AviationWeek.com/awst AVIATION WEEK & SPACE TECHNOLOGY/JANUARY 15-FEBRUARY 1, 2015 53
Graham Warwick Washington
Cleaner Rotors
Reducing emissions and noise are goals
for European rotorcraft research program
A
irbus Helicopters has begun
ground tests of a diesel-cycle
piston engine in an EC120 light
helicopter, with the goal of demon-
strating a 30% reduction in specific
fuel consumption over the existing
turboshaft engine. Flight tests are
planned for the second quarter of
2015.
Testing is being conducted under
the High-Compression Engine (HCE)
project within the European Clean Sky
research program’s Green Rotorcraft
(GRC) integrated technology demon-
stration. The 330-kw (440-hp.) HIPE-
AE440 engine has been developed by
AustroEngine and TEOS.
Diesel-cycle engines are more fuel-
efcient than gas turbines and can burn
the same kerosene jet fuel, but they are
heavy and have previously been unable
to achieve the power output required
at a weight low enough for use in a light
helicopter such as the EC120.
The HIPE-AE440 has been designed
using technologies from the motor-
racing sector. The core engine weighs
197 kg (434 lb.) dry and 249 kg as an
installed powerpack, including cooling,
clutch, harnesses and other ancillaries.
This gives a weight-to-power ratio of
0.8 kg/kw.
“This is the first time a piston engine
delivering 330 kw with a weight-to-
power ratio of 0.8 is being developed.
This was made possible thanks to
proven car-racing technologies; oth-
erwise it probably would have taken
twice as long,” says Sebastien Dubois,
GRC project ofcer.
“Engines with the power range to
replace the turbine did not exist with
the mass required for the EC120, but
there has been tremendous progress
in automobile racing, particularly Le
Mans,” he says.
Started two years ago, the €9.3 mil-
lion ($11.4 million) HCE program was
planned to last 39 months. After some
problems with parts breaking in pre-
liminary testing, the project will now
run for 42 months. Typically, devel-
oping a new engine takes around five
years, says Dubois.
The HIPE-AE440 is a V8 with four
valves per cylinder with common rail
high-pressure fuel injection and two
turbochargers with air-to-air inter-
cooler. Its design combines Austro-
Engines experience producing tur-
bodiesels for aircraft with TEOS’s
race-car engine expertise.
The project will enable direct com-
parison between the EC120 with tur-
bine and diesel power. In addition to
lower fuel consumption, reductions of
40% in carbon dioxide and 50% in nitro-
gen-oxides emissions are expected and
up to 30% lower direct operating costs.
Ground tests are being performed at
Airbus Helicopters’ Marignane plant
in France. Some 15 hr. of flight testing
is planned. This will take the high-
compression engine to a technology
readiness level (TRL) of 6—the objec-
tive for Clean Sky—ready to be used in
product development.
Other Green Rotorcraft projects are
entering the hardware demonstration
phase, including separate eforts look-
ing at actively controlled and passively
optimized rotor blades and an electric
tailrotor drive.
Under the active Gurney flap proj-
ect led by AgustaWestland, model ro-
tor testing is planned for the second
quarter of 2015, followed by full-scale
whirl-tower testing in the third quar-
ter and flight tests on an AW139 in the
fourth quarter.
A small surface that deploys verti-
cally upward from the trailing edge of
the mid-blade section on the retreat-
ing side of the rotor, the Gurney flap
increases lift on the retreating blade
and reduces the power required to
maintain forward speed.
Airbus Helicopters, meanwhile,
is leading the passively optimized
blade project, which promises power
reductions of 5% in hover and 2% in
cruise—and 4-5-db lower approach
noise—through optimization of blade
chord, twist and other features, such
as anhedral.
Aerodynamic and acoustic design is to
be finished in January, says Dubois, with
manufacture of the blades to begin in the
second half of 2015. Whirl-tower testing
is planned for January 2016. Flight tests
on an EC135 in the early summer of 2016
are not yet funded, but a decision will be
taken in mid-2015, he says.
AgustaWestland is leading the elec-
tric tailrotor drive (Eletad) project,
working with Bristol University in the
U.K. The project is developing a high-
power-density electric motor with high
integrity and reliability. The first pro-
totype motor and an alternative solu-
tion have been delivered for evaluation.
The drive motor and control al-
gorithm will run on a tailrotor test
stand in 2015-16. The motor will be
integrated into a helicopter tailboom
and drive a complete AW139 tailrotor.
System power will come from aircraft
air-cooled electrical generators to pro-
vide a fully integrated system.
The rig will evaluate system dy-
namic operation while powering the
rotor through mission-representative
tail load cycles. “We will completely
simulate the working conditions of the
tailrotor with a complete system inside
a tail. The objective is TRL 5 through
ground test,” says Dubois. c
ROTORCRAFT
Ground tests of AustroEngine’s
diesel-cycle HIPE-AE440 in an
EC120 begin this month at Airbus
Helicopters in Marignane.
CLEAN SKY JOINT UNDERTAKING