Descripción del proyecto
Un enfoque integrado para el diseño de alas de aviones controladas de forma activa
El proyecto FLiPASED, financiado con fondos europeos, tiene como objetivo revolucionar las alas de los aviones, desarrollando y probando el llamado diseño de ala de control activo. Este concepto de cambio de forma de las alas puede reducir la repercusión de las ráfagas en el rendimiento aerodinámico en un 20 % y el consumo de combustible en un 10 %. Además, puede reducir a la mitad la cantidad de modelos distintos utilizados durante el proceso de desarrollo y certificación de aeronaves. El proyecto combinará modelos de diseño aerodinámico, estructural, aeroelástico y de control en una cadena de herramientas integrada para optimizar el diseño del ala. Las herramientas se validarán en una plataforma experimental segura y asequible. Los resultados experimentales junto con los requisitos de diseño se publicarán sin trabas.
Objetivo
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.
Ámbito científico
Palabras clave
Programa(s)
Convocatoria de propuestas
Consulte otros proyectos de esta convocatoriaConvocatoria de subcontratación
H2020-MG-2018-TwoStages
Régimen de financiación
RIA - Research and Innovation actionCoordinador
1111 Budapest
Hungría