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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.

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

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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