发明名称 |
A rotor including a lead/lag abutment mechanism, and an aircraft. |
摘要 |
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. |
申请公布号 |
EP2937282(B1) |
申请公布日期 |
2016.07.13 |
申请号 |
EP20150155949 |
申请日期 |
2015.02.20 |
申请人 |
AIRBUS HELICOPTERS |
发明人 |
MAZET, STÉPHANE;BENCARDINO, SANDRA |
分类号 |
B64C27/32;B64C27/51;B64C27/54 |
主分类号 |
B64C27/32 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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