COMPOSITE PANEL WITH REINFORCING PINS

The invention relates to a composite panel comprising a first skin, a second skin, a core arranged between the first skin and the second skin, a plurality of reinforcing pins (11, 12) connected by a first end to the first skin and connected by a second end to the second skin, in which a plurality of...

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Bibliographische Detailangaben
Hauptverfasser:	Weber, Markus J, Dr. Endres, Gregor Christian, Neumann, Ulf Henning
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AFTER-TREATMENT OF THE SHAPED PRODUCTS, e.g. REPAIRING 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 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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Beschreibung
Zusammenfassung:	The invention relates to a composite panel comprising a first skin, a second skin, a core arranged between the first skin and the second skin, a plurality of reinforcing pins (11, 12) connected by a first end to the first skin and connected by a second end to the second skin, in which a plurality of inclined reinforcing pins (12) form an angle comprised between 25 degrees and 45 degrees with the first skin and/or the second skin.