HINGED COMPOSITE SANDWICH PANELS

HINGED COMPOSITE SANDWICH PANELS

An apparatus comprises a composite sandwich panel (100), a seal (110), and a hinge (112). The composite sandwich panel has a first edge (104) in a first over-crush edge region (106), wherein a thickness (108) of the composite sandwich panel decreases within the first over-crush edge region in a dire...

Ausführliche Beschreibung

Gespeichert in:
Bibliographische Detailangaben
Hauptverfasser: Swanson, Kevin G, Turner, Jason, Young, Stephen M, Egging, Duane M
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:An apparatus comprises a composite sandwich panel (100), a seal (110), and a hinge (112). The composite sandwich panel has a first edge (104) in a first over-crush edge region (106), wherein a thickness (108) of the composite sandwich panel decreases within the first over-crush edge region in a direction towards the first edge. The seal is bonded to the first over-crush edge region of the composite sandwich panel and extending past the first edge. The hinge is connected to the composite sandwich panel such that an axis of rotation (114) of the hinge is positioned over the first over-crush edge region of the composite sandwich panel.