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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

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