HELICOPTER LANDING GEAR WITH A FIBER-REINFORCED, COMPOSITE, STRUCTURAL MEMBER EXHIBITING NON-LINEAR STRAIN-TO-FAILURE

HELICOPTER LANDING GEAR WITH A FIBER-REINFORCED, COMPOSITE, STRUCTURAL MEMBER EXHIBITING NON-LINEAR STRAIN-TO-FAILURE

A fiber-reinforced, organic matrix, composite structural member includes a plurality of layers of fiber-reinforced, organic matrix, composite material in which adjacent layers are bonded to one another, wherein the structural member exhibits a non-linear stress-strain response when mechanically load...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: DERISI, BIJAN, HOA, SUONG, VAN, HOJJATI, MEHDI, FEWS, ROBERT, CLIVE
Format: Patent
Sprache:eng ; fre ; ger
Schlagworte:
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Beschreibung
Zusammenfassung:A fiber-reinforced, organic matrix, composite structural member includes a plurality of layers of fiber-reinforced, organic matrix, composite material in which adjacent layers are bonded to one another, wherein the structural member exhibits a non-linear stress-strain response when mechanically loaded to failure. A helicopter landing gear includes a pair of skids and one or more cross members extending between the pair of skids. The one or more cross members includes a plurality of layers of fiber-reinforced, organic matrix, composite material in which adjacent layers are bonded to one another, wherein the cross members exhibit non-linear stress-strain responses when mechanically loaded to failure.