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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 09 Issue: 07 | July 2022 www.irjet.net p-ISSN: 2395-0072
© 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 262
THE PERFORMANCE OF SHROUDED WIND TURBINE USING CYCLE
DYNAMO
Albin Roy1, Aman Shine2, Athul P U3, Abraham Antony4
1,2,3UG scholars Department of Mechanical Engineering, Viswajyothi College of Engineering and Technology,
Vazhakulam, Kerala, India
4 Assistant professor, Department of Mechanical Engineering Viswajyothi College of Engineering and Technology,
Vazhakulam, Kerala, India
---------------------------------------------------------------------***---------------------------------------------------------------------
Abstract - Wind energy is transformed into electrical
energy by wind turbines for distribution. Propeller-like blades
turn when the wind blows, capturing wind energy to drive the
generator and produce power. Horizontal-axis turbines and
vertical-axis turbines are the two main types of wind turbines
on the market. The power output of small wind turbines is 10
kW, whereas the power output of large-scale wind turbines
ranges from 5000 to 8000 kW. It is crucial to realize thatwind
turbines cannot function in either excessively high or
excessively low wind conditions. Only 59.3% of the kinetic
energy is transformed into electricity output utilizing wind
turbines, which is below the Betz limit. The cubic power of
velocity directly relates to the wind power generated by a
wind turbine. Therefore, a small increase in velocity might
result in a significant increase in power production. In
shrouded wind turbines, this idea is applied. The pressure
gradient produced by a diffuser shroud increases the speed of
the approaching wind. Additionally, because of the growing
sophistication of engineering and technology, the rotor size of
a wind turbine grows in direct proportion to its swept area. In
this project, we create a shrouded wind turbine with which we
run several tests with various specs and blade counts. Itaidsin
comprehension of the various outputs and efficiencies offered
by a wind turbine. The output of a wind turbine increasesasits
efficiency rises. and contributestoboostingenergyproduction.
Keywords: vertically inclined winds, Betz limit, shroud,
nozzle, diffuser.
1. INTRODUCTION
In order to generate, transmit, and integrate wind turbines
into the power system, electrical engineering is used in
conjunction with a variety of multidisciplinary and broad
technological disciplines, including aerodynamics,
mechanics, structure dynamics, and meteorology. The most
promising and dependablekindofrenewable energytodayis
wind turbine technology, which has improved over time.
Since the early 1980s, the transition from small wind
turbines with a few kilowatts to the multimegawatt wind
turbines of today has happened quite quickly.Windturbines
transform wind's kinetic energyintouseful electrical energy.
Propeller-like blades turn when the wind blows, capturing
wind energy to drive the generator and produce power.
There are two main types of wind turbines on the market:
horizontal-axis turbines and turbines with vertical axes.
Large-scale wind turbines can produce power up to 5000–
8000 kW, whereas small wind turbines have production
capability of 10–20kW.
To ascertain whether the wind flows are adequate for
generating power, the location for placing wind turbines
must also be adequately examined. A suitable wind turbine
system for the location is also found with the aid of the
evaluation. The quality of the wind resources at the area of
installation considerably affects the efficiency of wind
energy, which can reach more than 40% if the locationofthe
wind energy system is correctly chosen. It is crucial to
realize that wind turbines cannot function in either too high
or too low wind conditions.
Wind power is inversely correlated with wind speed cubed.
The output power of a wind turbine can be significantly
improved if we can harness the fluid dynamics surrounding
a structure to increase the wind speed, specifically if we can
catch and concentrate the wind energy locally. When
compared to an open turbine with a rotor of an equivalent
size, a shroud in a shrouded wind turbine serves to enhance
the velocity of the air travelling through the rotor plane.
As the size of the wind turbine increases, its costrisesandits
failure rate rises in conventional windturbines.Additionally,
those enormous wind turbines cause social issues like
increased noise (aerodynamic noise) as a result of the
turbines, an increase in the risk of bird strikes, deterioration
of the surrounding scenery as a result of the turbines'size or
their sharp blades, and more. As a result, it is challenging for
the local population to accept such enormouswindturbines,
which makes it challenging to build such wind turbines.
Scaling of blades has limitations, as several recent
investigations have shown.
In this paper, we develop a shrouded wind turbine which is
used to perform different tests according to different
specifications and number of blades. It helps in
understanding the different outputs and efficiencies in the
given specifications.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 09 Issue: 07 | July 2022 www.irjet.net p-ISSN: 2395-0072
© 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 263
1.1 Objectives
•To find out the most optimum arrangement in a shrouded
wind turbine.
•To study the difference between the performance of
conventional horizontal axis wind turbines and shrouded
wind turbines.
•To study the changes in different output parameters of a
shrouded wind turbine at different wind speeds.
•To understand the difference betweenusageofthreebladed
and five bladed rotors in horizontal axis wind turbines.
1.2 Scope
•This turbine will be capable of producing more power than
conventional horizontal axis wind turbines.
•A clear-cut image of the most optimum geometrical
arrangement to produce electricity efficiently in a shrouded
wind turbine is obtained.
•Increase in the volume of swept wind by the use of nozzle
and diffuser.
•Can be used as wind guidance system for larger wind
turbines.
2. THEORY OF WIND TURBINES
2.1 POWER IN THE WIND:
When one comprehends how the speed influences the
power, the significance of correct wind speed data becomes
apparent. Take into account a disc of area "A" with air mass
"dm" moving through it. The mass will travel a distance of'U
dt' in time dt, resulting in the formation of a cylinder with a
volume of 'A x U x dt' and a mass of ‘dm = A x ρ x U x dt’,
where " denotes the air density. The temporal rate ofchange
in kinetic energy, or the power contained in the moving
mass, is given by P = d(KE) / dt = d (½ x mU²)/ dt = ½ x U²
dm / dt = ½ x A x ρ U³.
As a result, power is inversely related to wind speed cubed.
The wind speed must be precisely known because any
inaccuracy in the power calculation is amplified.
2.2 BETZ’S LAW:
Independent of the design of a wind turbine operating in
open flow, Betz's law identifies the maximum power that
may be obtained from the wind. For all Newtonian fluids,
including wind, Betz's law is applicable. The wind speed
would decrease to zero if all of the energy from wind
movement via a turbine were collected as useable energy. A
blockage would prevent any additional fresh wind from
entering if the wind stopped blowing at the turbine's exit.
There must be some wind movement, however slight,on the
opposite side with some wind speed greater than zero in
order to maintain the wind going through the turbine.
According to Betz's law, as an area's airflow increasesandas
energy is lost during energy extraction from a turbine, wind
speed drops, requiring airflow to be distributed across a
larger region. Geometrythereforerestrictsturbineefficiency
to a maximum of 59.3%.
2.3 BETZ LIMIT:
The Betz limit is based on an open-disk actuator. More
energy can be obtained if a diffuser is employed to gather
more wind and route it through the turbine, butthelimitstill
applies to the cross-section of the overall structure.
The Betz Limit is the most energy that can be extracted from
a fluid moving at a specific speed using an infinitely thin
rotor.
The Betz Limit is the most energy that can be extracted from
a fluid moving at a specific speed using an infinitely thin
rotor.
Assumptions:
1. The rotor is ideal, without a hub, and has an infinite
number of blades that are completely free of drag. Any
ensuing drag would only make this ideal value smaller.
2. Axial flow enters and exits the rotor. In order to create a
solution for this control-volume analysis,thecontrol volume
must include all incoming and outgoing flow; otherwise, the
conservation equations would be broken.
3. There is no compression of the flow. There is no heat
transfer, and the density does not change.
4. The disc or rotor is subjected to a uniform thrust.
2.4 THEORY OF SHROUDED TURBINES:
The theory behind revealed that a diffuser-shaped structure
can accelerate the wind at the entrance of the body. Using a
nozzle will reduce the pressure and increase the velocity of
air intake and cuts the blades. As the air leaves through the
diffuser the pressureisincreasedreducingthevelocity.Since
the change in pressure is continuous a smooth flow of air
occurs.
3. METHODOLOGY
The fabrication work began with the production of two type
of blades; 5-blade and 3-blade, made of PVC. Then theywere
bolted onto a bearing housing made of cylinder pipe of
diameter 50mm and a bearing of internal diameter 16mm
(SKF 6202) was fixed into the cylindrical pipe, as shown in
fig 1.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 09 Issue: 07 | July 2022 www.irjet.net p-ISSN: 2395-0072
© 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 264
Fig – 1: Rotor
For power generation a standard bicycle dynamo of head
diameter of 20mm is used. The typical electrical output
produced from a bicycle dynamo is 12 volts. Dynamos have
traditionally been used to power lights with alternating
current (AC). There have been sufficient advancements in
battery technology, LED light technology, and charging
technology as we havemovedintoa worldofcommunication
and become more efficient. The bicycledynamowascoupled
to a wheel of diameter 100mm for speed addition to the
dynamo as shown in fig 2. A speed ratio of 5:1 is achieved on
the dynamo.
Fig - 2: Wheel and dynamo (speed addition)
The shroud was clipped onto the outer peripherical ring of
the arrangement to complete the fabrication work. A bulb
was connected to the dynamo using a regulator IC (IC 7305)
in series with two resistors in parallel (630 ohm) to the
dynamo. The completed fabrication of shrouded wind
turbine producing an output using dynamo is shown in fig 3.
Fig – 3: Shrouded wind turbine
Specifications Of the Fabricated Wind Turbine:
 Throat diameter = 710mm
 Length of the blades = 310mm
 Rotor diameter = 705mm
 Tower Height = 1210mm
 Nozzle inlet diameter = 760mm
 Diffuser outlet diameter = 850mm
 Bearing housing diameter = 50mm
 Dynamo rotating ridged
knob diameter = 20mm
 Addition wheel diameter = 100mm
 L/D Ratio, L/D = 0.44
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 09 Issue: 07 | July 2022 www.irjet.net p-ISSN: 2395-0072
© 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 265
4. RESULT AND DISCUSSION
The various tests are conducted with the use of wind tunnel
at constant wind speed. A constant wind speed is obtained
by setting a constant value for rpm of the wind tunnel. After
setting a constant wind speed the different parameters like
variation in output voltage, variation in rpm of the rotor
shaft, cut-in wind speed, etc. are recorded for different
arrangement of the blades, nozzle and diffuser. Two sets of
wind speeds are used – 6.3m/s and 5.1m/s.
4.1 VOTAGE VARIATIONS AT 6.3 m/s
The wind speed is set to a constant value of 6.3m/s by
setting the wind tunnel to 625rpmandthevoltagevariations
of the 3-blade and 5-blade arrangement are recorded by
using a multimeter for the below shown geometrical
parameters.
Table 1 below shows the values obtained in volts(V) for
different geometrical parameters.
Table -1: Voltage variations at 6.3m/s
TESTS 5 BLADE 3 BLADE
REFERENCE
TEST
4.0V 5.5V
NOZZLE ONLY 7.8V 7.1V
NOZZLE+
DIFFUSER
8.8V 9.7V
DIFFUSER ONLY 6.9V 6.1V
A chart is plotted showing the voltage variations at 6.3m/s
as shown in chart 1 below:
Chart 1: Voltage variation graph at 6.3m/s
Here the reference test or the test without the addition any
nozzle or diffuser has the least output. With the addition of
nozzle, a marginal increase in voltageoutputisseen.Diffuser
alone has lesser output than nozzle alone since the intake of
air is less in the beginning. The intake of wind is increased
with nozzle. The diffuser alone arrangementcanonlyreduce
the pressure but the pressure reduction can only happen
with the use of nozzle. But with the help of both nozzle and
diffuser the pressure reduction and addition can happen
simultaneously in both nozzle and diffuser arrangement
(shroud). The value has significantly increased with the use
of shroud to approximately from 4V to 10V. Shroud
arrangement offers higher output and load carrying
capability. With the increase in output gives more power.
4.2 RPM VARIATIONS AT 6.3 m/s
The wind speed is set to a constant value of 6.3m/s by
setting the wind tunnel to 625rpm and the rpm variationsof
the 3-blade and 5-blade arrangement are recorded by using
a tachometer for the below shown geometrical parameters.
Table 2 below shows the values obtained in revolutions per
minute(rpm) for different parameters.
Table -2: RPM variations at 6.3m/s
TESTS 5 BLADE 3 BLADE
REFERENCE
TEST
220 rpm 250 rpm
NOZZLE ONLY 230 rpm 260 rpm
NOZZLE+
DIFFUSER
360 rpm 410 rpm
DIFFUSER ONLY 300 rpm 320 rpm
A chart showing the variations of rpm at 6.3m/s is shown in
chart 2 above.
Chart 2: RPM variation graph at 6.3m/s
Here the reference test has the least output. With the
addition of nozzle, a marginal increase in rpmoutputisseen.
Diffuser alone has lesser output than nozzle alone since the
intake of air is less in the beginning. The intake of wind is
increased with nozzle. The diffuser alone arrangement can
only reduce the pressurebut thepressurereductioncanonly
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 09 Issue: 07 | July 2022 www.irjet.net p-ISSN: 2395-0072
© 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 266
happen with the use of nozzle. But with the help of both
nozzle and diffuser the pressure reduction and addition can
happen simultaneously in both nozzle and diffuser
arrangement (shroud). The value has significantlyincreased
with the use of shroud to approximately from 220 rpm to
410 rpm. Shroud arrangement offers higher outputandload
carrying capability. With the increase in output gives more
power.
4.3 VOTAGE VARIATIONS AT 5.1 m/s
The wind speed is set to a constant value of 5.1m/s by
setting the wind tunnel to 555rpmandthevoltagevariations
of the 3-blade and 5-blade arrangement are recorded by
using a multimeter for the below shown geometrical
parameters.
Table 3 below shows the values obtained in volts(V) for
different parameters.
Table -3: Voltage variations at 5.1m/s
TESTS 5 BLADE 3 BLADE
REFERENCE
TEST
3.8V 5.2V
NOZZLE ONLY 4.2V 5.7V
NOZZLE+
DIFFUSER
6.8V 8.9V
DIFFUSER ONLY 3.9V 5.3V
A chart showing the voltage variationsat5.1m/sasshownin
chart 3 below:
Chart 3: Voltage variation graph at 5.1m/s
4.4 RPM VARIATIONS AT 5.1 m/s
The wind speed is set to a constant value of 5.1m/s by
setting the wind tunnel to 555rpm and the rpm variationsof
the 3-blade and 5-blade arrangement are recorded by using
a tachometer for the below shown geometrical parameters.
Table 4 below shows the values obtained in revolutions per
minute (rpm) for different parameters.
Table -4: RPM variations at 5.1m/s
TESTS 5 BLADE 3 BLADE
REFERENCE
TEST
215 245
NOZZLE ONLY 220 255
NOZZLE+
DIFFUSER
285 410
DIFFUSER ONLY 225 280
A chart is plotted showing the rpm variations at 5.1m/s as
shown in chart 4 below:
Chart 4: RPM variation graph at 5.1m/s
o CUT-IN WIND SPEED
 Reference test - 4.2m/s
 Nozzle only - 3.6m/s
 Diffuser only - 3.8m/s
 Nozzle+
Diffuser - 3.0m/s
5. CONCLUSIONS
To increase the output of the HAWTs we proposed the
design of shroud into the system. By doing so we were able
to increase the output by 2-3 times. Since this project used a
cycle dynamo the varying output was limited. The output
was limited to 12V maximum. Although, the range of output
was limited, the increaseinvoltageandrpmweresignificant.
The output varied from 4V to 10V and the rpm from 215 –
410 rpm. Among the various arrangements we used the
nozzle and diffuser arrangement was the best suited to
produce the best result. It gave an output voltageof9.7Vand
410rpm. Wind turbines with nozzle-diffusers can
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 09 Issue: 07 | July 2022 www.irjet.net p-ISSN: 2395-0072
© 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 267
significantly improve rotor performance. Thisisbecausethe
wind turbine inside the diffuser is drawn to more mass flow
by a low-pressure area created by a strong vortex formation
behind the broad diffuser. The ability of creating a pressure
difference produces an output that far exceeds the normal
HAWTs. Even for a slight variation in applied wind load a
significant output can be produced. Improved research will
be fruitful in utilizing the unlimited resources that are free
and bountiful in nature. Since the usage of fossil fuels are
very high, developments in wind energy production can be
very resourceful
REFERENCES
[1] Ohya, Y. and Karasudani, T., 2010. A shrouded wind
turbine generating high output power with wind-lens
technology. Energies, 3(4), pp.634-649.
[2] Pambudi, N.A., Febriyanto, R., Wibowo, K.M., Setyawan,
N.D., Wardani, N.S., Saw, L.H. and Rudiyanto, B., 2019.
The performance of shrouded wind turbine at low wind
speed condition. Energy Procedia, 158, pp.260-265.
[3] Alquraishi, B.A., Asmuin, N.Z., Mohd, S., Abd Al-Wahid,
W.A. and Mohammed, A.N., 2019. Review on Diffuser
AugmentedWindTurbine(DAWT). InternationalJournal
of Integrated Engineering, 11

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THE PERFORMANCE OF SHROUDED WIND TURBINE USING CYCLE DYNAMO

  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 09 Issue: 07 | July 2022 www.irjet.net p-ISSN: 2395-0072 © 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 262 THE PERFORMANCE OF SHROUDED WIND TURBINE USING CYCLE DYNAMO Albin Roy1, Aman Shine2, Athul P U3, Abraham Antony4 1,2,3UG scholars Department of Mechanical Engineering, Viswajyothi College of Engineering and Technology, Vazhakulam, Kerala, India 4 Assistant professor, Department of Mechanical Engineering Viswajyothi College of Engineering and Technology, Vazhakulam, Kerala, India ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract - Wind energy is transformed into electrical energy by wind turbines for distribution. Propeller-like blades turn when the wind blows, capturing wind energy to drive the generator and produce power. Horizontal-axis turbines and vertical-axis turbines are the two main types of wind turbines on the market. The power output of small wind turbines is 10 kW, whereas the power output of large-scale wind turbines ranges from 5000 to 8000 kW. It is crucial to realize thatwind turbines cannot function in either excessively high or excessively low wind conditions. Only 59.3% of the kinetic energy is transformed into electricity output utilizing wind turbines, which is below the Betz limit. The cubic power of velocity directly relates to the wind power generated by a wind turbine. Therefore, a small increase in velocity might result in a significant increase in power production. In shrouded wind turbines, this idea is applied. The pressure gradient produced by a diffuser shroud increases the speed of the approaching wind. Additionally, because of the growing sophistication of engineering and technology, the rotor size of a wind turbine grows in direct proportion to its swept area. In this project, we create a shrouded wind turbine with which we run several tests with various specs and blade counts. Itaidsin comprehension of the various outputs and efficiencies offered by a wind turbine. The output of a wind turbine increasesasits efficiency rises. and contributestoboostingenergyproduction. Keywords: vertically inclined winds, Betz limit, shroud, nozzle, diffuser. 1. INTRODUCTION In order to generate, transmit, and integrate wind turbines into the power system, electrical engineering is used in conjunction with a variety of multidisciplinary and broad technological disciplines, including aerodynamics, mechanics, structure dynamics, and meteorology. The most promising and dependablekindofrenewable energytodayis wind turbine technology, which has improved over time. Since the early 1980s, the transition from small wind turbines with a few kilowatts to the multimegawatt wind turbines of today has happened quite quickly.Windturbines transform wind's kinetic energyintouseful electrical energy. Propeller-like blades turn when the wind blows, capturing wind energy to drive the generator and produce power. There are two main types of wind turbines on the market: horizontal-axis turbines and turbines with vertical axes. Large-scale wind turbines can produce power up to 5000– 8000 kW, whereas small wind turbines have production capability of 10–20kW. To ascertain whether the wind flows are adequate for generating power, the location for placing wind turbines must also be adequately examined. A suitable wind turbine system for the location is also found with the aid of the evaluation. The quality of the wind resources at the area of installation considerably affects the efficiency of wind energy, which can reach more than 40% if the locationofthe wind energy system is correctly chosen. It is crucial to realize that wind turbines cannot function in either too high or too low wind conditions. Wind power is inversely correlated with wind speed cubed. The output power of a wind turbine can be significantly improved if we can harness the fluid dynamics surrounding a structure to increase the wind speed, specifically if we can catch and concentrate the wind energy locally. When compared to an open turbine with a rotor of an equivalent size, a shroud in a shrouded wind turbine serves to enhance the velocity of the air travelling through the rotor plane. As the size of the wind turbine increases, its costrisesandits failure rate rises in conventional windturbines.Additionally, those enormous wind turbines cause social issues like increased noise (aerodynamic noise) as a result of the turbines, an increase in the risk of bird strikes, deterioration of the surrounding scenery as a result of the turbines'size or their sharp blades, and more. As a result, it is challenging for the local population to accept such enormouswindturbines, which makes it challenging to build such wind turbines. Scaling of blades has limitations, as several recent investigations have shown. In this paper, we develop a shrouded wind turbine which is used to perform different tests according to different specifications and number of blades. It helps in understanding the different outputs and efficiencies in the given specifications.
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 09 Issue: 07 | July 2022 www.irjet.net p-ISSN: 2395-0072 © 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 263 1.1 Objectives •To find out the most optimum arrangement in a shrouded wind turbine. •To study the difference between the performance of conventional horizontal axis wind turbines and shrouded wind turbines. •To study the changes in different output parameters of a shrouded wind turbine at different wind speeds. •To understand the difference betweenusageofthreebladed and five bladed rotors in horizontal axis wind turbines. 1.2 Scope •This turbine will be capable of producing more power than conventional horizontal axis wind turbines. •A clear-cut image of the most optimum geometrical arrangement to produce electricity efficiently in a shrouded wind turbine is obtained. •Increase in the volume of swept wind by the use of nozzle and diffuser. •Can be used as wind guidance system for larger wind turbines. 2. THEORY OF WIND TURBINES 2.1 POWER IN THE WIND: When one comprehends how the speed influences the power, the significance of correct wind speed data becomes apparent. Take into account a disc of area "A" with air mass "dm" moving through it. The mass will travel a distance of'U dt' in time dt, resulting in the formation of a cylinder with a volume of 'A x U x dt' and a mass of ‘dm = A x ρ x U x dt’, where " denotes the air density. The temporal rate ofchange in kinetic energy, or the power contained in the moving mass, is given by P = d(KE) / dt = d (½ x mU²)/ dt = ½ x U² dm / dt = ½ x A x ρ U³. As a result, power is inversely related to wind speed cubed. The wind speed must be precisely known because any inaccuracy in the power calculation is amplified. 2.2 BETZ’S LAW: Independent of the design of a wind turbine operating in open flow, Betz's law identifies the maximum power that may be obtained from the wind. For all Newtonian fluids, including wind, Betz's law is applicable. The wind speed would decrease to zero if all of the energy from wind movement via a turbine were collected as useable energy. A blockage would prevent any additional fresh wind from entering if the wind stopped blowing at the turbine's exit. There must be some wind movement, however slight,on the opposite side with some wind speed greater than zero in order to maintain the wind going through the turbine. According to Betz's law, as an area's airflow increasesandas energy is lost during energy extraction from a turbine, wind speed drops, requiring airflow to be distributed across a larger region. Geometrythereforerestrictsturbineefficiency to a maximum of 59.3%. 2.3 BETZ LIMIT: The Betz limit is based on an open-disk actuator. More energy can be obtained if a diffuser is employed to gather more wind and route it through the turbine, butthelimitstill applies to the cross-section of the overall structure. The Betz Limit is the most energy that can be extracted from a fluid moving at a specific speed using an infinitely thin rotor. The Betz Limit is the most energy that can be extracted from a fluid moving at a specific speed using an infinitely thin rotor. Assumptions: 1. The rotor is ideal, without a hub, and has an infinite number of blades that are completely free of drag. Any ensuing drag would only make this ideal value smaller. 2. Axial flow enters and exits the rotor. In order to create a solution for this control-volume analysis,thecontrol volume must include all incoming and outgoing flow; otherwise, the conservation equations would be broken. 3. There is no compression of the flow. There is no heat transfer, and the density does not change. 4. The disc or rotor is subjected to a uniform thrust. 2.4 THEORY OF SHROUDED TURBINES: The theory behind revealed that a diffuser-shaped structure can accelerate the wind at the entrance of the body. Using a nozzle will reduce the pressure and increase the velocity of air intake and cuts the blades. As the air leaves through the diffuser the pressureisincreasedreducingthevelocity.Since the change in pressure is continuous a smooth flow of air occurs. 3. METHODOLOGY The fabrication work began with the production of two type of blades; 5-blade and 3-blade, made of PVC. Then theywere bolted onto a bearing housing made of cylinder pipe of diameter 50mm and a bearing of internal diameter 16mm (SKF 6202) was fixed into the cylindrical pipe, as shown in fig 1.
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 09 Issue: 07 | July 2022 www.irjet.net p-ISSN: 2395-0072 © 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 264 Fig – 1: Rotor For power generation a standard bicycle dynamo of head diameter of 20mm is used. The typical electrical output produced from a bicycle dynamo is 12 volts. Dynamos have traditionally been used to power lights with alternating current (AC). There have been sufficient advancements in battery technology, LED light technology, and charging technology as we havemovedintoa worldofcommunication and become more efficient. The bicycledynamowascoupled to a wheel of diameter 100mm for speed addition to the dynamo as shown in fig 2. A speed ratio of 5:1 is achieved on the dynamo. Fig - 2: Wheel and dynamo (speed addition) The shroud was clipped onto the outer peripherical ring of the arrangement to complete the fabrication work. A bulb was connected to the dynamo using a regulator IC (IC 7305) in series with two resistors in parallel (630 ohm) to the dynamo. The completed fabrication of shrouded wind turbine producing an output using dynamo is shown in fig 3. Fig – 3: Shrouded wind turbine Specifications Of the Fabricated Wind Turbine:  Throat diameter = 710mm  Length of the blades = 310mm  Rotor diameter = 705mm  Tower Height = 1210mm  Nozzle inlet diameter = 760mm  Diffuser outlet diameter = 850mm  Bearing housing diameter = 50mm  Dynamo rotating ridged knob diameter = 20mm  Addition wheel diameter = 100mm  L/D Ratio, L/D = 0.44
  • 4. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 09 Issue: 07 | July 2022 www.irjet.net p-ISSN: 2395-0072 © 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 265 4. RESULT AND DISCUSSION The various tests are conducted with the use of wind tunnel at constant wind speed. A constant wind speed is obtained by setting a constant value for rpm of the wind tunnel. After setting a constant wind speed the different parameters like variation in output voltage, variation in rpm of the rotor shaft, cut-in wind speed, etc. are recorded for different arrangement of the blades, nozzle and diffuser. Two sets of wind speeds are used – 6.3m/s and 5.1m/s. 4.1 VOTAGE VARIATIONS AT 6.3 m/s The wind speed is set to a constant value of 6.3m/s by setting the wind tunnel to 625rpmandthevoltagevariations of the 3-blade and 5-blade arrangement are recorded by using a multimeter for the below shown geometrical parameters. Table 1 below shows the values obtained in volts(V) for different geometrical parameters. Table -1: Voltage variations at 6.3m/s TESTS 5 BLADE 3 BLADE REFERENCE TEST 4.0V 5.5V NOZZLE ONLY 7.8V 7.1V NOZZLE+ DIFFUSER 8.8V 9.7V DIFFUSER ONLY 6.9V 6.1V A chart is plotted showing the voltage variations at 6.3m/s as shown in chart 1 below: Chart 1: Voltage variation graph at 6.3m/s Here the reference test or the test without the addition any nozzle or diffuser has the least output. With the addition of nozzle, a marginal increase in voltageoutputisseen.Diffuser alone has lesser output than nozzle alone since the intake of air is less in the beginning. The intake of wind is increased with nozzle. The diffuser alone arrangementcanonlyreduce the pressure but the pressure reduction can only happen with the use of nozzle. But with the help of both nozzle and diffuser the pressure reduction and addition can happen simultaneously in both nozzle and diffuser arrangement (shroud). The value has significantly increased with the use of shroud to approximately from 4V to 10V. Shroud arrangement offers higher output and load carrying capability. With the increase in output gives more power. 4.2 RPM VARIATIONS AT 6.3 m/s The wind speed is set to a constant value of 6.3m/s by setting the wind tunnel to 625rpm and the rpm variationsof the 3-blade and 5-blade arrangement are recorded by using a tachometer for the below shown geometrical parameters. Table 2 below shows the values obtained in revolutions per minute(rpm) for different parameters. Table -2: RPM variations at 6.3m/s TESTS 5 BLADE 3 BLADE REFERENCE TEST 220 rpm 250 rpm NOZZLE ONLY 230 rpm 260 rpm NOZZLE+ DIFFUSER 360 rpm 410 rpm DIFFUSER ONLY 300 rpm 320 rpm A chart showing the variations of rpm at 6.3m/s is shown in chart 2 above. Chart 2: RPM variation graph at 6.3m/s Here the reference test has the least output. With the addition of nozzle, a marginal increase in rpmoutputisseen. Diffuser alone has lesser output than nozzle alone since the intake of air is less in the beginning. The intake of wind is increased with nozzle. The diffuser alone arrangement can only reduce the pressurebut thepressurereductioncanonly
  • 5. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 09 Issue: 07 | July 2022 www.irjet.net p-ISSN: 2395-0072 © 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 266 happen with the use of nozzle. But with the help of both nozzle and diffuser the pressure reduction and addition can happen simultaneously in both nozzle and diffuser arrangement (shroud). The value has significantlyincreased with the use of shroud to approximately from 220 rpm to 410 rpm. Shroud arrangement offers higher outputandload carrying capability. With the increase in output gives more power. 4.3 VOTAGE VARIATIONS AT 5.1 m/s The wind speed is set to a constant value of 5.1m/s by setting the wind tunnel to 555rpmandthevoltagevariations of the 3-blade and 5-blade arrangement are recorded by using a multimeter for the below shown geometrical parameters. Table 3 below shows the values obtained in volts(V) for different parameters. Table -3: Voltage variations at 5.1m/s TESTS 5 BLADE 3 BLADE REFERENCE TEST 3.8V 5.2V NOZZLE ONLY 4.2V 5.7V NOZZLE+ DIFFUSER 6.8V 8.9V DIFFUSER ONLY 3.9V 5.3V A chart showing the voltage variationsat5.1m/sasshownin chart 3 below: Chart 3: Voltage variation graph at 5.1m/s 4.4 RPM VARIATIONS AT 5.1 m/s The wind speed is set to a constant value of 5.1m/s by setting the wind tunnel to 555rpm and the rpm variationsof the 3-blade and 5-blade arrangement are recorded by using a tachometer for the below shown geometrical parameters. Table 4 below shows the values obtained in revolutions per minute (rpm) for different parameters. Table -4: RPM variations at 5.1m/s TESTS 5 BLADE 3 BLADE REFERENCE TEST 215 245 NOZZLE ONLY 220 255 NOZZLE+ DIFFUSER 285 410 DIFFUSER ONLY 225 280 A chart is plotted showing the rpm variations at 5.1m/s as shown in chart 4 below: Chart 4: RPM variation graph at 5.1m/s o CUT-IN WIND SPEED  Reference test - 4.2m/s  Nozzle only - 3.6m/s  Diffuser only - 3.8m/s  Nozzle+ Diffuser - 3.0m/s 5. CONCLUSIONS To increase the output of the HAWTs we proposed the design of shroud into the system. By doing so we were able to increase the output by 2-3 times. Since this project used a cycle dynamo the varying output was limited. The output was limited to 12V maximum. Although, the range of output was limited, the increaseinvoltageandrpmweresignificant. The output varied from 4V to 10V and the rpm from 215 – 410 rpm. Among the various arrangements we used the nozzle and diffuser arrangement was the best suited to produce the best result. It gave an output voltageof9.7Vand 410rpm. Wind turbines with nozzle-diffusers can
  • 6. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 09 Issue: 07 | July 2022 www.irjet.net p-ISSN: 2395-0072 © 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 267 significantly improve rotor performance. Thisisbecausethe wind turbine inside the diffuser is drawn to more mass flow by a low-pressure area created by a strong vortex formation behind the broad diffuser. The ability of creating a pressure difference produces an output that far exceeds the normal HAWTs. Even for a slight variation in applied wind load a significant output can be produced. Improved research will be fruitful in utilizing the unlimited resources that are free and bountiful in nature. Since the usage of fossil fuels are very high, developments in wind energy production can be very resourceful REFERENCES [1] Ohya, Y. and Karasudani, T., 2010. A shrouded wind turbine generating high output power with wind-lens technology. Energies, 3(4), pp.634-649. [2] Pambudi, N.A., Febriyanto, R., Wibowo, K.M., Setyawan, N.D., Wardani, N.S., Saw, L.H. and Rudiyanto, B., 2019. The performance of shrouded wind turbine at low wind speed condition. Energy Procedia, 158, pp.260-265. [3] Alquraishi, B.A., Asmuin, N.Z., Mohd, S., Abd Al-Wahid, W.A. and Mohammed, A.N., 2019. Review on Diffuser AugmentedWindTurbine(DAWT). InternationalJournal of Integrated Engineering, 11