Composite structural part

Composite structural part

The part has multiple fiber layers oriented with respect to longitudinal direction (2) of the part. One of the fiber layers is constituted of continuous fibers extending from one edge to another edge of the part on a surface of the part, where thickness of the part is constant. The fiber layers are...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: GUILLEMAUT, JULIEN, SOULA, DENIS
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
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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Beschreibung
Zusammenfassung:The part has multiple fiber layers oriented with respect to longitudinal direction (2) of the part. One of the fiber layers is constituted of continuous fibers extending from one edge to another edge of the part on a surface of the part, where thickness of the part is constant. The fiber layers are formed as a lay-up with multi-axes (110, 140, 150), where the multi-axes are arranged in a central part of the structural part. An independent claim is also included for a center wing box of an aircraft comprising a spar.