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ACASIAS SIGNED

Advanced Concepts for Aero-Structures with Integrated Antennas and Sensors

Total Cost €

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EC-Contrib. €

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Partnership

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 ACASIAS project word cloud

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

covered    fibre    aviation    laminate    disciplinary    consumption    substrates    nasa    19890003194    gov    active    asac    aircraft    slot    layer    decreased    efficient    ntrs    integration    savings    foam    fuselage    action    ing    satcom    composite    metal    aerodynamic    innovations    band    stiffened    partly    multifunctional    mm    panel    installation    11    sensors    sound    acasias    co2    facilitated    smart    rotating    conformal    performance    disciplines    communication    pressure    antenna    panels    competitive    harmonic    airlines    cabin    propulsion    vhf    equivalent    fuel    wiring    countries    25    glare    glass    meuros    structural    months    ortho    annoying    realize    quartz    miniaturized    turbofan    archive    http    blade    winglet    tiles    posed    noise    chain    radiated    grid    casi    energy    cror    aero    integrating    pdf    uses    structures    36    caused    epoxy    emissions    supply    acoustic    special    engines    antennas    rotor    contra    ku   

Project "ACASIAS" data sheet

The following table provides information about the project.

Coordinator
STICHTING NATIONAAL LUCHT- EN RUIMTEVAARTLABORATORIUM 

Organization address
address: Anthony Fokkerweg 2
city: AMSTERDAM
postcode: 1059CM
website: www.nlr.nl

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 Netherlands [NL]
 Project website http://www.acasias-project.eu/
 Total cost 5˙836˙430 €
 EC max contribution 5˙836˙430 € (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  2020-11-30

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    STICHTING NATIONAAL LUCHT- EN RUIMTEVAARTLABORATORIUM NL (AMSTERDAM) coordinator 1˙310˙087.00
2    IMST GMBH DE (KAMP LINTFORT) participant 922˙696.00
3    DEUTSCHES ZENTRUM FUER LUFT - UND RAUMFAHRT EV DE (KOELN) participant 603˙427.00
4    INVENT INNOVATIVE VERBUNDWERKSTOFFEREALISATION UND VERMARKTUNG NEUERTECHNOLOGIEN GMBH DE (BRAUNSCHWEIG) participant 558˙442.00
5    VYZKUMNY A ZKUSEBNI LETECKY USTAV AS CZ (PRAHA 18) participant 461˙295.00
6    TRACKWISE DESIGNS LIMITED UK (TEWKESBURY) participant 409˙100.00
7    FOKKER AEROSTRUCTURES BV NL (Papendrecht) participant 401˙775.00
8    CENTRE INTERNACIONAL DE METODES NUMERICS EN ENGINYERIA ES (BARCELONA) participant 366˙014.00
9    EVEKTOR SRO CZ (KUNOVICE) participant 360˙184.00
10    L - UP SAS FR (PARIS) participant 279˙520.00
11    FOKKER ELMO BV NL (HOOGERHEIDE) participant 163˙884.00

Map

 Project objective

The overall objective of ACASIAS is to contribute to the reduction of energy consumption of future aircraft by improving aerodynamic performance and by facilitating the integration of novel efficient propulsion systems such as contra-rotating open rotor (CROR) engines.

The aerodynamic performance is improved by the conformal and structural integration of antennas. The installation of CROR engines is facilitated by installation of an Active Structural Acoustic Control (ASAC) system in the fuselage. The integration of such a system in fuselage panels will annoying noise in the cabin caused by multi-harmonic sound pressure level which is radiated by CROR engines. CROR engines are able to realize up to 25% fuel and CO2 savings compared to equivalent-technology turbofan engines (http://ntrs.nasa.gov/archive/nasa/casi.ntrs.nasa.gov/19890003194.pdf).

The ACASIAS project focuses on challenges posed by the development of aero- structures with multifunctional capabilities. The following concepts structural concepts are considered: • A composite stiffened ortho-grid fuselage panel for integrating Ku-band SATCOM antenna tiles. • A fuselage panel with integrated sensors and wiring for reduction of CROR cabin noise. • A smart winglet with integrated blade antenna (integrated substrates into special foam, partly covered by a 1 mm glass/quartz epoxy layer). • A Fibre Metal Laminate GLARE panel with integrated VHF communication slot antenna.

The 36 months action with a project cost of 5.8 MEuros will bring together 11 partners from 6 countries covering the three main disciplines required: (composite) structures, advanced antennas and miniaturized sensors in a multi-disciplinary project. The project innovations facilitated by integration of these disciplines, as well as resulting in operational cost reduction and decreased emissions for airlines, will also lead to a more competitive supply chain in the aviation sector, which increasingly uses composite structures.

 Deliverables

List of deliverables.
Dissemination set (leaflet, poster, newsletter) Documents, reports 2020-02-17 14:55:22
Requirements and Specification Document. Documents, reports 2020-02-17 14:55:22
Gender Equity Policy Documents, reports 2020-02-17 14:55:22
Public website Websites, patent fillings, videos etc. 2020-02-17 14:55:22
Structural modelling Documents, reports 2020-02-17 14:55:22
Industrial integration technology from WP3 Documents, reports 2020-02-17 14:55:22
Specifications for the smart active panel Documentation of specifications in task 3.1 Documents, reports 2020-02-17 14:55:22

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

 Publications

year authors and title journal last update
List of publications.
2018 Stephan Algermissen
Smart Acoustic Lining Panel
published pages: , ISSN: , DOI:
8th EASN-CEAS International Workshop on Manufacturing for Growth & Innovation 4.-7.09.2018 2020-02-17
2018 Petr Vrchota, Stefan Steeger, Marta Martinez-Vazquez, Martin Svetlik, Zdenek Reznicek
Aerodynamic and structural design of winglet with integrated VHF antenna
published pages: 18, ISSN: 2261-236X, DOI: 10.1051/matecconf/201823300018
MATEC Web of Conferences 233 2020-02-17

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