 50 -120
Boron 40 – 60 Molybdenum < 20
Calcium 245 – 500 Nickel 10 -105
Chromium 50 – 200 Phosphorus 20 -50
Copper 15 – 45 Titanium 140 – 300
Iron 1550 – 6500 Vanadium 50 – 250
Magnesium 10 – 50 Zirconium 20
Characteristics of MG-Si
 MG-Si obtained is 98-99% pure with major
impurities being aluminum and iron.
 Energy and raw material intensive(production
of one metric ton (1,000 kg) of MGS requires
2500 - 2700 kg quartzite, 600 kg charcoal, 600
- 700 kg coal or coke, 300 - 500 kg wood chips,
and 500,000 kWh of electric power ).
Characteristics of MG-Si contd…
 Most of the production ( 70% approx) is used for
metallurgical applications (e.g., aluminum-
silicon alloys are commonly used for automotive
engine blocks)
 Applications in a variety of chemical products
such as silicone resins account for about 30% or
less.
 Only 1% or less used for the manufacturing of
high purity Semiconductor grade Si.
Metallurgical grade Si to
Semiconductor grade Si
Semiconductor grade silicon(EGS)
 EGS is one of the purest materials
commonly available.
 The formation of EGS from MGS is
accomplished through chemical purification
processes.
 The standard process to purify it is known
Siemens process.
Siemens Process
The basic concept involves the
conversion of MGS to a volatile silicon
compound, which is purified by distillation,
and subsequently decomposed to re-form
elemental silicon of higher purity (i.e., EGS).
Steps involved in Siemens process
 Physical pulverization of MGS.
The MG-Si is converted to a volatile
compound (Trichlorosilane) that is
condensed and refined by fractional
distillation.
The reasons for the predominant use of
SiHCl3 in the synthesis of EGS
 SiHCl3 can be easily formed by the reaction of
anhydrous hydrogen chloride with MGS at
reasonably low temperatures (200 - 400 °C).
 It is liquid at room temperature so that
purification can be accomplished using
standard distillation techniques.
 It is easily handled and if dry can be stored in
carbon steel tanks;
 Its liquid is easily vaporized and, when mixed
with hydrogen it can be transported in steel
lines without corrosion.
 It can be reduced at atmospheric pressure in
the presence of hydrogen.
 Its deposition can take place on heated
silicon, thus eliminating contact with any
foreign surfaces that may contaminate the
resulting silicon.
 It reacts at lower temperatures (1000 - 1200
°C) and at faster rates than does SiCl4.
Chlorosilane(siemens)process
 Trichlorosilane, is synthesized by heating
powdered MGS with anhydrous hydrogen
chloride (HCl) in the presence of Cu catalyst
at around 300 °C in a fluidized-bed reactor.
 SiHCl3 is reduced by
hydrogen when
mixture of the gases
are heated. Si is
deposited in a fine
grained
polycrystalline form
onto an electrically
heated Si rod.
SiHCl3 + H2→ Si + 3HCl
Schematic representation of the reaction pathways for the
formation of EGS using the chlorosilane(siemens) process.
Characteristics of EGS
 Requires a lot of energy.
 Low yield ~37% .
 Expensive
 Purity of about 99.9999% obtained.
Impurity concentration in EGS
Element Concentration
(ppb)
Element Concentration
(ppb)
Arsenic < 0.001 Gold < 0.00001
Antimony < 0.001 Iron 0.1-1.0
Boron ≤ 0.1 Nickel 0.1-0.5
Carbon 100 -1000 Oxygen 100-400
Chromium < 0.01 Phosphorus ≤ 0.3
Cobalt 0.001 Silver < 0.001
Copper 0.1 Zinc < 0.1
Figure showing different methods for Si production and purification
Silicon type Metallurgical
grade
Solar grade Electronic
grade
Designation MG SG EG
Purity 98% 99.9999%
(with 6 nines)
99.9999999%
(with 9 nines)
Performance
(in solar cells)
inadequate optimal Marginally better
than solar grade
Approximate
$/kg
$4 $15-50 $50
Availability >1MMtons/year No dedicated
producers
~150 Ktons/year
Three Silicon grades and their relative
costs/availability
Semiconductor grade to Si
wafer
EGS to ingot
 To convert EGS to ingot , we need to grow a
single crystal.
 Two techniques are used to grow single
crystal :
1. Czochralski (CZ) method
2. Float zone method
Czochralski Technique
Czochralski-Si grower, called puller
consists of three main components :
1.A furnace, which includes a fused-silica
crucible, a graphite suscepter, a rotation
mechanism (clock wise) , a heating element,
and a power supply.
2. A crystal-pulling mechanism, which includes
a seed holder and a rotation mechanism
(counter-Clockwise).
CzochralskiTechnique
3. An ambient control,
which includes a gas
source (such as
argon), a flow control
and an exhaust
system
CzochralaskiTechnique
 High-purity, semiconductor-grade silicon (only a few
parts per million of impurities) is melted in a crucible,
usually made of quartz.
 Dopant impurity atoms such as boron or phosphorus
can be added to the molten silicon in precise amounts
to dope the silicon, thus changing it into p-type or n-
type silicon. This influences the electronic properties of
Czochralski Technique contd…
 A precisely oriented rod-mounted seed crystal is
dipped into the molten silicon.
 The seed crystal's rod is slowly pulled upwards and
rotated simultaneously.
 By precisely controlling the temperature
gradients, rate of pulling and speed of rotation, it
is possible to extract a large, single-crystal,
cylindrical ingot from the melt.
CZtechnique
1.Melting of poly-
Silicon, doping.
2.Introduction of
Seed crystal.
3.Beginning of
crystal growth.
4.Formed crystal
With residue of
melted silicon.
Why Czochralski Technique ??
TheVast Majority OfThe Commercially
grown Silicon uses CzochralskiTechnique
due to :
1.The Better Resistance Of The
WafersToThermal Stress
2.The Speed Of Production
3.The Low Cost
Disadvantages of CZ technique :
 A large amount of oxygen in the silicon wafer.
It reduces the minority carrier lifetime in the solar
cell, thus reducing the voltage current and efficiency.
 In addition, the oxygen and complexes of the
oxygen with other elements may become active at
higher temperatures, making the wafers sensitive to
high temperature processing.
FLOATING ZONE TECHNIQUE
Produced by cylindrical polysilicon rod that already has a
seed crystal in its lower end.
An encircling inductive heating coil melts the silicon
material.
 The coil heater starts from the bottom and is raised
pulling up the molten zone
FLOATINGZONETECHNIQUE
 A solidified single crystal
ingot forms below.
 Impurities prefer to remain
in the molten silicon so very
few defects and impurities
remain in the forming
crystal
SINGLECRYSTALGROWTHTECHNIQUES
Czochralski Growth
(CZ)
 Most single crystal
silicon made this
way.
 Lower quality silicon
than FZ with Carbon
and Oxygen present.
 Cheaper production
than FZ.
 Produces cylinders
and circular wafers
Float Zone (FZ)
 Better Quality than
CZ.
 More Expensive than
CZ.
 Produces cylinders
and circular wafers
Ingots (poly and monocrystalline)
Doping Si ingot
 To achieve a crystal of desired resistivity,
known amount of dopants is added to the
melt.
For silicon, boron and phosphorous are the
most common dopants for p- and n- type
materials
For gallium arsenide, cadmium and zinc are
commonly used for p-type material, while
selenium , silicon, and tellurium are used for
n-type material
Doping during FZ process
Slicing into wafers
 Ingots are cut into thin
wafers for solar
cells(100μm to
300μm).
 Two techniques :
 Wire sawing
 Diamond blade sawing
Cutting of ingot into columns by
wire saw
Characteristics
 By present wafering technology its difficult to
cut wafers from large crystals as they are
thinner than 300μm and had to retain a
reasonable yield.
More than half the silicon is wasted as
kerfs or cutting loss in the process.
Time consuming.
Water cooled and dirty.
Si wafer to solar cell
Texturing
Diffusion
Edge isolation
(Removal of n-
material from edges)
Anti Reflection
Coating
Front Ag printing (Ag
printing for collection
of generated carriers)
Back pad printing (Ag-
Al pad on the back side
for soldering)
Back Al printing (Al
screen printing to
provide contact)
Solar cell
Texturing surface
 To minimize reflection from the flat surface
solar cell wafers are textured by creating a
roughened surface(pyramids).
 By doing this, incident light will have a larger
probability of being absorbed into the solar
cell.
 Performed by etching in a weak alkaline
solution such as HF.
Diffusion process
 In diffusion process, impurities are introduced
in a controlled manner so as to obtain pn
junction in a p-type or n-type wafer.
 To make solar cell, n-type impurities must be
introduced in p-type wafer to give a p-n
junction ,phosphorus is the impurity generally
used .
Phosphorus diffusion process
 A carrier gas is bubbled through POCL3mixed
with a small amount of oxygen.
 It is then passed down a heated furnace in
which the wafers are stacked.
 An oxide layer containing phosphorous
grows on the surface.
 At high temperatures(800—1100°C ) ,
phosphorous diffuses into Si from the oxide.
Phosphorus diffusion process
Phosphorus diffusion process
After about 20 mins , the P impurities override
the B impurities in the surface to give a thin ,
heavily doped n-type region as shown in the
figure..
Vacuum evaporation
Metal contact are then attached to both the n-
type and the p-type region ,the metal to be
deposited is heated in a vacuum to a high
enough temp to cause it to melt and vaporize, it
will then condense on any cooler parts of the
vacuum system in direct line of sight, including
the solar cells, the back contact is normally
deposited over the entire back surface, while
the top contact is required in the form of a grid.
Techniques for defining top
grid
1. Use a metal shadow mask
2. The metal can be deposited over the
entire front surface of the cell and
subsequently etched a way from
unwanted region using a
photographic technique known
photolithography
The contact made up three
separate layer
1. Thin layer of silver and aluminium is used
as the bottom layer.
2. Layer of silver in the top with silver finger
printing.
3. The aluminium finger printing on bottom
side is done.
Characteristics
Yield of about 90% from starting wafers to
completed terrestrial cells can be
obtained.
This make the processing very labor-
intensive.
The vacuum evaporation equipment is
expensive compared to its throughput.
the material expensive such Ag.
Solar cells to solar module
Cell Sorting
Tabbing
Stringing
Module Lay up
Lamination &Trimming
Framing
Sealing &Cleaning
Cell Sorting
 According to measured parameters of current and
voltage by cell sorter.
 At standard irradiation of 1000W/m^2 by pulsed xenon
lamp and standard temperature of 25°C.
 Cell sorter measures and displays the following cell
parameters:
 Complete I-V curve, Open circuit voltage ,
 Short-circuit current , Short-circuit current density
 Peak power, Cell efficiency (η),Fill factor (FF), Series
resistance, Shunt resistance.
 Max. power output.
To maximize efficiency of solar module by minimizing
mismatch between connected cells.
Tabbing
 Tabbing refers to connecting flat tab leads to bus bar of solar
cells.
 Flat tab leads:
 Contains 90% silver and 10% impurities.
 Now a days tinned copper ribbons are used.
 High conductivity.
 Two tabs per cell are employed.
 Tabs provide accommodation for thermal expansion
Stringing
 Stringing is process of series connection of similar rating
tabbed solar cells.
 Cells in series = output voltage of a module / voltage of a
cell.
 Several cell strings can be internally paralleled according
to power requirement from module.
 Module power = voltage × current.
 Each cell string is now inspected for continuity of
connections before lay up process
Module lay up
The laminating materials are laid up in a sequence as
shown:
 3 to 4 mm thick low iron tempered glass is used.
 Ethyl vinyl acetate is a thermoplastic i.e. it’s shape changes
under heating are reversible.
 Back layer is a composite plastic sheet (Tedlar-polyster-
tedlar) provides insulation to humidity and high- electrical
voltage.
Lamination and trimming
 Layout is sealed by heating (140°C-150°C) in a
lamination unit.
 Laminator creates a pneumatic vacuum inside the
module to remove air bubbles and other gases.
 EVA flows and soaks the cell.
 Excess polymer sheets are trimmed off from the edges.
Framing
 Anodized aluminum frame is used.
 To make handling easier.
 To improve resistance to structural stress and weather
conditions.
 Frame must be electrically insulated from active cell circuit to
sustain high electrical voltage between terminals and frame.
 Junction box is attached to back side of frame and connected to
laminated solar cell string.
Sealing and cleaning
 Sealing is done by using RoomTemperatureVulcanizing(RTV) silicone.
 Features of RTV silicone rubber:
 Light viscosity and good flow ability.
 Low shrinkage Favorable tension .
 No deformation.
 Favorable hardness.
 High temperature resistance, acid and alkali-resistance and ageing
resistance
 The modules are cleaned using mild chemical solution.
Solar module to solar array
Electrical
characteristics at
STC
Interconnections of
modules
Mismatch in modules
connected in series
Mismatch in modules
connected in parallel
Role of bypass diode
and blocking diode.
Electrical characteristics atSTC
Standard Test Conditions
 Global radiation = 1000
W/m^2
 Ambient temperature
= 25°C
 Spectral
distribution=AM1.5
 Wind speed = 1 m/s
Electrical characteristics
 Short circuit current
(Isc)
 Open circuit current
(Voc)
 Maximum power
output (Pmax)
 Fill-factor (FF)
 Normal Operating Cell
Temperature (NOCT)
Interconnectionsof modules
 Solar modules are connected in series or parallel
depending upon the voltage and current requirement
at the output.
 Modules in series = (Total battery bank voltage)/ 12
V
 Modules in parallel = (Array peak amp.) / (Peak
amp. Per
modules)
where, Array peak amp. = (Average Ah per day to be
supplied by the array) / (peak
sunshine hour per day)
 When two or more modules with different
electrical properties are connected, the
output power is determined by the modules
with the lowest output power.
 Interconnections have suitable bypass and
blocking diode.
 Mostly mismatch occur due to difference in
either Isc orVoc.
Mismatchin moduleconnectedin
series
In series connections, mismatch due toVoc
and Isc occurs.
Mismatch inVoc of modules connected in
series :
No mismatch in current rating, same
current will be flow in the all modules.
Total output voltage is summation of
voltage rating of individual module.
I-Vcharacteristicoftheresultantmodule
ofdifferentVoc
Mismatchin Iscofmodules
connectedinseries
 Current in array is due to module with the least current
and further this modules act as a load.
 Power gets dissipated in the poor module and this leads
to:
 Irreversible damage.
 Hot spot formation
Mismatchin modulesconnectedin
parallel
 Mismatch in parallel connections is not as severe in
series.
 The voltage across the module combination is
always the same.
 The current from the combinations of modules is
the sum of the currents in the individual modules
Roleofbypassdiode and blockingdiode
 The bypass diode is connected in parallel but with
opposite polarity.
 Normally, for a 36-cell modules, two bypass diode
are used.
 It blocks the current from flowing in to the shaded
modules from the parallel module.
 It also prevents the flow of current from the battery
to the module during in night or rainy season.
Uses of blocking and bypass diode
Standard silicon solar cell

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Standard silicon solar cell

  • 1.
  • 2. Introduction  Earlier Solar cells were used in spacecrafts.  In 1973,interest increased in renewable energy post oil crisis because of war between Arab and Israel.  Production of solar cell started for terrestrial use.  A standard technology is used for manufacturing of solar cells.
  • 3. Steps for making solar cells 1. Sand to metallurgical grade silicon. 2. Metallurgical grade to semiconductor grade . 3. Semiconductor grade to Si wafer. 4.Conversion of Si wafer to solar cell. 5. Solar cell to solar module. 6.Solar module installation.
  • 4. Why Si for making solar cell?  Silicon is 2nd most abundant element in the earth crust (about 28% by mass ) after oxygen.  Stable: in terms of temperature.  Available in the form of sand(SiO2).
  • 5. Sand to metallurgical grade Si  Si in the form of crystal(quartzite) is used.  It is then reduced in an arc furnace with some reducing agent like coal ,wooden chips and coke at a high temperature of about .  Molten Si thus obtained is called metallurgical grade Si.
  • 6. Arc furnace with chemical reactions involved
  • 7.  Si is periodically poured from the furnace and blown with oxygen to further purify it  It is then poured into shallow troughs , where it solidifies and is subsequently broken into chunks.  MGS of the order of 1 million metric tons is produced globally each year.
  • 8. Impurity concentration in MGS Element Concentration(ppm) Element Concentration(ppm) Aluminum 1000 – 4350 Manganese 50 -120 Boron 40 – 60 Molybdenum < 20 Calcium 245 – 500 Nickel 10 -105 Chromium 50 – 200 Phosphorus 20 -50 Copper 15 – 45 Titanium 140 – 300 Iron 1550 – 6500 Vanadium 50 – 250 Magnesium 10 – 50 Zirconium 20
  • 9. Characteristics of MG-Si  MG-Si obtained is 98-99% pure with major impurities being aluminum and iron.  Energy and raw material intensive(production of one metric ton (1,000 kg) of MGS requires 2500 - 2700 kg quartzite, 600 kg charcoal, 600 - 700 kg coal or coke, 300 - 500 kg wood chips, and 500,000 kWh of electric power ).
  • 10. Characteristics of MG-Si contd…  Most of the production ( 70% approx) is used for metallurgical applications (e.g., aluminum- silicon alloys are commonly used for automotive engine blocks)  Applications in a variety of chemical products such as silicone resins account for about 30% or less.  Only 1% or less used for the manufacturing of high purity Semiconductor grade Si.
  • 11. Metallurgical grade Si to Semiconductor grade Si
  • 12. Semiconductor grade silicon(EGS)  EGS is one of the purest materials commonly available.  The formation of EGS from MGS is accomplished through chemical purification processes.  The standard process to purify it is known Siemens process.
  • 13. Siemens Process The basic concept involves the conversion of MGS to a volatile silicon compound, which is purified by distillation, and subsequently decomposed to re-form elemental silicon of higher purity (i.e., EGS).
  • 14. Steps involved in Siemens process  Physical pulverization of MGS. The MG-Si is converted to a volatile compound (Trichlorosilane) that is condensed and refined by fractional distillation.
  • 15. The reasons for the predominant use of SiHCl3 in the synthesis of EGS  SiHCl3 can be easily formed by the reaction of anhydrous hydrogen chloride with MGS at reasonably low temperatures (200 - 400 °C).  It is liquid at room temperature so that purification can be accomplished using standard distillation techniques.  It is easily handled and if dry can be stored in carbon steel tanks;
  • 16.  Its liquid is easily vaporized and, when mixed with hydrogen it can be transported in steel lines without corrosion.  It can be reduced at atmospheric pressure in the presence of hydrogen.  Its deposition can take place on heated silicon, thus eliminating contact with any foreign surfaces that may contaminate the resulting silicon.  It reacts at lower temperatures (1000 - 1200 °C) and at faster rates than does SiCl4.
  • 17. Chlorosilane(siemens)process  Trichlorosilane, is synthesized by heating powdered MGS with anhydrous hydrogen chloride (HCl) in the presence of Cu catalyst at around 300 °C in a fluidized-bed reactor.
  • 18.  SiHCl3 is reduced by hydrogen when mixture of the gases are heated. Si is deposited in a fine grained polycrystalline form onto an electrically heated Si rod. SiHCl3 + H2→ Si + 3HCl
  • 19. Schematic representation of the reaction pathways for the formation of EGS using the chlorosilane(siemens) process.
  • 20. Characteristics of EGS  Requires a lot of energy.  Low yield ~37% .  Expensive  Purity of about 99.9999% obtained.
  • 21. Impurity concentration in EGS Element Concentration (ppb) Element Concentration (ppb) Arsenic < 0.001 Gold < 0.00001 Antimony < 0.001 Iron 0.1-1.0 Boron ≤ 0.1 Nickel 0.1-0.5 Carbon 100 -1000 Oxygen 100-400 Chromium < 0.01 Phosphorus ≤ 0.3 Cobalt 0.001 Silver < 0.001 Copper 0.1 Zinc < 0.1
  • 22. Figure showing different methods for Si production and purification
  • 23. Silicon type Metallurgical grade Solar grade Electronic grade Designation MG SG EG Purity 98% 99.9999% (with 6 nines) 99.9999999% (with 9 nines) Performance (in solar cells) inadequate optimal Marginally better than solar grade Approximate $/kg $4 $15-50 $50 Availability >1MMtons/year No dedicated producers ~150 Ktons/year Three Silicon grades and their relative costs/availability
  • 25. EGS to ingot  To convert EGS to ingot , we need to grow a single crystal.  Two techniques are used to grow single crystal : 1. Czochralski (CZ) method 2. Float zone method
  • 26. Czochralski Technique Czochralski-Si grower, called puller consists of three main components : 1.A furnace, which includes a fused-silica crucible, a graphite suscepter, a rotation mechanism (clock wise) , a heating element, and a power supply. 2. A crystal-pulling mechanism, which includes a seed holder and a rotation mechanism (counter-Clockwise).
  • 27. CzochralskiTechnique 3. An ambient control, which includes a gas source (such as argon), a flow control and an exhaust system
  • 28. CzochralaskiTechnique  High-purity, semiconductor-grade silicon (only a few parts per million of impurities) is melted in a crucible, usually made of quartz.  Dopant impurity atoms such as boron or phosphorus can be added to the molten silicon in precise amounts to dope the silicon, thus changing it into p-type or n- type silicon. This influences the electronic properties of
  • 29. Czochralski Technique contd…  A precisely oriented rod-mounted seed crystal is dipped into the molten silicon.  The seed crystal's rod is slowly pulled upwards and rotated simultaneously.  By precisely controlling the temperature gradients, rate of pulling and speed of rotation, it is possible to extract a large, single-crystal, cylindrical ingot from the melt.
  • 30. CZtechnique 1.Melting of poly- Silicon, doping. 2.Introduction of Seed crystal. 3.Beginning of crystal growth. 4.Formed crystal With residue of melted silicon.
  • 31. Why Czochralski Technique ?? TheVast Majority OfThe Commercially grown Silicon uses CzochralskiTechnique due to : 1.The Better Resistance Of The WafersToThermal Stress 2.The Speed Of Production 3.The Low Cost
  • 32. Disadvantages of CZ technique :  A large amount of oxygen in the silicon wafer. It reduces the minority carrier lifetime in the solar cell, thus reducing the voltage current and efficiency.  In addition, the oxygen and complexes of the oxygen with other elements may become active at higher temperatures, making the wafers sensitive to high temperature processing.
  • 33. FLOATING ZONE TECHNIQUE Produced by cylindrical polysilicon rod that already has a seed crystal in its lower end. An encircling inductive heating coil melts the silicon material.  The coil heater starts from the bottom and is raised pulling up the molten zone
  • 34. FLOATINGZONETECHNIQUE  A solidified single crystal ingot forms below.  Impurities prefer to remain in the molten silicon so very few defects and impurities remain in the forming crystal
  • 35. SINGLECRYSTALGROWTHTECHNIQUES Czochralski Growth (CZ)  Most single crystal silicon made this way.  Lower quality silicon than FZ with Carbon and Oxygen present.  Cheaper production than FZ.  Produces cylinders and circular wafers Float Zone (FZ)  Better Quality than CZ.  More Expensive than CZ.  Produces cylinders and circular wafers
  • 36. Ingots (poly and monocrystalline)
  • 37. Doping Si ingot  To achieve a crystal of desired resistivity, known amount of dopants is added to the melt. For silicon, boron and phosphorous are the most common dopants for p- and n- type materials For gallium arsenide, cadmium and zinc are commonly used for p-type material, while selenium , silicon, and tellurium are used for n-type material
  • 38. Doping during FZ process
  • 39. Slicing into wafers  Ingots are cut into thin wafers for solar cells(100μm to 300μm).  Two techniques :  Wire sawing  Diamond blade sawing
  • 40. Cutting of ingot into columns by wire saw
  • 41. Characteristics  By present wafering technology its difficult to cut wafers from large crystals as they are thinner than 300μm and had to retain a reasonable yield. More than half the silicon is wasted as kerfs or cutting loss in the process. Time consuming. Water cooled and dirty.
  • 42. Si wafer to solar cell
  • 43. Texturing Diffusion Edge isolation (Removal of n- material from edges) Anti Reflection Coating
  • 44. Front Ag printing (Ag printing for collection of generated carriers) Back pad printing (Ag- Al pad on the back side for soldering) Back Al printing (Al screen printing to provide contact) Solar cell
  • 45. Texturing surface  To minimize reflection from the flat surface solar cell wafers are textured by creating a roughened surface(pyramids).  By doing this, incident light will have a larger probability of being absorbed into the solar cell.  Performed by etching in a weak alkaline solution such as HF.
  • 46.
  • 47. Diffusion process  In diffusion process, impurities are introduced in a controlled manner so as to obtain pn junction in a p-type or n-type wafer.  To make solar cell, n-type impurities must be introduced in p-type wafer to give a p-n junction ,phosphorus is the impurity generally used .
  • 48. Phosphorus diffusion process  A carrier gas is bubbled through POCL3mixed with a small amount of oxygen.  It is then passed down a heated furnace in which the wafers are stacked.  An oxide layer containing phosphorous grows on the surface.  At high temperatures(800—1100°C ) , phosphorous diffuses into Si from the oxide.
  • 50. Phosphorus diffusion process After about 20 mins , the P impurities override the B impurities in the surface to give a thin , heavily doped n-type region as shown in the figure..
  • 51. Vacuum evaporation Metal contact are then attached to both the n- type and the p-type region ,the metal to be deposited is heated in a vacuum to a high enough temp to cause it to melt and vaporize, it will then condense on any cooler parts of the vacuum system in direct line of sight, including the solar cells, the back contact is normally deposited over the entire back surface, while the top contact is required in the form of a grid.
  • 52. Techniques for defining top grid 1. Use a metal shadow mask 2. The metal can be deposited over the entire front surface of the cell and subsequently etched a way from unwanted region using a photographic technique known photolithography
  • 53.
  • 54. The contact made up three separate layer 1. Thin layer of silver and aluminium is used as the bottom layer. 2. Layer of silver in the top with silver finger printing. 3. The aluminium finger printing on bottom side is done.
  • 55. Characteristics Yield of about 90% from starting wafers to completed terrestrial cells can be obtained. This make the processing very labor- intensive. The vacuum evaporation equipment is expensive compared to its throughput. the material expensive such Ag.
  • 56. Solar cells to solar module
  • 57. Cell Sorting Tabbing Stringing Module Lay up Lamination &Trimming Framing Sealing &Cleaning
  • 58. Cell Sorting  According to measured parameters of current and voltage by cell sorter.  At standard irradiation of 1000W/m^2 by pulsed xenon lamp and standard temperature of 25°C.  Cell sorter measures and displays the following cell parameters:  Complete I-V curve, Open circuit voltage ,  Short-circuit current , Short-circuit current density  Peak power, Cell efficiency (η),Fill factor (FF), Series resistance, Shunt resistance.  Max. power output. To maximize efficiency of solar module by minimizing mismatch between connected cells.
  • 59. Tabbing  Tabbing refers to connecting flat tab leads to bus bar of solar cells.  Flat tab leads:  Contains 90% silver and 10% impurities.  Now a days tinned copper ribbons are used.  High conductivity.  Two tabs per cell are employed.  Tabs provide accommodation for thermal expansion
  • 60. Stringing  Stringing is process of series connection of similar rating tabbed solar cells.  Cells in series = output voltage of a module / voltage of a cell.  Several cell strings can be internally paralleled according to power requirement from module.  Module power = voltage × current.  Each cell string is now inspected for continuity of connections before lay up process
  • 61. Module lay up The laminating materials are laid up in a sequence as shown:  3 to 4 mm thick low iron tempered glass is used.  Ethyl vinyl acetate is a thermoplastic i.e. it’s shape changes under heating are reversible.  Back layer is a composite plastic sheet (Tedlar-polyster- tedlar) provides insulation to humidity and high- electrical voltage.
  • 62. Lamination and trimming  Layout is sealed by heating (140°C-150°C) in a lamination unit.  Laminator creates a pneumatic vacuum inside the module to remove air bubbles and other gases.  EVA flows and soaks the cell.  Excess polymer sheets are trimmed off from the edges.
  • 63. Framing  Anodized aluminum frame is used.  To make handling easier.  To improve resistance to structural stress and weather conditions.  Frame must be electrically insulated from active cell circuit to sustain high electrical voltage between terminals and frame.  Junction box is attached to back side of frame and connected to laminated solar cell string.
  • 64. Sealing and cleaning  Sealing is done by using RoomTemperatureVulcanizing(RTV) silicone.  Features of RTV silicone rubber:  Light viscosity and good flow ability.  Low shrinkage Favorable tension .  No deformation.  Favorable hardness.  High temperature resistance, acid and alkali-resistance and ageing resistance  The modules are cleaned using mild chemical solution.
  • 65. Solar module to solar array
  • 66. Electrical characteristics at STC Interconnections of modules Mismatch in modules connected in series Mismatch in modules connected in parallel Role of bypass diode and blocking diode.
  • 67. Electrical characteristics atSTC Standard Test Conditions  Global radiation = 1000 W/m^2  Ambient temperature = 25°C  Spectral distribution=AM1.5  Wind speed = 1 m/s Electrical characteristics  Short circuit current (Isc)  Open circuit current (Voc)  Maximum power output (Pmax)  Fill-factor (FF)  Normal Operating Cell Temperature (NOCT)
  • 68. Interconnectionsof modules  Solar modules are connected in series or parallel depending upon the voltage and current requirement at the output.  Modules in series = (Total battery bank voltage)/ 12 V  Modules in parallel = (Array peak amp.) / (Peak amp. Per modules) where, Array peak amp. = (Average Ah per day to be supplied by the array) / (peak sunshine hour per day)
  • 69.  When two or more modules with different electrical properties are connected, the output power is determined by the modules with the lowest output power.  Interconnections have suitable bypass and blocking diode.  Mostly mismatch occur due to difference in either Isc orVoc.
  • 70. Mismatchin moduleconnectedin series In series connections, mismatch due toVoc and Isc occurs. Mismatch inVoc of modules connected in series : No mismatch in current rating, same current will be flow in the all modules. Total output voltage is summation of voltage rating of individual module.
  • 72. Mismatchin Iscofmodules connectedinseries  Current in array is due to module with the least current and further this modules act as a load.  Power gets dissipated in the poor module and this leads to:  Irreversible damage.  Hot spot formation
  • 73. Mismatchin modulesconnectedin parallel  Mismatch in parallel connections is not as severe in series.  The voltage across the module combination is always the same.  The current from the combinations of modules is the sum of the currents in the individual modules
  • 74. Roleofbypassdiode and blockingdiode  The bypass diode is connected in parallel but with opposite polarity.  Normally, for a 36-cell modules, two bypass diode are used.  It blocks the current from flowing in to the shaded modules from the parallel module.  It also prevents the flow of current from the battery to the module during in night or rainy season.
  • 75. Uses of blocking and bypass diode