NATURAL LAMINAR FLOW WINGTIP

A method comprises forming a wing tip device of an aircraft. The wing tip device, once formed, comprises a unitized, monolithic leading edge torque box. The forming comprises: forming the unitized, monolithic leading edge torque box of the wing tip device using a pair of rigid soluble mandrels which...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	CAMPBELL, DARRELL D, LYONS, BRETT I
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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