CFRP fuselage frame fixed to vertical tail

The invention relates to a CFRP fuselage frame fixed to a vertical tail. A securing assembly for securing a vertical tail assembly to an aircraft includes a first lug member secured to the vertical tail assembly. The fixation assembly further includes a first U-joint member. The first U-joint member...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	DIEP PAUL BOTHELL, PHIYEN T PHAM
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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