COMPOSITE PANEL SYSTEMS AND METHODS

A composite panel assembly and method of forming the same includes a core (102), an inner skin (104, 106) coupled to a first side (106) of the core (102) and an outer skin (108) coupled to a second side (110) of the core (102). A peripheral edge including portions of the core (102), the inner skin (...

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Bibliographic Details
Main Author SWITZER, Lon E
Format Patent
LanguageEnglish
French
German
Published 28.10.2020
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
LAYERED PRODUCTS
LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM
PERFORMING OPERATIONS
TRANSPORTING
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Summary:A composite panel assembly and method of forming the same includes a core (102), an inner skin (104, 106) coupled to a first side (106) of the core (102) and an outer skin (108) coupled to a second side (110) of the core (102). A peripheral edge including portions of the core (102), the inner skin (104), and the outer skin (108), is compressed to close a path into the core.
Bibliography:Application Number: EP20200170227