发明名称 Aircraft control surface actuating linkage
摘要 A force transmission part (22) provided with vanes is placed on a cylindrical rod (20). The part is formed from three vanes connected at their ends and a pair of star shaped elements which connect the vanes. The part allows the rod to transmit to webs (24) supported on its ends a radial force applied to the rod center by an activator, while minimizing the mass for a given gap of the webs.
申请公布号 EP1201537(A1) 申请公布日期 2002.05.02
申请号 EP20010402771 申请日期 2001.10.25
申请人 AIRBUS FRANCE 发明人 MILLIERE, JEROME
分类号 B64C9/02;B64C13/24;F16C11/04 主分类号 B64C9/02
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