Devices and methods to structurally close and seal openings in an aircraft wing fuel tank

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Devices and methods to structurally close and seal openings in an aircraft wing fuel tank

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VILAS BOAS ALBERTO VILAR / DA SILVA DANIEL GONÇALVES / MARTINS GUSTAVO DEDDING / DE OLIVEIRA JULIANO / MARTINS LUCIANO ALVES / SUZUKI LUIZ GUSTAVO / CORREA ROBSON GARCIA / SAMPAIO SOARES VITOR JULIANO / VERRI WAGNER GARCEZ

Abstract

Closure devices and methods are provided for closing a stringer penetration space defined between a stringer and a wing rib of an aircraft wing section. According to certain embodiments, the closure devices will integrally include a forward face plate positioned in covering relationship to at least a portion of the stringer penetration space, and a rearwardly projecting attachment arm rigidly adapted for rigid attachment to the stringer so as to positionally fix the forward face plate relative to the stringer penetration space.

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Titel :

Devices and methods to structurally close and seal openings in an aircraft wing fuel tank

Beteiligte:

VILAS BOAS ALBERTO VILAR (Autor:in) / DA SILVA DANIEL GONÇALVES (Autor:in) / MARTINS GUSTAVO DEDDING (Autor:in) / DE OLIVEIRA JULIANO (Autor:in) / MARTINS LUCIANO ALVES (Autor:in) / SUZUKI LUIZ GUSTAVO (Autor:in) / CORREA ROBSON GARCIA (Autor:in) / SAMPAIO SOARES VITOR JULIANO (Autor:in) / VERRI WAGNER GARCEZ (Autor:in)

Erscheinungsdatum :

2023-01-24

Medientyp :

Patent

Format :

Elektronische Ressource

Sprache :

Englisch

Klassifikation :

IPC:

B64C AEROPLANES , Flugzeuge

Devices and methods to structurally close and seal openings in an aircraft wing fuel tank

Devices and methods to structurally close and seal openings in an aircraft wing fuel tank

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