by dr adil sarwar · dr adil sarwar . layout of lecture •wind potential of the world •global...
TRANSCRIPT
Wind Power By
Dr Adil Sarwar
Layout of Lecture
• Wind potential of the world
• Global wind installed capacity
• India: Wind installed Potential
• India: Wind installed Capacity
• Wind Energy basics
• Wind turbines classifications
Wind Potential 80 m=748 GW
Wind Energy basics
• Wind is air in motion.
• It is produced by the uneven heating of the earth's surface by the sun.
• Since the earth's surface is made of various land and water formations, it absorbs the sun's radiation unevenly.
• Hot air rises and cool air sinks. This brings about spatial differences in atmospheric pressure, caused by uneven heating.
Contd…
• Moderate to high speed winds, typically from 5 m/s to about 25 m/s are considered favourable for most wind turbine.
• The global potential in wind energy for large scale grid connected power generation has been estimated as 9000TWh/year.
Flow of Wind
Factors affecting flow of wind
• On the planetary level, great mountain masses influence the circulation of air current.
• Surface roughness or friction, owning to the resistance that different elements of the earth’s surface offer to air circulation affects the nature of wind.
• Climatic disturbances such as downdraught from thunderclouds and precipitation also affect the local winds.
• Winds speed also increases while passing through narrow mountain gaps, where it gets channelled.
Earlier Use
Wind Mill Vs Wind Turbine
Brief History
• The idea of harnessing wind is not new.
• Windmills were used in Babylon and China around 2000 to 1700 BC to pump water and grind grains.
• It was used traditionally been used worldwide for ship propulsion until start of industrialisation era.
• Europeans were the first to introduce the horizontal axis windmill around the 12th century, and by 1750, Holland had 8000 wind mills and England had 10000.
Present Scenario
• Several demonstration and commercial plants of different sizes, from few MW are in operation in different parts of the world.
• Improved turbine design and plant utilization have contributed to large scale reduction of wind energy generation cost from Rs 17.00 kWh in 1980 to about Rs 2.50 per kWh at present, at favourable location.
• The installation cost has come down to level comparable to that of a conventional thermal power plant i.e. to 4.00 crore Rs/MW.
• It is fastest growing energy source among all renewable resources in recent years.
How wind turbine works
Energy estimation of wind
• If uo is the speed of free wind in unperturbed state, the volume of air column passing through an area A per unit time is given by Auo .
• If ρ is the density of air column ,the air-mass flow rate, through area A, is given as ρAuo .
• Thus power(Po) available in wind, is equal to kinetic energy associated with the mass of moving air, i.e.,
Po=½ (ρAuo)uo² or Po=½(ρA)(uo)³ (1)
• Power available in wind per unit area is
Po/A = ½ρ(uo)³ , (2)
this indicates that power available in wind is proportional to the cube of wind speed.
• If a typical value of wind density ,ρ at 15°C at sea level is 1.2kg/m³, then power available in moderate wind of 10m/s is 600W/m³.
Power Extraction from wind
• A wind turbine is used to harness useful mechanical power from wind.
• For a simple analysis an unperturbed smooth laminar flow is assumed. A horizontal wind turbine which is most commonly used , is considered.
• The rotor may be considered as an actuator disk across which there is decrease in pressure as energy is extracted.
• As air mass flow rate must be same everywhere within the stream tube , the speed must decrease as air expands.
• The stream tube model, also known as Betz model of expanding air stream tube is shown as
uo Ao uo
(a)Unperturbed wind stream tube in absence of turbine
uo u1 u2
Upstream Downstream zo z2
(b)Wind stream tube in presence of turbine
Fig. Betz model
• As per the Betz model, the stream tube area of constant air mass is Ao upstream, which expands to A1 while passing through the rotor and becomes A2 downstream.
• The wind speed is uo upstream, which reduces to u1 while passing through the rotor and becomes u2 downstream.
• The air-mass flow rate remains constant throughout. Therefore,
m̊= ρAouo = ρA1u1 =ρA2u2 .......(3)
The force/thrust on rotor is equal to the reduction in momentum per unit time from the air mass flow rate m̊:
F= m̊uo-m̊u2 …….(4)
This force is applied by the air at uniform air flow speed of u1, passing through the turbine. The power extracted is
PT= Fu1 = m̊ (uo-u2)u1 ……….(5)
• The wind power extracted from is also equal to loss in KE per unit time. Thus,
PW= ½m̊(uo²-u2²) ……(6)
Equating eqn. 5 & 6, we have
u1= (uo+u2)/2 ……(7)
An interference factor, a is defined as fractional wind speed decrease at the turbine thus:
a= (uo-u1)/uo ………(8)
or u1=(1-a)/uo
or a=(uo-u2)/(2uo) ……...(9)
a is also known as the Induction factor.
• Using eqns. 3, 5, 7 & 8, power extracted by the turbine may be written as:
PT=4a(1-a²)(½ρA1uo³) (10)
comparing with eqn.2 :
PT=CpPo (11)
where Cp is the fraction of available power in the wind that can be extracted and is known as power coefficient. Cp is given as:
Cp =4a(1-a²) (12)
• The variation of power coefficient with the interference factor a is shown graphically in the figure below
0.7
0.6
0.5
0.4
0.3
0.1
0 0.2 0.4 0.6 0.8 1.0
a
Fig. CP versus a
• When no load is coupled to the turbine, the blades just freewheel. There is no reduction of wind speed at the turbine, therefore, u1=uo and the value of a is zero. The turbine does not generate any power.
• Now as load is applied, power is extracted, so Cp increase as u1 decreases. Maximum value of Cp (i.e.,Cpmax=16/27=.593) occurs at a=1/3.At this condition, u1=2uo/3 and u2=uo/3.
That means at maximum power extraction condition, the upstream wind speed is reduced to two-third at the turbine at the turbine and further reduced to one third downstream.
• The criterion for maximum power extraction, i.e., Cp=16/27 is called the Betz criterion. This applies to an ideal case. For a commercial wind turbine, however, maximum power coefficient is less than the ideal value.
• When u2=0, a=0.5 and the simple model breaks down as no wind is predicted to be leaving downstream. In practice, this is equivalent to the onset of a turbulence downstream.
• Power extraction decrease due to mismatch of rotational frequency and wind speed and partial stalling begins. The turbine blades will still be turning, causing extensive turbulence in the air stream, leading to more losses.
• When the speed reduces to zero, a becomes unity and no power is extracted. This state is known as (complete) stall state of blades.
• Betz Criterion:
In practice, all of the kinetic energy in the wind cannot be converted to shaft power since the air must be able to flow away the rotor area. The Betz criteria, derived using the principles of conservation of momentum and conservation of energy, suggests a maximum possible turbine efficiency, (or power coefficient) of 59%. In practice, power coefficients of 20-30% are more common.
Types of Wind Turbine
• Horizontal Axis Wind Turbine (HAWT)
Dutch windmills
Multi-blade water pumping windmills
High speed propeller type wind machines
• Vertical Axis Wind Turbine (VAWT)
Darrieus
Savonius
HAWT
Axis of rotation is horizontal w.r.t Ground.
HAWT’s have emerged as the most widely
used turbines.
These are being used for commercial energy
generation in many parts of the world.
Their theoretical basis is well researched and
sufficient field experience is available with
them.
31
Main Components
Turbine Blades
Hub
Nacelle
Yaw-control Mechanism
Tower 32
Turbine Blades
These are made of high density wood or glass fiber
and epoxy composites.
They have an air foil type of cross section.
The blades are slightly twisted from the outer tip to
the root to reduce the tendency to stall.
In addition to centrifugal force and fatigue due to
continuous vibrations, there are many extraneous
forces arising from wind turbulence, gust,
gravitational forces, and directional change in the
wind.
All these factors are to be taken care off at the
designing stage. 33
App. Dia. of MW range, modern rotor is 100 m.
Modern wind turbines have two or three blades.
Two/three blades rotor HAWT are also known as
propeller-type wind turbines owing to their similarity
with propeller of old aeroplanes.
However, the rotor rpm in case is case of a wind
turbine is very low as compared to that for propeller.
34
Relative merits and demerits of two and three blade rotors:
Compared to the two-blade, the three blades machine has
smoother power output and balanced gyroscopic force.
There is no need to teeter (to the discussed later in this
section) the rotor allowing the use of a simple rigid hub. The
blades may be cross –linked for greater rigidity.
Adding a third blade increase the power output by about 5%
only, while the weight and cost of a rotor increases by 50%,
thus giving a diminished rate of return for additional 50%
weight and cost.
35
The two-blades rotor is also simpler to erect, since it
can be assembled on the ground and lifted to the shaft
without complicated maneuvers during the lift.
Three blades are more common in Europe and other
developing countries including India. The American
practice, however, is in favour of two blades.
36
HUB
The Center solid portion of the rotor wheel is known
as hub.
All blades are attached to the hub.
The mechanism for pitch angle control is also
provided inside the hub.
37
NACELLE
The term nacelle is derived from the name for housing
containing the engine of an aircraft.
The rotor is attached to the nacelle, and mounted at the
top of a tower.
It contain rotor brakes, gearbox, generator and electric
switchgear and control.
38
Brakes are used to stop rotor when power generator is
not desired.
The gearbox steps up the shaft rpm to suit the
generator.
Protection and control functions are provided by
switchgear and control block.
The generator electrical power is conducted to ground
terminals through a cable.
39
Yaw-control Mechanism
Adjusting the nacelle about the vertical axis to bring
the rotor facing the wind is known as yaw control.
The yaw-control system continuously orients the rotor
in the direction of wind.
For localities with prevailing wind in one direction
only, the rotor can be in a fixed orientation. Such a
machine is said to be yaw fixed.
40
Most wind turbines however, are yaw active.
In small wind turbines, a tail vane is used for passive
yaw control.
In large turbines however, an active yaw control with
power steering and wind direction sensor is used to
maintain the orientation.
41
Control mechanism in wind turbine
Types of Rotors
Depending on the number of blade, wind speed and
nature of application rotors have been developed in
various types of shapes and size.
43
The type of rotors shown in (a) to (e) are relatively
high speed ones, suitable for application such as
electric power generation.
Large HAWTs have been manufactured with two and
three blades.
A single blade rotor, with a balancing counterweight
is economical, has simple controls but it is noisier and
produces unbalanced forces.
It is used for low-power applications.
44
Those given in (f) and (g) are low-power rotor and
most suited for water-lifting applications, which
require a high starting torque.
They can capture power even from very slow winds.
45
Teetering of Rotor
As wind speed rises with height, the axial force on
blade when upper position is significantly higher as
compared to that when it is at a lower positions.
For one-and two blade rotors, this causes cyclic
(sinusoidal) load on a rigid hub leading to fatigue.
46
47
This is greatly relieved by
providing a teeter hinge (a pivot
within the hub) that allows a
see-saw motion to take place out
of the plane of rotation (i.e.,
vertical plane).
The rotor leans backwards to
accommodate the extra force.
This also reduces blade loads near the root by
approximately 40%.
The use of a third blade has approximately the same
effect as a teeter hinge on the hub moments since the
polar symmetry of the rotor averages out the applied
sinusoidal loads.
Therefore, teetering is not required when the number
of blades is three or more.
48
Upwind and Downwind Machines
In an upwind machines, the rotor is located upwind (in front) of the tower whereas in a downwind machine, the rotor is located of (behind).
49
Both types have certain benefits.
A downwind machine allow the use of a free yaw
system (in low rating machines).
It also allows the blades to deflect away from the
tower when loaded.
However, it suffers from wind shadow effects of the
tower on the blades as they pass through the tower’s
wake, in a region of separated flow.
50
For a high-solidity tower with limited rotor overhang,
the wind speed might be effectively reduced to zero
causing a severe impulsive load of periodic nature.
This may be very dangerous as it may excite any
nature mode of the systems if that lies near a rotor
harmonics.
An upwind machine, on the other hand, produces
higher power as it eliminates the tower shadow on the
blades.
This also results in lower noise, low blade fatigue and
smoother power output.
51
Pitch Control System
The pitch of a blade is controlled by rotating it from its
root, where it connected to the hub as shown in fig.
52
The pitch controlled mechanism is provided through the
hub using a hydraulic jack in the nacelle.
The control system continuously adjusts the pitch to
obtain optimal performance.
In modern machines, pitch control is incorporated by
controlling only the outer 20% length of the blade (i.e.,
tip), keeping the remaining part of the blade as fixed.
53
Vertical Axis Wind Turbine
A wind turbine, in which axis of rotation is perpendicular
to the air stream (i.e. vertical), is known as Vertical Axis
Wind Turbine (VAWT).
Vertical axis wind turbines are in development stage and
many models are undergoing field trial.
The size of rotor and its speed depends on the rating
of the turbine.
54
The main attractions of a VAWT are:-
(1) It can accept wind from any direction, eliminating the need
of yaw control.
(2) The gearbox, generator etc. are located at the ground, thus
eliminating the heavy nacelle at the top of the tower, thus
simplifying the design and installation of the whole structure,
including the tower.
(3) The inspection and maintenance also gets easier, and
(4) It also reduces the overall cost.
55
56 Fig .1 Vertical Axis Wind (Darrieus) Turbine
57
CONSTRUCTION:-
A. MAIN COMPONENTS-
The constructional details of a vertical axis wind turbine
(Darrieus-type rotor) are shown in fig.1. The main
components of VAWT are as follows:
Tower (or Rotor Shaft):- The tower is a hollow vertical
rotor shaft, which rotates freely about the vertical axis
between the top and bottom bearings. It is installed above
a support structure . The upper part of the tower is
supported by guy ropes. The height of a large turbine is
around 100 m .
58
Blades:- It has two or three thin, curved blades shaped like
an eggbeater that minimizes the bending stress caused by
centrifugal forces. The blades have an airfoil cross section
with constant chord length. The first large (3.8 MW),
Darrieus type, Canadian machine has a rotor height as 94m
and the diameter as 65 m with a chord of 2.4 m.
Support Structure:- The support structure is provided at
the ground to support the weight of the rotor. Gearbox,
brakes, electrical switchgear and controls are housed within
this structure
59
B. TYPES OF ROTORS-
Various types of rotors for Vertical Axis Wind Turbine
(VAWT) are:
Cup type rotor
Savonious rotor
Darrieus rotor
Musgrove rotor
Evans rotor
60 Various Types of Rotors for VAWT
Cup Type Rotor
• It consists of a three or four-cup structure attached symmetrically to a vertical shaft.
• The drag force on the concave surface is more than that on the convex surface. As a result, the structure starts rotating.
• The main characteristics of this rotor is that its rotational frequency is linearly related to wind speed. Therefore, it is used as a transducer for measuring the wind speed and the apparatus is known as Cup Anemometer .
61
Savonious Rotor
• The Savonious or S- rotor consists of two half
cylinders attached to a vertical axis and facing in
opposite directions to form a two vaned rotor.
• It has high starting torque, low speed and low
efficiency.
• It can extract power even from very slow wind,
making it working most of the time.
• These are use for low power applications.
• A high starting torque particularly makes it
suitable for pumping applications.
Darrieus Rotor :-
• It is used for large scale power generation.
• Its power coefficient is better than that of an S-rotor.
• It runs at a large tip-speed ratio.
• One of the drawbacks of this rotor is that it is usually not self-starting. Movement may be initiated by using electrical generator as motor.
• As the pitch of the blade cannot change, the rotor frequency and thus the output power cannot be controlled.
• Rotor frequency increases with wind speed and power output keeps on increasing till the blades stall.
63
Musgrove Rotor
• Musgrove or H- shaped rotor consists of fixed
pitch blades, attached vertically to a horizontal
cross arm.
• Power control is achieved by controlled
folding of the blades.
• Inclining the blades to the vertical provides an
effective means of altering the blades angle of
attack and hence controlling the power output.
Evans Rotor
• The Evans rotor, also known as Gyromill is an
improvement over the H-shaped rotor.
• In this type of rotor, blades remain straight but
the blade pitch is varied cyclically to regulate
the power output.
65
Lift and Drag -Type Machines Wind turbines make use of either lift force or drag
force predominantly to cause motion and accordingly
are known as lift or drag-type machines.
• In lift devices, the ratio of lift to drag forces may be
as high as 30:1. Lift devices are more efficient and
turn faster than wind. They are able to benefit from
high-power densities available in strong winds.
• In drag devices, the wind literally pushes the blades
out the way. Drag devices are less efficient and turn
slower than wind. It produce high torque and thus are
suitable for pumping applications. They do not
benefit from high energy density available in wind. 66
Drag-based wind turbine
Lift-based Wind Turbines
Horizontal Axis Versus Vertical-
Axis Turbines
Most wind turbines used at present are of
horizontal axis type. They have been well
researched and have gone through extensive
field trial. As a result, well established
technology is available for HAWTs.
69
Advantages of VAWT
It can accept wind from any direction without adjustment which avoids the cost and complexity of a yaw-orientation system.
Gearing and generators are located at ground level, which simplifies the design of tower, the installation and subsequent inspection and maintenance, and
Also they are less costly as compared to HAWTs.
Disadvantage VAWT
• Many vertical axis machines have suffered
from fatigue arising from numerous natural
resonances in the structure.
• Rotational torque from the wind varies
periodically within each cycle, and thus
unwanted power periodicities appear at the
output.
71
72
• It normally requires guy ropes attached to the top
for support, which could limit its applications
particularly for offshore sites.
• It is noisier than HAWT.
• As wind speed increases significantly with
height, for the same tower height HAWT
captures more power than VAWT, and
• The technology is under development stage and
far less is known about them as compared to
HAWTs.
Speed Control Strategies for Wind
Turbine Various options are available for speed control of a
turbine. Small machines use simple, low-cost
methods while large machines use more sophisticated
methods incorporating pitch control along with power
electronic circuit. These methods may be grouped in
the following categories:
i. No speed control at all. Various components of the
entire system are designed to withstand extreme
speed under gusty winds.
73
74
ii. Yaw and tilt control, in which the rotor axis shifted out
of wind direction, either by yaw control or by tilting the
rotor plane with respect to normal vertical plane when
the wind exceeds the design limit.
iii. Pitch control, in which the pitch of the rotor blades
is controlled to regulate the speed.
iv. Stall control, in which the blades are shifted to a
position such that they stall when wind speed exceeds
the safe limit.
Wind Turbine Operation and Power
Versus Wind Speed Characteristics The power-speed characteristics of a wind turbine
have four separate regions:
(1) Low-speed Region(Zero to Cut-in speed) : In this
region, the turbine is kept in braked position till
minimum wind speed (about 5m/s), known as cut-in
speed becomes available. Below this speed, the
operation is not efficient.
(2) Maximum Power-coefficient Region : In this region
rotor speed is varied with wind speed so as to
operate it at constant tip-speed ratio, corresponding
to maximum power coefficient, Cpmax. 75
76
(3) Constant Power Region(Constant-turbine-speed Region):
During high-speed winds (above 12 m/s), the rotor speed is
limited to an upper permissible value based on the design
limits of the system components . In this region, the power
coefficient is lower than Cpmax.
(4) Furling speed Region (Cut-out Speed and Above) :
Beyond a certain maximum value of wind speed (around 25
m/s ), the rotor is shut down and power generation is stopped
to protect the blades, generator and other components of the
system.
Axial Thrust on Turbine, FA
• With no energy extraction, Bernoulli’s eqn. for upstream and downstream,(refer Betz model) may written as
po/ρo + gzo +uo²/2 = p2/ρ2 + gz2 +u2²/2
As z0=z2 and variation in air density is negligible compares to other terms, considering ρ as average air density, the static pressure difference across the turbine may be written as
∆p=po-p2 =(uo²-u2²)ρ/2
• The maximum value of static pressure difference occurs when u2 approaches zero. Thus,
∆pmax= ρuo² and maximum thrust on disk is
Fmax= A1ρuo²/2 (13)
This axial thrust must me equal to loss of momentum. Therefore,
FA = m̊(uo-u2)
Using eqn 1, 7 & 8 we can write
FA=4a(1-a)(A1)ρuo²/2 (14)
or FA=CFFAmax (15)
where CF = 4a(1-a) (16)
• Maximum axial thrust occurs when CF=1, which is achieved when a=0.5, equivalent to u2 =0. Maximum power extraction by the Betz criterion occurs when a=1/3, corresponding to CF=8/9.
Torque Developed by the Turbine, T
• The maximum conceivable torque TM on an ideal rotor would occur if maximum circumferential force acts at the tip of the blade with radius R. Thus,
TM=FcirmaxR (17)
TM=PoR/uo (18)
Now, if λ is the tip speed then TM can be written as
TM=Poλ/ω (19)
Thus, the shaft torque, Tsh is given as
Tsh=CTTM
• As the product of shaft torque and angular speed equals power developed by the turbine,
Tshω=PT
or CTTMω=CPPo
Substituting for TM from eqn 19, we have,
CTPoλ=CPPo
or CT=CP/λ (20)
Both CT & CP are functions of λ. As per Betz criterion, the maximum value of CP can be 0.593, therefore,
CTmax= CPmax/λ (21)
Thus, machines with higher speeds have low value of CTmax or low starting torque.
References
• B. H. Khan, “ Non conventional Energy Resources”, 3rd ed, Tata Mc graw Hill publisher.