ELADINE: sensor monitoring and numerical model approach for composite material wing box shape distortions prediction

Out-of-Autoclave technologies are emerging as cost-effective alternatives to autoclave cure prepreg. However, their implementation in aerospace industry is still presenting many challenges. A common problem is the shape distortions that results in geometry mismatches with the tool. A way to avoid th...

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Bibliographic Details
Published in:IOP conference series. Materials Science and Engineering 2022-02, Vol.1226 (1), p.12001
Main Authors: Torre-Poza, A, Pinto, A M R, Grandal, T, González-Castro, N, Carral, L, Travieso-Puente, R, Rodríguez-Senín, E, Banu, C, Paval, A, Bocioaga, M, Firtat, L
Format: Article
Language:English
Subjects:
Aerospace industry
Autoclaves
Bragg gratings
Composite materials
Composite wings
Finite element method
Manufacturing
Mathematical models
Numerical models
Sensors
Wing boxes
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Summary:Out-of-Autoclave technologies are emerging as cost-effective alternatives to autoclave cure prepreg. However, their implementation in aerospace industry is still presenting many challenges. A common problem is the shape distortions that results in geometry mismatches with the tool. A way to avoid this and ensure a good final quality part is identifying the mechanisms that induce these deformations and optimize the manufacturing process of each component with the aim of reducing the production of faulty parts. The main objective of ELADINE project is to provide a method for shape distortions prediction on composite integral structures using an experimental-numerical approach. Different manufacturing parameters were monitored using Fiber Bragg Grating (FBG) sensors and DC-dielectric (DC) sensors and the resulting part geometry was examined by means of 3D coordinate analysis. The study performed for LRI (Liquid Resin Infusion) manufactured parts and the scenarios considered for the calibration of a Finite Element Method (FEM) based simulation tool are presented in the article. The resulting model will be implemented in a sub-scale demonstrator and, eventually, in a full 7-meter composite wing-box.
ISSN:1757-8981
1757-899X
DOI:10.1088/1757-899X/1226/1/012001