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FLEXOP

Financiado

Cerrado

Flutter Free FLight Envelope eXpansion for ecOnomical Performance improvement

The FLEXOP project is about developing multidisciplinary aircraft design capabilities for Europe that will increase competitiveness with emerging markets -particularly in terms of aircraft development costs. A closer coupling of w... ver más

30/11/2019

HUN-REN SZTAKI

7M€

Presupuesto del proyecto: 7M€

Líder del proyecto

HUNREN SZAMITASTECHNIKAI ES AUTOMATIZALASI KU... No se ha especificado una descripción o un objeto social para esta compañía.

TRL 4-5

Fecha límite participación Sin fecha límite de participación.

Ver 10 Participantes

Financiación concedida El organismo H2020 notifico la concesión del proyecto el día 2019-11-30

MG-1.1-2014: Competitiveness of European Aviatio... Scope:Specific challenge: The aviation sector contributes 2% to the EU GDP. It is also an important...

I+D

Cerrada hace 11 años

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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.

10 Participantes

HUN-REN SZTAKI

980.80K€ | Lider

UNIVERSITY OF BRISTOL

643.47K€ | Participante

AIRBUSGROUP LIMITED

282.15K€ | Participante

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Duración del proyecto: 55 meses Fecha Inicio: 2015-04-20
Fecha Fin: 2019-11-30

Líder del proyecto

HUNREN SZAMITASTECHNIKAI ES AUTOMATIZALASI KU... No se ha especificado una descripción o un objeto social para esta compañía.

TRL 4-5

Presupuesto del proyecto 7M€

Fecha límite de participación Sin fecha límite de participación.

Descripción del proyecto The FLEXOP project is about developing multidisciplinary aircraft design capabilities for Europe that will increase competitiveness with emerging markets -particularly in terms of aircraft development costs. A closer coupling of wing aeroelasticity and flight control systems in the design process opens new opportunities to explore previously unviable designs. Common methods and tools across the disciplines also provide a way to rapidly adapt existing designs into derivative aircraft, at a reduced technological risk (e.g. using control to solve a flutter problem discovered during development). The goal will be achieved by: (a) improving efficiency of currently existing wing, by increased span at no excess structural weight, while establishing modifications by aeroelastic tailoring to carry the redesigned derivative wing; (b) developing methods and tools for very accurate flutter modeling and flutter control synthesis, to enable improved flutter management during development, certification, and operation, enabling to fly with the stretched wing at same airspeed as the baseline aircraft; (c) validating the accuracy of developed tools and methods on an affordable experimental platform, followed by a scale-up study, demonstrating the interdisciplinary development cycle. Manufacturers will gain cost efficient methods, tools and demonstrators for enhancing aircraft performance by integrated development of flutter control and aeroelastic tailoring. These inter-disciplinary capabilities will improve the design cycle and the Verification& Validation process of both derivative and new aircraft. Better control of development and certification costs can be achieved if these capabilities are used to address problems early in the design process. Flight test data will be posted on the project website to provide a benchmark for the EU aerospace community. The project’s results will serve as a preliminary outlining of certification standards for future EU flexible transport aircraft.

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