A rotor having a hub and a plurality of lift assemblies, the rotor having one lead/lag abutment mechanism per lift assembly. Each abutment mechanism includes an elastomer spacer strip and two C-shaped metal clips engaged respectively on a first base and on a second base of the strip. Two fastener pins each pass through a clip and the longitudinal projections of a base and through an orifice in the hub.
ROTOR INCLUDING A LEAD/LAG ABUTMENT MECHANISM, AND AN AIRCRAFT
2015-10-29
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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