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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.

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

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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