Note : Les descriptions sont présentées dans la langue officielle dans laquelle elles ont été soumises.
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1 ~ FIELD OF THE INVENTION
2 This invention relates to a horizontal axis wind turbine
3 assembly.
4 SUMMARY OF THE INVENTION
The present applicant has developed a wind turbine which
6 comprises the following components in combination:
7 1. A head assembly, which is basically a frame, mountable
8 on a tower so that it may extend in a horizontal plane
9 and may pivot about a vertical axis passing through theframe, said pivot axis being termed the yaw axis;
1l 2. A rotor assembly which comprises a central hub, which
12 carries a plurality of rotor blades of delta wing
13 configuration, said hub being attached to an output
14 shaft, said rotor blades extending generally radially
from the hub and being angled, so as to rotate the
16 hub when contacted by an air flow;
17 3. A tail assembly which comprises a frame carrying one or18 more upstanding tails at the rear end thereof, said tail
19 assembly being pivotally mounted at its front end to the
rear end oP the head assembly by suitable means, for
21 pivotiny about a vertical axis~ whereby the tail assembly
22 is operative to track the wind;
23 4. The horizontal central axis of the rotor assembly being
24 offset from the plane of the yaw axis, whereby wind
acting upon the rotor blades will exert a moment causlng
26 the head assembly to want to pivot about the yaw axis,
27 5. Said head and tail assemblies being provided with stops,
28 which contact when the former reaches each of the fully
29 operatiye and fully feathered positions, to preYent the
head assembly from pivoting further; and
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1 ~. Means, connected with the head assembly, for applying
2 a counterbalancing counter-rotational moment, which
3 counter-rotational moment resists the pivoting move-
4 ment caused by the wind moment, so that the head
assembly will only pivot from the fully operative
6 position, transverse to the wind direction, to a
7 feathered position, edgewise to the wind, when the
8 wind moment exceeds the counterbalancing moment.
9 Now, when applicant tested this assembly, it was found that
the head assembly would pivot back and forth with unexpected velocity
11 between the two extreme positions of being fully operative and being
12 fully feathered. Gyroscopic moments~ which would stress the rotor shaft,
13 were developed and the contact between the head and tail assemblies was
14 violent when their stops met.
So applicant completed the combination by pivotally mounting
16 damping means between the ta;l and head assemblies, to resist the p;voting
17 movement of the latter and slow such movement.
18 In a preferred form, the damping means comprises a double-
19 acting cylinder. A reservoir containér is mounted on the turbine assembly,to supply and exhaust operating oil or the 11ke to and from the cylinder,
21 via connecting hydraulic fluid lines. Means, such as restrictive orifices,
22 are provided in the hydraulic fluid lines, to control khe rate of fluid
23 movement therethrough, so that the rate of pivoting of the head assembly
2~ as it moves from the operati~e to the Feathered positions ~s relatively
fast and when moving in the opposite direction it is relati~ely slow.
26 The reason for this is that it is desirable that the machine should furl
27 more easily than it should unfurl. This prevents it, under stormy gusting
; 28 conditions, from persistently swinging back into the operational configura-
~ 29 tion between gusts only, to be re-furled again.
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1 By choosing appropriate orifices, the rate of damp-ing can
2 be made substantially proportional to the square of the velocity of
3 movement of the cylinder piston, which corresponds with the velocity
4 of furling. The signiFicance of this is that damping obtained in this
way is highly non-linear, i.e. very slow movements can be made with
6 negligible damping force and yet fast movements are very severly
7 damped.
8 ~ESC~IPTION OF THE DRAWI _
9 Figure 1 is a top plan schematic view of the wind turbine
assembly in the operative position - the direction oF the wind is indicated
11 by the arrow;
12 Figure 2 is a side schematic view oF the assembly, showing
3 it mounted on the upper end of a tower and in the operative position - the
14 direction ~f the wilnd i;s ilndicated by the arrow;
Figure 3 is a top plan schematic view similar to Figure 1,
16 except that the head assembly is in the feathered position - the wind
17 d;rection is ind;cated by the arrow; and
18 Figure 4 is a side schematic view showing the damping
19 assembly, partly in section.
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1 DESCRIPTION OF THE PREFERRED EMBODIMENT
2 The wind turbine assembly 1 comprises a head assembly 2,
3 which is pivotally mounted on the upper end of a tower 3. The head
4 assembly 2 thus can pivot about a vertical axis 4 termed the yaw axis.
A rotor assembly 5 is rotatably secured to the front end
6 of the head assembly 2. The rotor assembly 5 comprises a central hub 6
7 and a number of blades 7, of delta wing configuration, extending radially
8 from the hub. The hub rotates a turbine output shaft 8, the details of
g which form no part of the present invention.
It is to be noted that the central horizontal axis 9 of
11 the rotor assembly 5 is offset laterally from the yaw axis 4. Thus the
12 wind acting on the blades 7 will exert a moment which seeks to turn the
13 head assembly 2 about the yaw axis 4 to the feathered position il-
14 lustrated in Figure 3.
A tail assembly 10 is pivotally mounted on the rear end of
16 the head assembly 2 by a vertically extending pin assembly 11. The tail
17 assembly 10 has a pair of upstanding parallel tails 12 which are slightly
18 slanted relative.to the axis 9 of the rotor assembly 5.
19 Stops 13 and 14 are provided on the head assembly 2 and tail
assembly 10, for limiting the ex-tent of rotation of thè.head assembly 2.
21 There is provided means for applying a counterbalancing
22 counter-rotational moment to the hea~l assembly 2, to resist the wind moment
23 up to a pre-determined value. Such means may comprise a counterweight 15
24 suspended by a cable 16 clamped to a sheave l7 which, in turn, ~s secured
to the head assembly 2. For the wind to pivot the head assembly 5 about
26 the yaw axis 4, it must exert sufficient moment to commence the head
27 assembly 5 turning while simultaneously lifting the counterweight 15.
28 By virtue of the arrangement which has been described, the
29 following results arise:
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1 1. The head assembly 2 only begins to pivot when the wind
2 velocity is great enough to.overcome the maximum
3 counterbalancing moment exerted by the counterweight
4 15;
2. The tails 12 cause the tail assembly 10 to track the
6 wind; and
7 3. The counterweight 13 functions to maintain the tail
8 assembly 10 and the head assembly 2 as a rigid unit
9 until the wind moment reaches the threshold at which
the head assembly begins to pivot - thus the head
1l assembly tracks the wind together with the tail assembly
12 until the wind moment reaches said threshold.
13 A double-acting, standard, hydraulic cylinder 18 is
14 pivotally connected between the head and tail assemblies 2~ 10. More
particularly, a first bracket 19 extends from the side of the front end
16 of the tail assembly 10 and a second bracket 20 extends from the side
17 of the rear end of the head assembly 2. 'The'cylinder body is con-
18 nected by a pin 21 with the bracket `79 and the cy'l7nder piston rod 22 is19 connected by a pin 23 with the bracket'20. For the head assembly 2
to pivot to the feathered pos7t7qn1 7t has to extend the cylinder 18
21 and cause the piston 24' to expel ~il from the cylinder chamber 26; for
22 it to pivot ~o the operational pos7tiqn. it has to compress the çYlinder
23 18 by causing the piston 24 to expel o71 From the cylinder chamber ?5'.
24 Oil expelled from chamber 25'passes through return line 27 to reservoir
container 28. Passage of oil through this.line 27 is controlled by
26 restrictive orifice 29. '071 expelled from chamber 26 passes through
27 return line 30 to the reservoir container 28. Passage of oil through
28 line 30 is controlled by restrictive orifice 31.
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1 The orifice 31 is larger than orifice 29 ; thus the head
2 assembly will move relatively rapidly (but not freely without resistance)3 to the feathered position and more slowly to the operative positlon.
4 Operating oil is fed by gravity to the chambers 25 and 26
by supply line 32 and its branches 32a, 32b, the latter being controlled
6 by check valves 33.
