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FLOWCAASH SIGNED

FLOW Control Actuators at Aircraft scale manufacturing by SLM with high aerodynamic performance for using in Harsh environment

Total Cost €

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EC-Contrib. €

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Partnership

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 FLOWCAASH project word cloud

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

laser    geometries    am    preferred    environments    center    tests    chosen    installed    sand    accomplished    rain    aerodynamic    pulsed    flowcaash    treatments    reduce    safe    distortion    blowing    melting    fluid    active    aircraft    quality    manufacturing    structural    thermal    bar    assure    actuators    additive    afterwards    post    withstand    source    designs    harsh    steady    jet    anti    flight    pressures    coefficient    selective    separation    balanced    brings    manufacture    surface    flow    temperatures    cta    melt    ultra    aerospace    dimensional    innovative    powder    ratio    lortek    numerical    actuator    heat    stability    generation    icing    simulations    vibrations    dust    restricted    reliability    alloy    processed    parts    performance    manufactured    weight    bypass    uhbr    energy    strength    deg    utilizes    engines    lift    pja    environment    ti6al4v    afc    prediction    aircrafts    resistance    laboratory    slm    bed    reducing    validated    sba    ti    bionic    space    260   

Project "FLOWCAASH" data sheet

The following table provides information about the project.

Coordinator
LORTEK S COOP 

Organization address
address: ARRANOMENDIA KALEA 4 A
city: ORDIZIA
postcode: 20240
website: www.lortek.es

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 Spain [ES]
 Project website http://www.flowcaash.eu/
 Total cost 549˙061 €
 EC max contribution 549˙061 € (100%)
 Programme 1. H2020-EU.3.4.5.1. (IADP Large Passenger Aircraft)
 Code Call H2020-CS2-CFP06-2017-01
 Funding Scheme CS2-IA
 Starting year 2018
 Duration (year-month-day) from 2018-04-01   to  2020-12-31

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    LORTEK S COOP ES (ORDIZIA) coordinator 348˙811.00
2    FUNDACION CENTRO DE TECNOLOGIAS AERONAUTICAS ES (MINANO (ALAVA)) participant 200˙250.00

Map

 Project objective

The main goal of FLOWCAASH project is to design and manufacture reliable and safe flow control actuators at aircraft scale by Selective Laser Melting (SLM) able to withstand the high temperatures (up to 260 °C) and pressures (5 bar) during flight test with aerodynamic performance and high resistance to harsh environments. FLOWCAASH project is focused on the development of innovative designs of Active Flow Control (AFC) actuators to be manufactured by powder bed based additive manufacturing (AM) using Ti6Al4V alloy. Selective Laser Melting (SLM), that utilizes a laser as a thermal energy source to melt the powder has been chosen as the preferred AM technology. The innovative designs of these AFC actuators will allow to be installed in restricted space in the next generation aircrafts with UHBR (Ultra High Bypass Ratio) engines. Two different actuators will be considered, Pulsed Jet Actuator (PJA) and Steady Blowing Actuator (SBA). These actuators will have the potential to reduce aerodynamic flow separation and to increase lift coefficient. This will be obtained by bionic design which allows complex geometries and improve structural strength while reducing the weight. In order to assure process reliability of large Ti parts, distortion prediction numerical simulations will be accomplished. As-built part will be post-processed by means of heat and surface treatments in order to ensure dimensional stability and adequate surface quality for aerodynamic performance. Afterwards the actuators will be validated by aerodynamic and harsh environment tests including rain, icing, sand and dust, vibrations and anti-icing fluid. The FLOWCAASH project will be developed by a well-balanced consortium that brings together 2 partners: the research center LORTEK and the aerospace test laboratory CTA.

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

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