Composite panel and aircraft turbojet engine nacelle comprising such a panel

Number of patents in Portfolio can not be more than 2000

United States of America Patent

PATENT NO 10746130
APP PUB NO 20180066608A1
SERIAL NO

15810267

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Abstract

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The present disclosure relates to a composite panel having a sandwich structure formed by a central core having a primary cellular structure, for example, of the honeycomb type, sandwiched between two skins. The primary cellular structure includes an array of main cells. The composite panel further includes a plurality of pins, each pin being, on the one hand, arranged to be housed and to cooperate inside a main cell and, on the other hand, formed of a secondary cellular structure having an array of secondary cells.

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Patent Owner(s)

Patent OwnerAddress
SAFRAN NACELLESGONFREVILLE-LA ROCHELLE FRANCE SEVRES HAUTS-DE-SEINE

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Bienvenu, Philippe Gonfreville l'Orcher, FR 28 97
Lefebvre, Michel Gonfreville l'Orcher, FR 36 297
Rivoal, Jean-Claude Gonfreville l'Orcher, FR 5 22

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