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TRIMIS

ConcEpt validatioN sTudy foR fusElage wake-filLIng propulsioN intEgration

CENTRELINE

ConcEpt validatioN sTudy foR fusElage wake-filLIng propulsioN intEgration

Link to CORDIS:
Objectives: 

"The CENTRELINE project aims at maximising the benefits of aft-fuselage wake-filling under realistic systems design and operating conditions. The concept realises fuselage wake-filling through a single propulsive device installed at the fuselage aft-end with the purpose to entrain and re-energise the fuselage boundary layer flow, the so-called Propulsive Fuselage Concept (PFC). The aft-fuselage propulsor is driven turbo-electrically with power supplied through generator off-takes from advanced geared turbofan engines in under-wing installation.

CENTRELINE will perform the proof of concept and initial experimental validation for a highly promising propulsion-airframe integration approach in order to mature this technology from currently TRL 1-2 to TRL 3-4. Advanced pre-design methods based on high-fidelity numerical simulation and integrated multidisciplinary design optimisation techniques will be adopted in order to produce best and balanced design solutions for the concept. The technological key features will be initially validated through physical experiments including scale-model wind tunnel testing for the overall configuration as well as specialised aerodynamic rig testing of the boundary layer ingesting aft-fuselage propulsor. The proposed research and innovation actions represent the immediate exploitation of results of the highly successful FP7 L-0 project “DisPURSAL” (GA no. 323013).

The optimised system technology concept will be eco-environmentally benchmarked against an advanced conventional reference aircraft equipped with aerodynamic, structural, power plant and systems technologies suitable for a potential Entry Into Service (EIS) year 2035, referred to as "R2035". The objective CO2 reductions of the concept at integrated vehicular level are -11% against the R2035 (which means –40% CO2 versus the Y2000 SRIA reference). A detailed technology roadmap will be developed, indicating how to transfer these improvements to TRL 6 in 2030."

Institution Type:
Institution Name: 
European Commission
Type of funding:
Lead Organisation: 

Bauhaus Luftfahrt Ev

Address: 
Boltzmannstraße
85748 Garching Near Munich
Germany
EU Contribution: 
€802,190
Partner Organisations: 

The Chancellor Masters And Scholars Of The University Of Cambridge

Address: 
TRINITY LANE THE OLD SCHOOLS
CAMBRIDGE
CB2 1TN
United Kingdom
EU Contribution: 
€549,922

Airbus Defence And Space Gmbh

Address: 
Ludwig-Boelkow-Allee 1
85521 Ottobrunn
Germany
EU Contribution: 
€199,995

Politechnika Warszawska

Address: 
Plac Politechniki 1
00 661 Warszawa
Poland
EU Contribution: 
€250,675

Arttic

Address: 
58A rue du Dessous des Berges
75013 PARIS
France
EU Contribution: 
€295,901

Mtu Aero Engines

Address: 
Dachauer Strasse 665
80995 MUENCHEN
Germany
EU Contribution: 
€151,250

Siemens Ag

Address: 
Wittelsbacherplatz 2
80333 MUENCHEN
Germany
EU Contribution: 
€331,250

Technische Universiteit Delft

Address: 
.
2600 GA Delft
Netherlands
EU Contribution: 
€798,296

Chalmers Tekniska Hoegskola Ab

Address: 
-
41296 GOTHENBURG
Sweden
EU Contribution: 
€301,041
Technologies: 
Development phase: