Design of a Leading Edge Morphing Based on Compliant Structures in the Framework of the CS2-AIRGREEN2 Project

A. Gaspari, A. Gilardelli, S. Ricci, A. Airoldi, F. Moens
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引用次数: 5

Abstract

This paper summarizes the results obtained in the framework of Clean Sky 2 REG-IADP, AIRGREEN on the development of a dedicated morphing device, i.e. a Leading Edge morphing. This device, designed so to be installed on a advanced, twin prop, regional aircraft, is conceived to guarantee high lift conditions together with a smoothed and continuous skin surface, especially important due to the presence of a laminar wing. The design of a such as complex devices required a multi-disciplinary approach, able to combine the aerodynamic performances and the structural ones related to the compliant structures concept adopted for the internal structure. The paper includes an overview of all the design challenges, the adopted solutions and finally the obtained numerical assessments.
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CS2-AIRGREEN2项目框架下基于柔性结构的前缘变形设计
本文总结了在Clean Sky 2 regg - iadp, AIRGREEN框架下关于专用变形装置(Leading Edge morphing)研制的研究成果。该装置的设计目的是安装在先进的双支柱支线飞机上,旨在保证高升力条件以及光滑连续的表面,特别是由于层流机翼的存在,这一点尤为重要。如此复杂的装置的设计需要多学科的方法,能够将气动性能和与内部结构所采用的柔性结构概念相关的结构性能结合起来。本文概述了所有的设计挑战,采用的解决方案,最后得到了数值评估。
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