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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.

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

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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