Morphing structure for a wing leading edge

The wing leading edge (1) has a deformable shell (2), which is connected to a supporting structure (8) at its two ends (3,4). A fiber composite has a shear-flexible intermediate layer in an area of a neutral fiber of the shell. The shear-flexible intermediate layer is made from an elastomer material...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	KINTSCHER, MARKUS, HEINTZEOLAF
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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