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CENTRELINE SIGNED

ConcEpt validatioN sTudy foR fusElage wake-filLIng propulsioN intEgration

Total Cost €

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EC-Contrib. €

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Partnership

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Outcomes and
results

CENTRELINE project word cloud

Explore the words cloud of the CENTRELINE project. It provides you a very rough idea of what is the project "CENTRELINE" about.

realises re improvements pfc perform aircraft 11 fp7 layer technologies innovation propulsive validation configuration entrain solutions mature wing environmentally ga power entry technological off actions reference techniques balanced centreline device conventional r2035 2030 initially experiments 323013 benefits eis specialised tunnel reductions purpose supplied trl turbo sria aft roadmap co2 proof installation wind takes engines optimisation service successful benchmarked initial equipped maximising vehicular turbofan fuselage versus indicating single suitable structural model propulsor filling numerical ingesting boundary propulsion realistic flow rig fidelity experimental 40 2035 aerodynamic dispursal y2000 wake generator eco transfer physical simulation electrically multidisciplinary geared integration plant airframe installed energise validated

Project "CENTRELINE" data sheet

The following table provides information about the project.

Coordinator	BAUHAUS LUFTFAHRT EV Organization address address: WILLY MESSERSCHMITT STRASSE 1 city: TAUFKIRCHEN postcode: 82024 website: www.bauhaus-luftfahrt.net contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.
Coordinator Country	Germany [DE]
Project website	https://www.centreline.eu/
Total cost	3˙680˙520 €
EC max contribution	3˙680˙519 € (100%)
Programme	1. H2020-EU.3.4. (SOCIETAL CHALLENGES - Smart, Green And Integrated Transport)
Code Call	H2020-MG-2016-Two-Stages
Funding Scheme	RIA
Starting year	2017
Duration (year-month-day)	from 2017-06-01 to 2020-05-31

Partnership

Take a look of project's partnership.

#	participants	country	role	EC contrib. [€]
1	BAUHAUS LUFTFAHRT EV BAUHAUS LUFTFAHRT EV Organization address address: WILLY MESSERSCHMITT STRASSE 1 city: TAUFKIRCHEN postcode: 82024 website: www.bauhaus-luftfahrt.net contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	DE (TAUFKIRCHEN)	coordinator	802˙190.00
2	TECHNISCHE UNIVERSITEIT DELFT TECHNISCHE UNIVERSITEIT DELFT Organization address address: STEVINWEG 1 city: DELFT postcode: 2628 CN website: www.tudelft.nl contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	NL (DELFT)	participant	798˙296.00
3	THE CHANCELLOR MASTERS AND SCHOLARSOF THE UNIVERSITY OF CAMBRIDGE THE CHANCELLOR MASTERS AND SCHOLARSOF THE UNIVERSITY OF CAMBRIDGE Organization address address: TRINITY LANE THE OLD SCHOOLS city: CAMBRIDGE postcode: CB2 1TN website: www.cam.ac.uk contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	UK (CAMBRIDGE)	participant	549˙922.00
4	CHALMERS TEKNISKA HOEGSKOLA AB CHALMERS TEKNISKA HOEGSKOLA AB Organization address address: - city: GOETEBORG postcode: 41296 website: www.chalmers.se contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	SE (GOETEBORG)	participant	301˙041.00
5	ARTTIC ARTTIC Organization address address: RUE DU DESSOUS DES BERGES 58A city: PARIS postcode: 75013 website: www.arttic.eu contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	FR (PARIS)	participant	295˙900.00
6	SIEMENS AKTIENGESELLSCHAFT SIEMENS AKTIENGESELLSCHAFT Organization address address: WERNER-VON-SIEMENS-STR. 1 city: MUNCHEN postcode: 80333 website: www.siemens.com contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	DE (MUNCHEN)	participant	295˙086.00
7	POLITECHNIKA WARSZAWSKA POLITECHNIKA WARSZAWSKA Organization address address: PLAC POLITECHNIKI 1 city: WARSZAWA postcode: 00 661 website: http://www.pw.edu.pl contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	PL (WARSZAWA)	participant	250˙675.00
8	MTU AERO ENGINES AG MTU AERO ENGINES AG Organization address address: DACHAUER STRASSE 665 city: MUNCHEN postcode: 80995 website: www.mtu.de contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	DE (MUNCHEN)	participant	151˙250.00
9	AIRBUS DEFENCE AND SPACE GMBH AIRBUS DEFENCE AND SPACE GMBH Organization address address: WILLY-MESSERSCHMITT-STRASSE 1 city: TAUFKIRCHEN postcode: 82024 website: www.airbus-group.com contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	DE (TAUFKIRCHEN)	participant	104˙535.00
10	AIRBUS OPERATIONS GMBH AIRBUS OPERATIONS GMBH Organization address address: KREETSLAG 10 city: HAMBURG postcode: 21129 website: www.airbus.com contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	DE (HAMBURG)	participant	95˙459.00
11	ROLLS-ROYCE DEUTSCHLAND LTD & CO KG ROLLS-ROYCE DEUTSCHLAND LTD & CO KG Organization address address: Eschenweg 11 city: BLANKENFELDE-MAHLOW postcode: 15827 website: www.rolls-royce.com/deutschland contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	DE (BLANKENFELDE-MAHLOW)	participant	36˙163.00

Map

Project objective

'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.'

Deliverables

List of deliverables.
CENTRELINE technology transfer workshop	Websites, patent fillings, videos etc.	2020-04-02 10:46:07
Specification of wind tunnel model and test campaign plan	Documents, reports	2020-02-14 11:38:45
Interim report on fuselage and nacelle aero-structural pre-design	Documents, reports	2020-02-14 11:38:45
Specification of propulsive fuselage aircraft layout and design features	Documents, reports	2020-02-14 11:38:45
CENTRELINE public workshop for policy makers	Websites, patent fillings, videos etc.	2020-02-14 11:38:45
Electric machinery preliminary design report	Documents, reports	2020-02-14 11:38:45
Interim report on fuselage-wing junction aero-structural investigation	Documents, reports	2020-02-14 11:38:45
CENTRELINE public website	Websites, patent fillings, videos etc.	2020-02-14 11:38:45
Definition of multidisciplinary interfacing strategy	Documents, reports	2020-02-14 11:38:45
Dissemination and exploitation plan	Documents, reports	2020-02-14 11:38:45
Specification of fan design and rig test campaign plan	Documents, reports	2020-02-14 11:38:45

Take a look to the deliverables list in detail: detailed list of CENTRELINE deliverables.

Publications

List of publications.
year	authors and title	journal	last update
2019	Zdobyslaw Jan Goraj, Mariusz Kowalski, Bartlomiej Goliszek Stress, strain and displacement analysis of geodetic and conventional fuselage structure for future passenger aircraft published pages: , ISSN: 0002-2667, DOI:	Aircraft Engineering and Aerospace Technology	2020-02-14
2018	Bijewitz, J., Seitz, A. and Hornung, M. Power Plant Pre-Design Exploration for a Turbo-Electric Propulsive Fuselage Concept published pages: , ISSN: , DOI:		2020-02-14
2018	Seitz, A., Peter, F., Bijewitz, J., Habermann, A., Goraj, Z., Kowalski, M., Castillo Pardo, A., Hall C., Meller, F., Merkler, R., Petit, O., Samuelsson, S., Della Corte, B., van Sluis, M., Wortmann, G. and Dietz, M. Concept Validation Study for Fuselage Wake-Filling Propulsion Integration published pages: , ISSN: , DOI:		2020-02-14
2018	Goraj, Z., Goliszek, B., Kowalski , M., Seitz, A., Peter, F. and Meller, F. Strategy and Implementation of a Parametric CAD Model for R2035 Aircraft Structure and External Configuration published pages: , ISSN: , DOI:		2020-02-14
2018	Habermann, A.L., Bijewitz, J., Seitz, A. and Hornung, M. Performance Bookkeeping for Aircraft Configurations with Fuselage Wake-Filling Propulsion Integration published pages: , ISSN: , DOI:		2020-02-14

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The information about "CENTRELINE" are provided by the European Opendata Portal: CORDIS opendata.

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