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.


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    Title :

    Rotor including a lead/lag abutment mechanism, and an aircraft


    Contributors:

    Publication date :

    2015-11-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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