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NATHENA SIGNED

New Additive manufacTuring Heat ExchaNger for Aeronautic

Total Cost €

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EC-Contrib. €

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Partnership

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 NATHENA project word cloud

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

correlations    phenomenon    inner    hybrid    exchangers    flow    200    relevance    500x300x300mm    seems    fluidic    accordingly    latticed    power    pressure    limit    performances    inconel    heat    validity    matrix    thermal    structural    types    simulation    fins    performance    compact    structures    below    thin    tubing    see    exchanger    choices    400    500kw    walled    topological    nathena    technologies    deg    2kg    assies    manufacturing    reynolds    welded    parametric    structure    made    mostly    metal    model    models    physical    thermo    material    behavior    propulsion    regular    reached    max    additive    delta    tests    mechanical    combinations    optionally    customization    air    efficient    temperature    calculation    10000    basic    iterative    components    evolutionary    drop    core    new    regarding    01kg    repetitive    final    folded    aeronautic    sheet    combined    form    progress    direct    aluminium    size    entails    laws    predictive    manufacture    unitary    optimization    100mbar    hamper   

Project "NATHENA" data sheet

The following table provides information about the project.

Coordinator
SOGECLAIR AEROSPACE SAS 

Organization address
address: AVENUE ALBERT DURAND 7
city: BLAGNAC
postcode: 31700
website: n.a.

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 France [FR]
 Project website http://www.sogeclair.com/news/European
 Total cost 1˙499˙177 €
 EC max contribution 1˙499˙177 € (100%)
 Programme 1. H2020-EU.3.4.5.1. (IADP Large Passenger Aircraft)
 Code Call H2020-CS2-CFP06-2017-01
 Funding Scheme CS2-RIA
 Starting year 2018
 Duration (year-month-day) from 2018-03-01   to  2022-02-28

 Partnership

Take a look of project's partnership.

# participants  country  role  EC contrib. [€] 
1    SOGECLAIR AEROSPACE SAS FR (BLAGNAC) coordinator 416˙912.00
2    ADDUP FR (CEBAZAT) participant 388˙440.00
3    INSTITUT VON KARMAN DE DYNAMIQUE DES FLUIDES BE (RHODE SAINT GENESE) participant 367˙600.00
4    TEMISTH SAS FR (MARSEILLE) participant 326˙225.00

Map

 Project objective

New Additive manufacTuring Heat ExchaNger for Aeronautic Today’s technologies and processes dedicated to the exchangers manufacturing hamper progress on higher performances (mechanical assies of repetitive and regular unitary components like folded sheet metal and/or tubing mostly welded). Traditional manufacturing entails limit for the customization of the inner structure, which have a direct impact on the thermal behavior of the exchanger core. Design and manufacture a complex core structure accordingly and well adapted to the inner thermal phenomenon seems to be a promising way to increase performances. Accordingly, NATHENA project aims at developing new complex inner structures for heat exchangers. NATHENA project will focus on the design development of a complex compact heat exchanger that best addresses thermal performance, made by additive manufacturing. These new compact air-air heat exchangers developed in NATHENA project will provide an efficient thermal management system dedicated to hybrid propulsion system. Two types of material will be studied regarding heat exchanger use: Aluminium for low temperature range and Inconel for high temperature range. The set objectives (see targets below) will be reached using calculation and multi-physical simulation (thermo-mechanical-fluidic) applied to evolutionary latticed and thin-walled structures combined optionally with fins to form a matrix of complex structures. Predictive models and/or laws will be developed for pressure and temperature drop. Topological and parametric optimization will be carried out in an iterative way towards the most efficient model. Through sample tests and final element method, calculation correlations will be carried out to ensure the relevance and validity of the basic structural choices as well as their combinations. Targets: Delta temperature: 200°C to 400°C Flow: 0.01kg/s to 2kg/s Power: 0.5 to 500kW Reynolds number: 400 to 10000 Pressure drop: 100mBar max Size: up to 500x300x300mm

 Deliverables

List of deliverables.
Data management plan Open Research Data Pilot 2020-01-14 15:00:52
State of the art and its interpretation “word file” – Bibliography report Documents, reports 2020-01-14 14:59:42

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

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

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