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Opendata, web and dolomites

NATHENA SIGNED

New Additive manufacTuring Heat ExchaNger for Aeronautic

Total Cost €

EC-Contrib. €

Partnership

Views

Outcomes and
results

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.

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

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 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.	FR (BLAGNAC)	coordinator	416˙912.00
2	ADDUP ADDUP Organization address address: 5 RUE BLEUE ZONE INDUSTRIELLE DE LADOUX city: CEBAZAT postcode: 63118 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.	FR (CEBAZAT)	participant	388˙440.00
3	INSTITUT VON KARMAN DE DYNAMIQUE DES FLUIDES INSTITUT VON KARMAN DE DYNAMIQUE DES FLUIDES Organization address address: CHAUSSEE DE WATERLOO 72 city: RHODE SAINT GENESE postcode: 1640 website: www.vki.ac.be contact info title: n.a. name: n.a. surname: n.a. function: n.a. email: n.a. telephone: n.a. fax: n.a.	BE (RHODE SAINT GENESE)	participant	367˙600.00
4	TEMISTH SAS TEMISTH SAS Organization address address: 45 rue Frédéric Joliot-Curie city: MARSEILLE postcode: 13382 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.	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 â€œword fileâ€ â€“ 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.