Environmental Engineering Reference
In-Depth Information
pre-manufacturing analysis, from finite element or CAD software. Alternatively,
the analysis in Sect. 6.4 for the moment of inertia can be easily modified to give
m B . For the current timber blades with density 550 kg/m 3 , m B = 0.4 kg. The blade
centre of mass, R cog , can be determined in similar fashion, taking note that the hub
end
of
the
blade
is
not
likely
to
correspond
to
zero
radius.
In
this
case
R cog = 0.379 m. Thus
DF zB ¼ 2 0 : 4 0 : 379 73 : 30 2 ¼ 1629 : 23 N
ð 9 : 39 Þ
From ( 9.5 ) and ( 9.6 ) respectively:
DM xB ¼ 11 : 32 = 3 þ 2 0 : 4 9 : 81 0 : 379 ¼ 6 : 75 Nm
ð 9 : 40 Þ
and
DM yB ¼ 7 : 11 11 : 32 = 3 ¼ 25 : 55 Nm
ð 9 : 41 Þ
Equation 9.7 gives the shaft load as:
DF x shaft ¼ 3 7 : 11 11 : 32
2 0 : 97
¼ 118 : 55 N
ð 9 : 42 Þ
From ( 9.8 ), using e r = 0.005 9 0.97 = 0.0049 m, and a measured rotor mass
m r = 3.98 kg,
DM x shaft ¼ 11 : 32 þ 2 3 : 98 9 : 81 0 : 0049 ¼ 11 : 70 Nm
ð 9 : 43 Þ
so the assumed eccentricity has little effect in this case. The other shaft moment is
given by ( 9.9 ) using the measured (or designed) length from the rotor to the first
bearing, L rb = 0.026 m,
DM shaft ¼ 2 3 : 98 9 : 81 0 : 026 þ 0 : 97
6
118 : 55 ¼ 21 : 20 Nm
ð 9 : 44 Þ
9.4.2 Loads for Case B: Yawing
The blade root bending moment depends on the additional parameters
L rt = 0.218 m, the distance from the rotor to the yaw axis, and J B , the blade
moment of inertia. From the CAD model of the blade, J B = 0.0633 kg m 2 and this
value was confirmed by tests described by Wright [ 5 ]. 34
Note also that J B can be
J B m B R cog ¼ 0 : 4 0 : 379 2 ¼ 0 : 0575 kgm 2
approximated
as
for
the
present
rotor. From ( 9.10 ):
34 Note that this value of J for wooden blades is considerable less than for the composite blades
of the same shape considered in Chap. 6 .
 
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