A method for relieving kinematic binding and oscillatory drive forces in a rotor head of a rotary-wing aircraft

A torque coupling (13) for a rotor head (11) of a rotary-wing aircraft has upper and lower plates (29, 31) configured for rotation with a rotor mast (19). Drive links (33) pivotally connected to the upper and lower plates (29, 31) pivot about a pivot axis generally parallel to and radially offset fr...

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Bibliographische Detailangaben

Hauptverfasser:	STAMPS, FRANK, RAUBER, RICHARD
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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