STRUCTURAL EFFECT OF STAGGERED COMPOSITE REINFORCEMENTS WITHIN THE FIREWALL OF AN AIRCRAFT

VICTOR ALFONSO RAMIREZ ELÍAS; ALEJANDRO ESTEBAN RODRIGUEZ  SANCHEZ; ELIAS RIGOBERTO LEDESMA OROZCO; HILARIO HERNANDEZ MORENO; ERIK VARGAS ROJAS; LUIS FERNANDO  PUENTE  MEDELLIN; LUIS DAVID CELAYA  GARCIA

doi:https://doi.org/10.6036/9334

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STRUCTURAL EFFECT OF STAGGERED COMPOSITE REINFORCEMENTS WITHIN THE FIREWALL OF AN AIRCRAFT

SEPTEMBER 2019 - Volume: 94 - Pages: 486

DOI:

https://doi.org/10.6036/9334

Authors:

VICTOR ALFONSO RAMIREZ ELÍAS - ALEJANDRO ESTEBAN RODRIGUEZ SANCHEZ -

ELIAS RIGOBERTO LEDESMA OROZCO

- HILARIO HERNANDEZ MORENO - ERIK VARGAS ROJAS - LUIS FERNANDO PUENTE MEDELLIN - LUIS DAVID CELAYA GARCIA

Disciplines:

Materials technology (RESISTENCIA DE LOS MATERIALES )

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Key words:: Cortafuego, Compuestos, avión utilitario, Análisis Estructural, Método de elemento Finito, Análisis de Tsa-Wu, firewall, composites, utilitarian aircraft, structural analysis, finite element method, Tsai-Wu analysis.
Article type:: NOTA TECNICA / TECHNICAL NOTE
Section:: TECHNICAL NOTE

The performance of composite materials, such as high strength and low density, is ideal for aerospace applications. This paper presents the structural analysis of a component of a utility aircraft, the STELA M1. As this is still a prototype, the aim is to validate the resistance of its fuselage subjected first to static loads.

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