Environmental Engineering Reference
In-Depth Information
5.2.2 Optimization for maximum energy yield
An optimization is given by the condition that AEP will be maximum, i.e.:
AEP
Max
(8 )
A rotor designer must fi nd the optimal power curve P ( V ) together with WT
operation modes. An optimal rotor geometry which comprises of chord and twist
distributions and aerofoil sections is found in combination with operation modes;
cut-in, cut-out and rated wind speed in principle. Thus an optimal rotor design is
site-dependent. Further, since every reliable operation mode depends on power/
speed control methods, conceptual design of control methods are also needed at
the initial stage.
5.2.3 One-point optimal rotor design
Simplest optimization of rotor design is “One-point design method”, in which an
optimal rotor geometry is determined for one operation point: one combination of
a design wind speed V D and a design rotor speed
D by using BEM theory [2].
The optimization is given by the following condition for V = V D with selected rotor
speed
Ω
Ω
D :
C
Max. At every axial position of rotor blade
(9 )
P
Algebraic solution determines the chord and twist distributions along its axis of
the blade. However, it must be noticed that “One-point design method” does not
always give the maximum AEP, because a maximum AEP is obtained under the best
combination of decided WT's operation mode and wind characteristics at the site.
The question is how to decide design wind speed V D .
The simplest design by BEM theory is conducted under the following
assumptions:
Low Reynolds number effect is negligible
Power curve is a function of tip speed ratio
l only.
Then eqn (6) is expressed as:
V
V
1
R
out
3
3
AEP
=
r
Af VVC
(
)
( ) d
l
VVC
+
(
l
)
f VV
(
) d
(10 )
P
R
P
R
2
V
V
in
R
where V R is rated wind speed and
R
V
Ω
R
l
=
(11 )
R
R
Max(AEP) is derived as follows:
In case of variable-speed operation WT, an optimal l opt
l R is defi ned and the
optimal value can be possibly in the manner:
ll
for VVV
(12 )
opt
in
R
 
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