(27 Jan 2022)
The Airbus C295 Flight Test Bed 2 (FTB2)
performed its maiden flight from the Final Assembly Line in
Seville, on Wednesday.
The aircraft now starts a flight campaign with the
aim of testing the new semi-morphing wing, the new
flight control system, as well as a SatCom antenna embedded within
the aircraft’s fuselage.
“The first flight of the C295 FTB2 is a key
milestone that represents an important step forward in the
programme, following the successful integration of the new aero
structures, power-on and ground tests,” said Francisco Javier
Sánchez Segura, Executive Vice President Engineering Airbus
Defence and Space. “A few years ago this programme was just a
dream of a more sustainable future for aviation. Today we are at
the final stage and we finally made it fly.”
Based on the Airbus C295, the Flight Test Bed 2 is
an in-flight demonstrator of the European Clean Sky 2 (CS2) and
the EU Horizon 2020 research and innovation programme, where
technologies related to CS2’s future regional multimission
aircraft are tested.
Airbus C295 Flight Test Bed 2 (FTB2)
The modifications include new materials and
technologies designed to achieve noise, CO2 and NOx emissions
reduction.
With the new technologies applied in a future regional multimission configuration, up to 43% CO2 and 70% NOx reductions
can be achieved in a typical Search and Rescue mission of 400
nautical miles, as well as 45% less noise during take-off.
The main modifications in the aircraft are a new
high-efficiency semi-morphing wing, new dynamic winglets and a
flat panel SATCOM antenna integrated within the top of the
fuselage.
In addition, innovative flight controls for primary
control surfaces, including ailerons, flaps and flap tabs with
improved aerodynamics, are capable of adjusting in-flight and
contribute to a more efficient high lift system.
The new flight control system leverages digital
control systems to optimise the aerodynamic shape of the wing in
flight, while a new multifunctional flap has been completely
redesigned and includes flap tabs in the trailing edge controlled
by electro-mechanical actuators.
The advantages also extend into the
manufacturing process, not least with the use of advanced
materials and manufacturing ranging from the use of Scalmalloy and
additive manufacturing, to a new assembly method for the aero
structures of the wing.
A one shot assembly approach has been used
for the new composite winglet and winglet tab, moving from the
conventional ribs approach to a multi-spar integrated torsion box.
Finally, jig-less methods have been used for the assembly of flaps
and ailerons.
As a result, the C295 FTB2 brings improvements not
only to the purely operational aspects of the aircraft, but helps
introduce new improvement to the design and manufacturing process.
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