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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.

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

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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