In 2012, a manned aircraft powered by 11,628 photovoltaic
cells covering 2,200 sq ft of wing space will circumnavigate the globe - if a
global engineering team can make it light enough.
Called the Solar
Impulse, the first prototype of the aircraft flew an entire daily solar
cycle, including nearly nine hours of night flying, in July.
"During the whole of the flight, I just sat there and
watched the battery charge level rise and rise. Sitting in a plane producing
more energy than it consumes is a fantastic feeling", says Andrè Borschberg,
CEO and co-founder of the Solar Impulse project.
"Flying by night using solely solar power is a stunning
manifestation of the potential that clean technologies offer today to reduce
the dependency of our society on fossil fuels," says Bertrand Piccard,
initiator and president of Solar Impulse.
The engineer heading up the structural design of the Solar
Impulse is Peter Frei, who graduated from the Swiss Federal Institute of
Technology (ETHZ) in mechanical engineering with specialization in fluid
dynamics and lightweight structures. Frei also is a former Swiss fighter pilot.
Reporting to Frei are a small group of staff engineers and a
large group who work for corporate partners. They include Claude Michel, senior
vice president at Solvay and head of the Solvay-Solar Impulse Partnership. The
Solvay Group is one of the three major funding partners for the aircraft and the
current prototype features a profusion of new materials developments from
Solvay companies such as Solvay Advanced Polymers in Alpharetta, GA, and Solvay
Solexis of Milan, Italy.
"In terms of technical constraints, the question is very
simple," Michel told Design News
need a surface area of photovoltaics that delivers enough energy to put into
the air a certain amount of weight. This is what we call the equation of the Solar
Impulse. One square meter in photovoltaics delivers 30 watts, and with that 30
watts, we can put 8 kg (17.6 lb) in the air. This is our target, and it is an
One of the most interesting lightweighting solutions is a
honeycomb structure sandwiched between two carbon fiber foils that function as
wing and stabilizer spars. The honeycomb is a lightweight paper structure
impregnated with a Torlon
AI10 polyamide-imide polymer via a dipping process. The result is a composite
structure that possesses excellent mechanical properties, including strength,
torsion, flexion and vibration. Sections of the wing that are 66-ft long can be
easily handled by a few people.
Torlon, originally developed by Union Carbide, functions as a
glue in the honeycomb structure. It features the highest strength and stiffness
of any thermoplastic up to 525F and has outstanding resistance to wear, creep
and chemicals, making it ideal for severe environments.
Another interesting development is a centering cylinder for
the landing system. It was initially designed in aluminum and is being replaced
with Ixef polyarylamide 1022.
Ixef compounds are typically highly loaded with glass (50 to
60 percent) and possess the tensile and flexural strength similar to many cast
metals and alloys at ambient temperature. Ixef 1032 (60-percent glass fiber)
exhibits typical values of 280 MPa at 73F.
The internal cylinder component is machined to its final
dimension from an extruded rod of Ixef 1022. The external part remains aluminum
due to impact requirements. The shaft is made from PrimoSpire
due to its intrinsic modulus and its machinability. PrimoSpire
self-reinforced polyphenylene (SRP) is one of the stiffest and strongest
unreinforced plastics available. Even without fiber reinforcement, PrimoSpire
SRP delivers tensile properties that are comparable to those of many reinforced
plastics. The added benefits are lighter weight and no loss of ductility.Radel
polyphenylsulfone is used for the rear attachment legs in the landing system
assembly due to its high deformation capability.
Many other plastics from Solvay Advanced Polymers are used
for other parts, more than 6,000 all together, such as bolts, screws, nuts and washers
in the HB-SIA prototype to minimize weight.
High-performance plastic films play an important role in
stabilizing the wings of the Solar Impulse.
"The wings are somewhat flexible," says Michel. "Their shape
is quite different on the ground than in the air. We can use films to alleviate
Solef PVdF-based laminate is used to cover the ailerons,
elevators, rudder, airbrakes and spoilers because of its mechanical strength at
low thickness (15 microns). It will be used for the entire airplane wings of
the next version of the Solar Impulse, called HB-SIB, if Solvay can provide the
material in 3m (9.8 ft) width. The development partners for the new technology
of Woonsocket, RI, for the film extrusion and with Jehier
of Hutchinson, France, for the lamination.
Here's what the 60m (197 ft) wing looks like:
Spars are made of honeycomb-carbon fibers that support
120 ribs, which profile the shape of the wing;
An encapsulated photovoltaic system is on top; and
A laminated PVdF film is on the underside.
It may surprise some design engineers how stiff that system
is. The deflection, defined as the difference between ground and flight
positions, at the wing tips is less than 0.5M (19.7 inch).
The film that protects the photovoltaic (PV) cells from the
harsh environment is made from Halar
ethylene chlorotrifluoroethylene (ECTFE).
Both plasma and corona treatments have been studied in order
to increase the adhesiveness of the fluorinated films to the epoxy layer, the
encapsulation material used by Solar Impulse. The thickness of the film
produced by Ajedium of Newark, DE, was reduced to 17 microns, resulting in
about 35 percent weight savings with acceptable electrical performance.
Solvay Solexis is looking for more ways to save weight. A
solution with a single product replacing both the glass-reinforced epoxy layer
and the top film is under evaluation.
A PVdF-based adhesive tape that is both UV-transparent and
UV-resistant is used to close gaps between the solar cells.
The fuselage is made from carbon fiber rods encapsulated
with polyester film. The name of the supplier of the polyester film was not
made public. Décision
Swiss boat builder, is the composite materials specialist for the Solar
Impulse, and Brühlmeier Modellbau
also Swiss, manufactures composite parts.
Polyurethane foams are used to make the cockpit of the airplane
light, but also stable, while providing insulation.
"We're trying not to use any watts for heating or air
conditioning," says Michel. The pilot must be protected from temperatures that
can go as low as -40C (-40F), and the batteries must be kept above 15C (59F).
Solvay Fluor's third-generation blowing agent Solkane 365 provides
high gas phase lambda (thermal conductivity) value and foam dimensional
stability/compressive strength. Foam insulation is used for the cockpit, four
motor gondolas and the wing tips. These pieces are produced by forming big
blocks and then machining the eggshell-shaped wing tips out of them.
A new partner providing materials technologies for the Solar
Impulse is Bayer
(BMS) of Leverkusen, Germany.
Lightweight polyurethane foam from Puren GmbH
of Überlingen, Germany, used in the engine
cowling, cockpit cladding and the wings is based on raw materials from Bayer
MaterialScience. The cockpit windows are made of thin but strong Makrofol
The bar is rising for the next version of the Solar Impulse
both for structural requirements and materials' technologies.
One interesting possibility is the use of carbon nanotubes,
which are described as the strongest and stiffest materials available in terms
of tensile strength and elastic modulus, respectively.
BMS says they are nearly as strong as steel, but half as
heavy. They also conduct electric current as effectively as copper.
Bayer MaterialScience operates a CNT plant in Leverkusen
with an annual capacity of 200 metric tons. BCC Research forecasts
sales of carbon nanotube-reinforced plastics will grow at an average annual rate
exceeding 55 percent over the next five years for electrical/electronic,
transportation, structural and other applications.
The second prototype is scheduled to fly around the world in
five stages, each lasting five days, traveling at an average speed of 70 km/h
Improvements in battery technology will play a critical
"In order to fly at night, we need to store energy that is
captured during the day," says Michel. "There are 400 kilos (882 lb) of
batteries and this is the chief bottleneck in the system."
Electrical energy harvested by the solar cells is stored in
lithium batteries, where PVdF is used as a binder for both electrodes. The PVdF
also boosts the electrochemical stability of the cells, allowing repeated
charging and discharging cycles at a high rate, without deterioration of
The original design of the plane in 2004 was made with Li
batteries having an electric density of 180 Wh/Kg. The four 100 Kg batteries of
HB-SIA (the current prototype) have an electric density of 220 Wh/Kg.
Solvay says that a recently developed grade of PVdF offers
very high adhesion to the electrodes, potentially contributing to the weight
reduction of batteries for HB-SIB (the 2013 flight aircraft).
Carbon nanotubes could significantly improve battery
performance, but officials at Bayer MaterialScience declined specific comment.
New PV System
The original design of the plane was made with monocrystalline
silicon photovoltaic cells, having a thickness of 180 microns and an energy
efficiency of 18 percent. The PV system is now made of 11,628 mono crystalline
silicon cells whose thickness is below 150 microns for an energy efficiency of
22 percent after encapsulation.
Solar Impulse originally used small cells with both front
and back electrical contacts from RWE Solutions (now Azur Space Solar Power
GmbH). The Solar Impulse engineering team is now using large cells (125 x 125
mm) from Sun Power
(that are now on
the prototype). These have back contacts, higher efficiency, and need less
electrical connections due to their larger size.
For the design and development phases of Solar Impulse,
Solvay performed more than 2,000 hours of non-linear finite element analysis
(FEA) with ABAQUS on the thermo-mechanical behavior of several modules under
different conditions. Linear simulation is used to model metallic structures.