Anti-rotation clip

The present invention is for an improved rotating control system for use on tilt rotor aircraft and helicopters. Existing rotating control systems usually include a non-rotating swashplate and a rotating swashplate, both swashplates having a plurality of clevises, each clevis formed by at least two...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	ZIERER JOSEPH J, DAY CLIFTON B, COVINGTON C. ED
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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