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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