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BISANCE

financed

Biphasic Heat Transport integration for efficient heat exchange within Composite...

Biphasic Heat Transport integration for efficient heat exchange within Composite materials Nacelle BISANCE intends at defining a biphasic system integrated into a full composite nacelle and engine air intake. The biphasic system aims at decreasing significantly the weight, the environmatal footprint as well as the space allocat... see more

31/05/2023

SONACA SA

843K€

Project Budget: 843K€

Project leader

SOCIETE NATIONALE DE CONSTRUCTION AEROSPATIAL... No se ha especificado una descripción o un objeto social para esta compañía.

TRL 4-5

PARTICIPATION DEPralty Sin fecha límite de participación.

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Financing granted El organismo H2020 notifico la concesión del proyecto The day 2023-05-31

JTI-CS2-2018-CFP09-AIR-02-69: Biphasic Heat Transport Integration... Specific Challenge:The topic scope is to validate the technology required for the integration of a c...

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Este proyecto no cuenta con búsquedas de partenariado abiertas en este momento.

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3 Participantes

SONACA SA

460.00K€ | Leader

RTA RAIL TEC ARSENAL FAHRZEU...

140.00K€ | participant

CALYOS SA

243.31K€ | participant

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Project duration: 44 months Date Start: 2019-09-24
End date: 2023-05-31

Project leader

SOCIETE NATIONALE DE CONSTRUCTION AEROSPATIAL... No se ha especificado una descripción o un objeto social para esta compañía.

TRL 4-5

Project Budget 843K€

participation deadline Sin fecha límite de participación.

Project description BISANCE intends at defining a biphasic system integrated into a full composite nacelle and engine air intake. The biphasic system aims at decreasing significantly the weight, the environmatal footprint as well as the space allocated by the current active systems for the cooling of the engine oil and for the energy supply of th ice protection systems. These both active systems (needing external power) will be replaced by a biphasic passive system (autonomous with no need of external power) which will extract the energy from the engine oil and transfer it to the ice protected surfaces. The objective of the project is thus to decrease the weight by 25kg for the two nacelles of a turboprop A/C, to decrease the CO2 emissions by almost 900 000 kg per AC life and to save 200 000$ of operating costs per AC life. The project will be divided into 5 workpackages along 30 months. The first step intends at defining the specifications and the requirements of the product. Based on the requirements, several concepts of system integration into the structure will be proposed and manufactured for selecting the most promising one. Qualification tests are expected for characterizing the structural resistance and stifness of the concept, for verifying the resistance to heat cycles and to impacts. Finally a fulls scale demonstrator will be manufactured for testing it in icing Wind tunnel. The project will be coordinated by Sonaca, also in charge of the structural developments, in association with Calyos, in charge of the system developments and with RTA in charge of performing the icing wind tunnel testing.

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