The invention discloses a rotor (2) having a hub (3) and a plurality of lift assemblies (10). Each lift assembly (10) of the rotor (2) has a maintaining and moving member (15). Each abutment mechanism (20) includes an elastomer spacer strip (30) and two C-shaped metal clips (40) engaged respectively on a first base (32) and on a second base (33) of the strip. Each of two fastener pins (50) passes through the corresponding clip (40) and the longitudinal projections (35, 36) of a base (32, 34) and through an orifice in the hub.
Rotor including a lead/lag abutment mechanism, and an aircraft
04.11.2015
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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