Co-Cured UV/Visible Light-Resistant Fiberglass Coated Composite Material for Aircraft Fuselage Assembly

Co-curable and co-cured UV/visible light-resistant fiberglass-coated UV/visible light composite structural material substrates, and aircraft fuselages comprising co-cured UV/visible light-resistant fiberglass-coated composite material substrates and methods of their manufacture are disclosed.

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Bibliographic Details
Main Authors Ackerman, Patrice K, Adjorlolo, Alain A, Bolles, Jason A
Format Patent
LanguageEnglish
Published 05.10.2023
Subjects
AEROPLANES
AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
SHAPING OF MATERIAL IN A PLASTIC STATE, NOT OTHERWISE PROVIDEDFOR
SHAPING OR JOINING OF PLASTICS
TRANSPORTING
WORKING OF PLASTICS
WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
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Summary:Co-curable and co-cured UV/visible light-resistant fiberglass-coated UV/visible light composite structural material substrates, and aircraft fuselages comprising co-cured UV/visible light-resistant fiberglass-coated composite material substrates and methods of their manufacture are disclosed.
Bibliography:Application Number: US202217708404