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AEROL-HP

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Cerrado

Development construction integration and progress toward to two phase device...

Development construction integration and progress toward to two phase device monitoring and qualification on aircrafts The proposed project is part of the Cleansky Eco-Design activities for the all (or more) electric aircrafts. The main targets of the call are related to improved aircraft weight, improved electronic equipment life cycles & reduced... ver más

31/12/2014

EHP

360K€

Presupuesto del proyecto: 360K€

Líder del proyecto

EURO HEAT PIPES SA No se ha especificado una descripción o un objeto social para esta compañía.

TRL 4-5

Fecha límite participación Sin fecha límite de participación.

Financiación concedida El organismo FP7 notifico la concesión del proyecto el día 2014-12-31 No tenemos la información de la convocatoria

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Características del participante

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

Información adicional privada

No hay información privada compartida para este proyecto. Habla con el coordinador.

1 Participantes

EHP

0.00€ | Lider

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Líder del proyecto

EURO HEAT PIPES SA No se ha especificado una descripción o un objeto social para esta compañía.

TRL 4-5

Presupuesto del proyecto 360K€

Fecha límite de participación Sin fecha límite de participación.

Descripción del proyecto The proposed project is part of the Cleansky Eco-Design activities for the all (or more) electric aircrafts. The main targets of the call are related to improved aircraft weight, improved electronic equipment life cycles & reduced maintenance thanks to the use of highly efficient passive (green) thermal control systems (as already used on satellite systems). Technical objectives: The EHP proposal is part of the ECO-Design ITD and will address the development, and qualification aspects of highly efficient two-phase cooling devises such as heat pipes and loop heat pipes to be used on board of aeronautical aircrafts. The main objectives are : • Qualify two-phase heat transfer devises in accordance with specific aeronautical requirements such as : o High acceleration loads o Long duration vibration stresses • Reduce global aircraft weight at equipment and/or system level => reduce aircraft consumption and increase operating range • Lower impact on environment through the use of passive and maintenance free thermal equipments • Increase reliability of controlled equipment (power electronics) => decrease repair and maintenance aspects The Ammonia HP and LHP products are today baselined (with a TRL 9) on all Space satellites or payloads thanks to the reliable capability provided by these isothermal lightweight thermal management devises. Non-space applications are also more and more considered for these two-phases devises to be used on high power electronic (railway applications) or primary flight control actuators. The AeroL-HP products will be developped up to CDR level with qualification of the two-phase hardware. From a technical side, the proposed thermal link will have to provide a reliable and competitive (generic, modular and low cost) product (Rejected power/mass). The thermal link will be a scalable system able to address payload dissipations from 30W (TBC) up to 900W (or higher).

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