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FLiPASED

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FLIGHT PHASE ADAPTIVE AERO SERVO ELASTIC AIRCRAFT DESIGN METHODS

Flight Phase Adaptive Aero-Servo-Elastic Aircraft Design Methods (FliPASED) opens a complete new dimension for the integrated aircraft design. Coupling between aeroelasticity, gust response, flight control methods, instrumentation... ver más

30/06/2023

HUN-REN SZTAKI

4M€

Presupuesto del proyecto: 4M€

Líder del proyecto

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

TRL 4-5

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Financiación concedida El organismo H2020 notifico la concesión del proyecto el día 2023-06-30

MG-3-1-2018: Multidisciplinary and collaborative... Specific Challenge:Maintaining and extending European industrial leadership, through embedding desig...

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

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5 Participantes

HUN-REN SZTAKI

1.09M€ | Lider

ENVASES TECNICOS ZARAGOZA

440.40K€ | Participante

ONERA

313.84K€ | Participante

DLR

969.34K€ | Participante

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Duración del proyecto: 49 meses Fecha Inicio: 2019-05-06
Fecha Fin: 2023-06-30

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 4M€

Fecha límite de participación Sin fecha límite de participación.

Descripción del proyecto Flight Phase Adaptive Aero-Servo-Elastic Aircraft Design Methods (FliPASED) opens a complete new dimension for the integrated aircraft design. Coupling between aeroelasticity, gust response, flight control methods, instrumentation and certification aspects is not exploited in current aircraft design. A common set of models, coupled with joint requirements enable a multidisciplinary-optimized design for the entire aircraft, leading to more optimized overall performance. The concept of exploiting coupling between disciplines will take advantage of tools developed by the partners in former projects. The main objectives of the proposal aim at tightly coupled multi-objective optimization of advanced, active controlled wing designs through the integration of a collaborative design tool chain. More than 10% fuel efficiency improvement, and 20% reduction in peak amplitude of the gust response, as well as a 50% reduction of number of distinct models used during the development and certification process are set as project goals. Through the integration of all discipline tools from aerodynamics, structural design, aeroelastic simulation and control design in one integrated tool chain an active, condition optimized wing design becomes feasible, enabling enhanced performance at lower weight and cost. The project will raise the efficiency of a currently separately existing development toolchains, by advanced multidisciplinary and collaborative capabilities for whole aircraft along its life cycle. It will develop methods and tools for very accurate flexible-mode modelling and flexible aircraft control synthesis, in the context of reliable implementation of the avionics system, taking into consideration the fault detection and reconfiguration. The accuracy of developed tools and methods will be validated on a safe and affordable experimental platform, and results will be shared along with design requirements and standardized interfaces in an open source approach.

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