CASE STUDY
21REINFORCEDplastics 0034-3617/13 ©2013 Elsevier Ltd. All rights reserved JANUARY/FEBRUARY 2013
NOVA is a two-year renewable
energy feasibility project, supported
by the UK Energy Technologies
Institute (ETI) and the Engineering & Science
Research Council (EPSRC), with fi nancial
support from the European Regional
Development Fund (ERDF). The project aims
to investigate the aff ordability and feasibility
of manufacturing a VAWTS of this design
and scale.
The 50 kW prototype was manufactured at
Cranfi eld University’s Composites Centre,
with support in its design and manufac-
ture provided by key materials suppliers.
These included Scott Bader, whose Crystic®
Crestomer® 1152PA urethane acrylate
structural adhesive has been specifi ed for
bonding the various carbon fi bre and glass
fi bre epoxy composite parts which make up
the two 10 m by 1.9 m rotor sails.
To be a viable, the planned massive
scale up in off shore wind turbine
manufacture will require the rotor blades
to sustain at least 20 years’ service without
maintenance. As such, the structural design
and selection of suitable high quality
materials with these long term performance
capabilities is a critical factor for this project.
By fi rst developing a 50 kW prototype
scaled down demonstrator with embedded
structural strain and air pressure monitoring,
the NOVA project team will be able to
Bonding the bladesThe UK NOVA project team has achieved a key milestone with the
successful construction of the sails for a 50 kW prototype demonstrator
of its concept 10 MW ‘double arm’ vertical axis wind turbine system
(VAWTS). This commercial 10 MW offshore turbine will have two 160 m
long arms supporting two 80 m long V shaped sails. When built, it
would be the heaviest composite construction in the world, weighing
around 160 tonnes.
An artist’s impression of the final design of 10 MW Aerogenerator X offshore wind turbine. The arm and sail structures are made from epoxy resin with carbon and glass fibre reinforcement. (Picture courtesy of Wind Power Ltd.)
RP0113_Feature Adhesives 21 10-01-13 16:41:21
CASE STUDY
REINFORCEDplastics JANUARY/FEBRUARY 201322 www.reinforcedplastics.com
gain an understanding of the engineering
performance and aerodynamic behaviour of
the design in use and extensively test the
composite materials selected in off shore
operational conditions.
The fabrication stage has already helped
the team to address on a much smaller
Figure 1: The carbon fibre epoxy ribs, spars and skins of the box design were bonded together with Crystic Crestomer 1152PA structural adhesive.
Figure 2: All the bond joints in the sail sections use a simple joggle design and shim plates to allow for rapid assembly with minimum fixtures and aerodynamically smooth joints.
Prior to bonding the Cranfield team ‘dry’ assembled the prototype sail spars and skins on the skin mould tool.
The rib sections of the central box were bonding into place at precise locations along the 10 m length of the sail.
For the prototype, the application of adhesive to the spar caps and upper skin was carried out by hand using brushes and spatulas. For large scale commercial production, pneumatic hand guns and bulk dispensing equipment would be used for cost effective manufacturing.
scale, any processing challenges to cost
eff ectively manufacture and assemble the
composite components. These insights can
then be applied to the full sized version to
help ensure its aff ordability and commercial
viability.
The overall turbine assembly has been
designed and constructed to have the best
structural reliability long term in order to
meet the key criteria of being ‘maintenance
free’ during its expected 20 years service
life. The two prototype rotor sails each have
dimensions of 10 m long by 1.9 m wide,
with a maximum depth of 180 mm at the
mid section.
The structural approach used for the
rotor sails is similar to a large commercial
aircraft wing. The sail has a central box
section, designed with tapering thickness
skins, two C spars with ribs and ‘omega’
shaped hat stringers to provide resistance
to buckling (Figure 1). The sail central box
components were manufactured from
multiaxial carbon fi bre fabrics and epoxy
resin using a vacuum infusion moulding
process. To the central box is added glass
fi bre reinforced leading and trailing edge
components.
Bearing in mind that the scaled up 10 MW
wind turbine sails would be 80 m long,
fi nding ways to reduce weight in the
overall sail design was critical. For the
prototype, the rotor sail weight was
signifi cantly reduced by using a structural
adhesive, which had the added benefi t
of providing lower overall manufacturing
costs compared to a jointed sectional and
mechanical assembly design. The carbon
fi bre/epoxy ribs, spars and skins of the box
design were bonded together with Scott
Bader Crystic Crestomer 1152PA adhesive.
The leading and trailing edge components,
separately fabricated from glass fi bre/epoxy
composite, were then bonded onto the
central box of the sail. All the bond joints
used a simple joggle design and shim
plates to allow for rapid assembly with
minimum fi xtures and aerodynamically
smooth joints (Figure 2).
As the adhesive was such a critical factor
in both the manufacturing and long term
off shore performance of the two lightweight
rotor sails, Cranfi eld University Composites
Centre carried out its own detailed study to
evaluate a range of possible adhesives for
this very demanding application.
“The design and scale of the sail rotor
structure means that there are large bond
surface areas and wide bond lines,” explains
Andrew Mills, Nova project leader at
Cranfi eld University Composites Centre.
“The fully cured structural adhesive must,
therefore, have long term performance
properties which meet a number of key
requirements. These include gap fi lling and
providing outstanding peel resistance, while
at the same time being strong and very
tough, with exceptional fl exural strength
properties.”
RP0113_Feature Adhesives 22 10-01-13 16:41:21
CASE STUDY
23REINFORCEDplastics JANUARY/FEBRUARY 2013www.reinforcedplastics.com
The Cranfi eld team carried out adhesive
performance comparative testing on a
range of bond-line thicknesses from 30 mm
down to 2 mm. The test results obtained
showed that the best performing adhesive
for bonding both carbon fi bre and glass
fi bre epoxy laminate substrates was
Crystic Crestomer 1152PA. These fi ndings
are supported by to the quality and long
term performance of Crestomer adhesives,
which have already been proven for over
30 years in many demanding composite
marine applications, such as deck and hull
stringer and bulkhead bonding, endorsed
by both Lloyds and RINA for composite
bonding in a variety of marine applications.
For the 10 m sail prototype, each
component and mould tool was designed
with joggled part fi t, scored fi tting positions
and 1 mm adhesive shims. This provided
accurate fi nal sail dimensions without the
use of complex assembly jigs. As part of
the assembly process to ensure joint
accuracy, after positioning without adhesive,
each part was drilled and the holes used to
either pin or rivet each part together after
adhesive application. All of the adhesive
joints were post cured in a portable taped
foam board oven for 24 hours at 50°C and
joint gaps were subsequently fi lled with
a body fi ller and abraded smooth using a
circular sander to eliminate evidence of the
component joints. ■
Further information
Cranfield University; www.cranfield.ac.uk
Scott Bader; www.scottbader.com/adhesives
Wind Power Ltd; www.windpower.ltd.uk
The leading edge section of the sail was bonded onto the central box. All adhesive joints were post cured in an oven for 24 hours at 50°C.
For an aerodynamically smooth sail surface, all adhesive joint gaps were filled with a body filler and made smooth using a circular sander prior to painting.
Finished, painted 10 m sails minus end plates, which are bolted on at each end to seal the sail units.
The finished sails, including end plates. The sails have designed to sustain at least 20 years’ service without maintenance.
RP0113_Feature Adhesives 23 10-01-13 16:41:22