Development of two-bladed offshore wind turbine - Condor wind ...
Development of two-bladed offshore wind turbine - Condor wind ...
Development of two-bladed offshore wind turbine - Condor wind ...
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Vol. 24, No. 2<br />
Spring 2011<br />
ISSN 0903-5648<br />
Editor<br />
Bill Canter<br />
Assistant Editor<br />
Jack Jackson<br />
Contributing Editors<br />
Eize de Vries (the Netherlands)<br />
Birger T. Madsen (Denmark)<br />
David Milborrow (UK)<br />
Drew Robb (USA)<br />
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<strong>Development</strong> <strong>of</strong> <strong>two</strong>-<strong>bladed</strong><br />
<strong>of</strong>fshore <strong>wind</strong> <strong>turbine</strong><br />
by eize d e vries<br />
<strong>Condor</strong> Wind Energy, based in the UK,<br />
is at an advanced stage <strong>of</strong> developing<br />
a <strong>two</strong>-<strong>bladed</strong>, 5 MW <strong>of</strong>fshore <strong>wind</strong><br />
<strong>turbine</strong> aimed at substantially driving<br />
down costs <strong>of</strong> energy compared to current<br />
three-<strong>bladed</strong> designs.<br />
Conceptually, the <strong>Condor</strong> 5 is an <strong>of</strong>fshore<br />
dedicated, medium-speed, geared<br />
<strong>wind</strong> <strong>turbine</strong>. But, despite several conventional<br />
drive system elements, the<br />
overall design concept radically differs<br />
from conventional three-<strong>bladed</strong>,<br />
geared as well as direct drive <strong>of</strong>fshore<br />
equivalents.<br />
The <strong>Condor</strong> 5 builds upon an initial<br />
1.5 MW, <strong>two</strong>-<strong>bladed</strong>, variable speed<br />
Gamma 60 research <strong>turbine</strong>, whose<br />
product development originates from<br />
the late 1980s in Italy. A link between the<br />
<strong>two</strong> <strong>turbine</strong> developments is via <strong>Condor</strong>’s<br />
co-founder and managing director,<br />
Martin Ja kub owski, beginning back<br />
in 2004 when he founded floating <strong>wind</strong><br />
<strong>turbine</strong> system developer Blue H.<br />
Netherlands headquartered, three<br />
years later Blue H acquired the exclusive<br />
worldwide <strong>of</strong>fshore application rights to<br />
the Gamma 60 technology from US <strong>wind</strong><br />
<strong>turbine</strong> and helicopter pioneer Glidden<br />
Doman, a <strong>Condor</strong> co-founder. A noted<br />
pioneer, patent holder and aeronautics<br />
engineer, Doman earlier served with<br />
NASA exploring structural dynamics<br />
<strong>of</strong> very large <strong>wind</strong> <strong>turbine</strong>s. Doman was<br />
also Boeing’s Mod 2 proposal manager<br />
and system design manager at Hamilton<br />
Standard’s 4 MW, WTS-4 <strong>turbine</strong><br />
program.<br />
Radical design<br />
An artist’s impression (next page) <strong>of</strong> the<br />
<strong>Condor</strong> 5’s nacelle shows a distinct circular<br />
helicopter-hoisting platform positioned<br />
on top <strong>of</strong> the center <strong>of</strong> the nacelle.<br />
In This Issue<br />
The design arrangement aims at allowing<br />
easy delivery <strong>of</strong> service personnel—<br />
after the <strong>turbine</strong> has been brought to a<br />
stationary mode with both rotor blades<br />
in horizontal position. From a structural<br />
point <strong>of</strong> view, a centrally positioned<br />
hoisting-platform on top is likely easier<br />
to integrate with the nacelle structure as<br />
compared to a common rear-mounted<br />
platform arrangement.<br />
Human error<br />
With European Commission financial<br />
support, Italy’s AERITALIA together<br />
with industrial partners designed the<br />
Gamma 60 prototype, which was commissioned<br />
during May 1991 at Alta<br />
Nurra, Sardinia, Italy. According to<br />
Jakubowski, the <strong>turbine</strong> functioned well<br />
for about four years, but due to human<br />
error during a 1995 storm it was damaged.<br />
It was subsequently repaired and<br />
put back into operation up until 1997<br />
when the program was terminated.<br />
Initially Blue H’s aim was to develop<br />
in-house and up-scale the Gamma 60 together<br />
with its floating foundation technology<br />
in a parallel track. Turbine size<br />
was envisaged to grow from 1.5 MW<br />
to 2.2 MW and then again to about 3.5<br />
MW, together with increments in corresponding<br />
rotor sizes. However, in 2010<br />
Jakubowski and his Blue H partners decided<br />
to functionally split the <strong>two</strong> business<br />
activities and founded a separate<br />
company for <strong>of</strong>fshore <strong>turbine</strong> development.<br />
“The UK Energy Technologies<br />
Institute, a public-private partnership<br />
between the UK government and six<br />
large industries, responded positively to<br />
our <strong>of</strong>fshore <strong>turbine</strong> development project<br />
proposal. But as a precondition they<br />
demanded a power rating increase to at<br />
least 5 MW, which resulted in the cur-<br />
<strong>Development</strong> <strong>of</strong> <strong>two</strong>-<strong>bladed</strong> <strong>of</strong>fshore <strong>wind</strong> <strong>turbine</strong> 1<br />
Wind technology: What’s working and what’s not 4<br />
Improved <strong>wind</strong> station pr<strong>of</strong>its through excellence in O&M 5<br />
Wind <strong>turbine</strong> data summary tables 7<br />
Wind <strong>turbine</strong> performance summary 7<br />
Production from individual <strong>wind</strong> plant 9<br />
International <strong>wind</strong> energy directory 95
ent <strong>Condor</strong> <strong>of</strong>fshore <strong>turbine</strong> size,” says<br />
Jakubowski.<br />
Italian nuclear mechanical engineer<br />
Silvestro Caruso was from the start involved<br />
and a driving force behind the<br />
Gamma 60’s product development, building,<br />
testing and optimizing. More than a<br />
decade later he became engineering director<br />
for the <strong>Condor</strong> 5 development team.<br />
Most other <strong>Condor</strong> development team<br />
members are also Italian engineers who<br />
had worked in different technical capacities<br />
on the Gamma 60 project. Product development<br />
activities are conducted from<br />
<strong>of</strong>fices and other facilities in the port <strong>of</strong><br />
Genoa, Italy.<br />
Issues<br />
Onshore, <strong>two</strong>-<strong>bladed</strong> <strong>wind</strong> <strong>turbine</strong>s during<br />
the past thirty years have always<br />
played a minority role in the <strong>wind</strong> industry<br />
for a number <strong>of</strong> reasons, but particularly<br />
due to aesthetic acceptance and<br />
aerodynamic noise reasons. The latter due<br />
to the fact that <strong>two</strong>-<strong>bladed</strong> rotors must<br />
rotate substantially faster compared to<br />
three-<strong>bladed</strong> rotors with the same diameter<br />
unless very wide and, therefore, heavy<br />
blades are being applied. But for <strong>of</strong>fshore<br />
application aerodynamic noise in most<br />
situations is hardly an issue.<br />
One advantage <strong>of</strong> <strong>of</strong>fshore applications<br />
is that a nacelle with a <strong>two</strong>-<strong>bladed</strong> rotor<br />
combinations can be transported fully<br />
preassembled and pre-tested on a ship’s<br />
deck to a <strong>wind</strong> farm construction site. After<br />
arrival, the assemblies can be hoisted<br />
on top <strong>of</strong> a installed tower in a single, time-<br />
and cost-saving operation.<br />
The fact that <strong>two</strong>-<strong>bladed</strong> <strong>turbine</strong>s are<br />
by nature aerodynamically unbalanced<br />
provides a major design challenge. A<br />
well-known solution is to eliminate or at<br />
least minimize the high structural loads<br />
resulting from bending moments during<br />
operation by attaching the rotor blades to<br />
a flexible structure with limited pivoting<br />
capability. This is called a teeter hub. However,<br />
in the past rapid wear <strong>of</strong> the pivoting<br />
mechanism and resulting vibrations were<br />
reasons for their infamous premature failure.<br />
These and other operational lifetime<br />
issues have hampered commercial application<br />
opportunities <strong>of</strong> <strong>two</strong>-<strong>bladed</strong> <strong>turbine</strong>s,<br />
including teeter hub concepts.<br />
Teeter hub technology is, in practice,<br />
only suitable for <strong>two</strong>-<strong>bladed</strong> rotors according<br />
experts. Applying the technology<br />
to three-<strong>bladed</strong> <strong>wind</strong> <strong>turbine</strong>s would add<br />
substantially to system complexity, resulting<br />
in higher system—and likely installation—upkeep<br />
costs.<br />
Limited movement<br />
Like the Gamma 60 <strong>turbine</strong>, the <strong>Condor</strong><br />
5 features a teeter hinge with both blades<br />
being rigidly connected to a shared central<br />
rotor hub. This assembly in turn is<br />
attached to the main shaft by means <strong>of</strong> a<br />
shaft with <strong>two</strong> double elastomeric-type<br />
teeter elements. These patent pending<br />
hinges allow limited rotor teeter angle<br />
movement during operation <strong>of</strong> about <strong>two</strong><br />
degrees—positive and negative—relative<br />
to the rotor’s central position during rotation.<br />
The <strong>Condor</strong> 5’s rotor diameter is 120<br />
meters, which is an average size in the<br />
5 MW <strong>of</strong>fshore <strong>turbine</strong> model segment<br />
which typically varies between 115–128<br />
meters.<br />
What is really striking about <strong>Condor</strong>’s<br />
technical specifications is a 20.2 rpm rated<br />
rotor running speed, which corresponds<br />
to a maximum rotor blade tip speed <strong>of</strong><br />
127 m/s. By comparison, most 5 – 6 MW<br />
class <strong>of</strong>fshore <strong>turbine</strong>s have a rated tip<br />
speed <strong>of</strong> about 84 – 90 m/s. One known<br />
exception is the new 5 MW, XEMC Dar-<br />
WinD <strong>of</strong>fshore <strong>turbine</strong> with its 115-meter<br />
rotor diameter, which features a 108 m/s<br />
rated tip speed.<br />
Premature rotor blade airfoil surface<br />
erosion and high centrifugal forces are<br />
<strong>of</strong>ten named as technical challenges for<br />
rotors turning at very high tip speeds. Silvestro<br />
Caruso is said to be aware <strong>of</strong> these<br />
arguments but in his own view explains:<br />
“Erosion protection is manageable, and<br />
we plan to apply special anti-abrasive<br />
coatings to erosion sensitive rotor blade<br />
surface areas. Most critical with the <strong>Condor</strong><br />
design are extreme loads; but fatiguerelated<br />
loads and centrifugal forces are<br />
not an issue.”<br />
A added benefit <strong>of</strong> a high rotor speed<br />
for a given power rating is that the matching<br />
rotor and main shaft torque is relatively<br />
low. Silvestro Caruso claims that<br />
the <strong>Condor</strong> 5’s main shaft torque is about<br />
60% <strong>of</strong> the value for a 5 MW, three-<strong>bladed</strong><br />
rigid rotor.<br />
Active yaw-control<br />
Another unusual Gamma 60 feature that<br />
has re-emerged in the <strong>Condor</strong> 5 is active<br />
yaw-control, a system that fulfills <strong>two</strong> distinct<br />
but separate control functions:<br />
Artist’s concept <strong>of</strong> the <strong>Condor</strong> 5’s nacelle shows a distinct circular helicopter-hoisting platform positioned<br />
on top <strong>of</strong> the center <strong>of</strong> the nacelle in line with the tower.<br />
Apart from <strong>Condor</strong>, at<br />
least <strong>two</strong> other companies<br />
are developing <strong>of</strong>fshore<br />
<strong>turbine</strong>s based upon a<br />
<strong>two</strong>-<strong>bladed</strong> rotor concept.<br />
One is 2-B Energy <strong>of</strong> the<br />
Netherlands, and the second<br />
is aerodyn company<br />
SCD <strong>of</strong> Germany. Both<br />
companies are developing<br />
or have developed a<br />
Other <strong>two</strong>-bladers<br />
<strong>two</strong>-<strong>bladed</strong>, down<strong>wind</strong><br />
<strong>turbine</strong> <strong>of</strong>, respectively,<br />
6 MW and 6.5 MW. The<br />
latter SCD technology<br />
has been licensed to Ming<br />
Yang <strong>of</strong> China.<br />
The only likely mature<br />
and commercially viable<br />
<strong>two</strong>-<strong>bladed</strong> onshore<br />
<strong>turbine</strong>s today are <strong>two</strong><br />
models originally kW-<br />
1) to keep the rotor facing the <strong>wind</strong><br />
below rated speed;<br />
2) power output control above rated<br />
<strong>wind</strong> speed by adjusting the rotor angle<br />
relative to the <strong>wind</strong> direction as a function<br />
<strong>of</strong> the <strong>wind</strong> speed.<br />
The functional basis <strong>of</strong> active yaw-control<br />
is that a yaw motor activated system<br />
gradually turns the rotor out <strong>of</strong> the <strong>wind</strong><br />
when <strong>wind</strong> speed increases. A full rotor<br />
circle that initially faces the <strong>wind</strong> perpendicular<br />
to the prevailing direction at low<br />
and medium <strong>wind</strong> speeds, thereby gradu-<br />
size developed by former<br />
Lagerwey <strong>of</strong> the Netherlands<br />
in the 1980s and<br />
early 1990s. These original<br />
models <strong>of</strong> 80 kW and<br />
250 kW each have been<br />
continuously upgraded<br />
and are now being manufactured<br />
by the current<br />
Dutch owner and <strong>wind</strong><br />
<strong>turbine</strong> supplier, WES.<br />
2 WindStats Report • Spring 2011 • Vol. 24, No. 2
ally changes into an eclipse, seen from the<br />
<strong>wind</strong> direction. There are <strong>two</strong> components<br />
to this: the “normal” to the rotor disk,<br />
which gives “active” power and the cross<br />
flow, which causes flapping moments in<br />
the higher <strong>wind</strong> speed range. The resulting<br />
reduction <strong>of</strong> aerodynamic efficiency<br />
is not an issue, because at higher <strong>wind</strong><br />
speeds the available power is higher than<br />
what the <strong>turbine</strong> can actually extract. The<br />
reason being that the <strong>wind</strong>’s inclined angle<br />
<strong>of</strong> blade airfoil attack from the prevailing<br />
<strong>wind</strong> direction becomes less favorable and<br />
thus less effective.<br />
The inclined rotor actively turns in<br />
the opposite direction again once the<br />
<strong>wind</strong> calms down. Finally, during stationary<br />
safe-mode position, the <strong>wind</strong> blows<br />
against the smallest projected rotor plane<br />
parallel to the prevailing <strong>wind</strong> direction.<br />
In parked condition the <strong>Condor</strong> 5 can<br />
survive up to 70 m/s <strong>wind</strong> speeds, whereby<br />
the blades in horizontal position are<br />
being kept aligned to the prevailing <strong>wind</strong><br />
direction. Under these conditions the mechanical<br />
brake is closed and the rotor is<br />
mechanically locked as well.<br />
Yaw moments<br />
While elaborating further on active yawcontrol<br />
technology features and test results,<br />
Silvestro Caruso says “Analysis and<br />
tests clearly showed that nacelle yaw moments<br />
introduced by the <strong>wind</strong> <strong>of</strong> a <strong>two</strong><strong>bladed</strong>,<br />
teeter rotor are only about 15%<br />
compared to these values for an equivalent<br />
three-<strong>bladed</strong> rigid rotor. This value<br />
is about 20% for both the hub pitch and<br />
yaw moments.”<br />
<strong>Condor</strong> 5’s maximum yaw torque during<br />
yaw system acceleration and maximum<br />
yaw speeds in the range <strong>of</strong> 10 degrees<br />
per second is well below 2500 kNm,<br />
with a further reduction expected. More<br />
important for a <strong>turbine</strong> <strong>of</strong> this size, only<br />
three yaw motors are required; but only<br />
<strong>two</strong> <strong>of</strong> which are needed at a time. The<br />
third motor provides system redundancy,<br />
he added.<br />
Active yaw-control as applied in largescale<br />
<strong>Condor</strong> <strong>wind</strong> <strong>turbine</strong>s heavily contrasts<br />
with today’s state-<strong>of</strong>-the-art pitch<br />
controlled <strong>wind</strong> <strong>turbine</strong>s. With the latter<br />
technology, the full rotor circle continues<br />
facing the <strong>wind</strong> and the turn-able blade’s<br />
pitch angle is continuously varied for controlling<br />
power output.<br />
Yaw-control as an output regulating<br />
principle bears some resemblance to mechanical<br />
control systems known as “folding<br />
tail” output control technology, commonly<br />
applied in small <strong>wind</strong> <strong>turbine</strong>s up<br />
to about 10 – 12 kW power-ratings. The<br />
main difference is that a majority <strong>of</strong> these<br />
small size <strong>turbine</strong>s are free yawing.<br />
Regarding the choice made between<br />
an up<strong>wind</strong> and down<strong>wind</strong> rotor concept,<br />
Silvestro Caruso says “The active yawcontrol<br />
principle will work both up<strong>wind</strong><br />
and down<strong>wind</strong>, but during Gamma 60<br />
testing we found that an up<strong>wind</strong> rotor<br />
with active yawing is aerodynamically<br />
more stable. A second added benefit is<br />
that no stall effect occurs. We therefore decided<br />
for up<strong>wind</strong> in a combination with a<br />
s<strong>of</strong>t hydraulically dampened active yawcontrol<br />
system.”<br />
Design drivers<br />
Considering the typically much stronger<br />
<strong>wind</strong>s and therefore higher loads endured<br />
by large <strong>of</strong>fshore <strong>wind</strong> <strong>turbine</strong>s compared<br />
to onshore equivalents <strong>of</strong> similar size, Silvestro<br />
Caruso points at three main <strong>Condor</strong><br />
design drivers:<br />
1) to minimize peak and cyclic aerodynamic<br />
loads before they can impact<br />
critical drive system and other main components;<br />
2) protecting critical components from<br />
harmful forces and moments;<br />
3) incorporating a built-in capability<br />
for reducing the effects <strong>of</strong> extreme aerodynamic<br />
hurricane-type loads on the rotor.<br />
The <strong>Condor</strong> 5 has been designed for<br />
IEC 5 class <strong>wind</strong> sites with up to 12 – 13<br />
m/s and perhaps even higher mean <strong>wind</strong><br />
speeds and hurricane conditions. These<br />
high <strong>wind</strong> speed plus hurricane risk conditions<br />
do occur at potential <strong>of</strong>fshore sites<br />
in Chinese waters, said Silvestro Caruso.<br />
The “conventional” non-integrated<br />
<strong>Condor</strong> geared drive system comprises a<br />
main shaft supported by <strong>two</strong> main bearings,<br />
a so-called “<strong>two</strong> and a half-stage”<br />
planetary gearbox with i = 1:35 step-up ra-<br />
tio, an intermediate shaft and generator.<br />
The <strong>two</strong> main bearings have been<br />
purpose-designed with horizontally split<br />
housings with a removable upper section<br />
for easy assembly or disassembly and<br />
component exchange.<br />
Great effort has also been taken to protect<br />
the custom-designed and modular-<br />
The <strong>Condor</strong> 5 features a teeter hinge with both blades being rigidly connected to a shared central rotor hub. This<br />
assembly is attached to the main shaft by means <strong>of</strong> a shaft with <strong>two</strong> double elastomeric-type teeter elements.<br />
designed gearbox from unwanted rotor<br />
introduced loads and moments entering.<br />
The main shaft and gearbox are connected<br />
by means <strong>of</strong> gear coupling, which is integrated<br />
within the gearbox’s low-speed input<br />
side. A function <strong>of</strong> a gear coupling is to<br />
absorb slight shaft misalignment, and this<br />
serves to protect the gearbox against unwanted<br />
rotor bending moments entering<br />
bearings and gear systems. A flexible joint<br />
at the high-speed side serves as a second<br />
additional gearbox protection measure.<br />
Separate removal<br />
The gearbox will be manufactured by an<br />
experienced German gearbox producer<br />
and enables full on-board disassembly<br />
and separate removal <strong>of</strong> the second medium-speed<br />
gear stage. In addition, the<br />
first gear stage upper housing cover can<br />
be removed for major inspection and/or<br />
repair or retr<strong>of</strong>it actions if necessary. These<br />
combined gearbox design features allow<br />
even major repairs to be conducted inside<br />
the nacelle without having to replace the<br />
entire unit. Such operations are known to<br />
be very costly and time-consuming and<br />
typically necessitate the employment <strong>of</strong><br />
a jack-up crane vessel.<br />
The 3.3 kV, 8–pole, induction generator<br />
(4-poles is a semi <strong>wind</strong> industry standard)<br />
comes with an air-air heat exchanger<br />
and full power electronic converter. The<br />
WindStats Report • Spring 2011 • Vol. 24, No. 2 3<br />
development o f t w o-<strong>bladed</strong> o f f s h o r e w i n d t u r b i n e
ated speed is 700 rpm. “For the generator<br />
and converter development we cooperate<br />
closely with Ansaldo <strong>of</strong> Italy, which is a<br />
specialist technology developer and supplier<br />
<strong>of</strong> both key electrical—power electronic<br />
components. The combination with<br />
a state-<strong>of</strong>-the-art, full power, electronic<br />
converter ensures smooth grid connection<br />
and disconnection and also <strong>of</strong>fers excellent<br />
grid quality behavior,” says Caruso.<br />
All non-integrated main drive system<br />
components are attached to a stiffly-welded,<br />
fabricated steel bedplate or main chassis<br />
that comes in a single piece.<br />
Saftey<br />
Regarding operational safety, the <strong>Condor</strong><br />
5 will be equipped with <strong>two</strong> indepen-<br />
<strong>Condor</strong> 5 main specifications<br />
Rated power 5 MW<br />
Rotor diameter 120 m<br />
Rotor rated speed 20.2 rpm<br />
No. <strong>of</strong> blades 2<br />
Cut-in <strong>wind</strong> speed 3.4 m/s<br />
Cut-out <strong>wind</strong> speed 25 m/s<br />
Rated <strong>wind</strong> speed 12 m/s<br />
Survival <strong>wind</strong> speed 70 m/s<br />
(IEC 61400 Class I)<br />
Top head mass 259 tonnes, nacelle<br />
+ rotor (target 239T)<br />
Source: <strong>Condor</strong> Wind Energy, 4-2011<br />
dent braking systems, a “s<strong>of</strong>t” mechanical<br />
brake, located on the low speed main<br />
shaft near the rear main bearing and the<br />
active yaw-control. In case <strong>of</strong> yaw failure,<br />
for instance in a slewing bearing, the <strong>turbine</strong><br />
can still be brought to a full stop with<br />
the mechanical brake.<br />
The <strong>Condor</strong> 5 prototype is planned to<br />
be operating in 2013 and should be fully<br />
certified by Germanischer Lloyd in 2015.<br />
Jakubowski believes that a combination 5<br />
MW size and <strong>Condor</strong> <strong>two</strong>-<strong>bladed</strong> technology<br />
is well suited for future large-scale series<br />
production. He is also convinced that<br />
the <strong>Condor</strong> 5 will <strong>of</strong>fer a cost-effective, optimized<br />
solution for many <strong>of</strong> the world’s<br />
future <strong>of</strong>fshore <strong>wind</strong> projects.<br />
The prototype is partly financed by the<br />
GEOMA project, which in turn is funded<br />
by the Italian Ministry for Economic <strong>Development</strong>.<br />
4 WindStats Report • Spring 2011 • Vol. 24, No. 2