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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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 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.

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

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 DE (TAUFKIRCHEN) coordinator 802˙190.00
2    TECHNISCHE UNIVERSITEIT DELFT NL (DELFT) participant 798˙296.00
3    THE CHANCELLOR MASTERS AND SCHOLARSOF THE UNIVERSITY OF CAMBRIDGE UK (CAMBRIDGE) participant 549˙922.00
4    CHALMERS TEKNISKA HOEGSKOLA AB SE (GOETEBORG) participant 301˙041.00
5    ARTTIC FR (PARIS) participant 295˙900.00
6    SIEMENS AKTIENGESELLSCHAFT DE (MUNCHEN) participant 295˙086.00
7    POLITECHNIKA WARSZAWSKA PL (WARSZAWA) participant 250˙675.00
8    MTU AERO ENGINES AG DE (MUNCHEN) participant 151˙250.00
9    AIRBUS DEFENCE AND SPACE GMBH DE (TAUFKIRCHEN) participant 104˙535.00
10    AIRBUS OPERATIONS GMBH DE (HAMBURG) participant 95˙459.00
11    ROLLS-ROYCE DEUTSCHLAND LTD & CO KG 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

year authors and title journal last update
List of publications.
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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