发明名称 AIRCRAFT BRAKE ACTUATOR ASSEMBLIES
摘要 The present disclosure provides an actuator assembly comprising a ballnut (110) having a helical track (112), an actuator drive unit ("ADU") housing (140) having an ADU track (141), and a ballscrew (220). In various embodiments, the ballscrew (220) comprises a first translation bearing track (222), wherein the helical track (112) and the first translation bearing track (222) form a first translation bearing raceway (451) in which a plurality of first translation bearing balls (421) having a first diameter are disposed, and a second translation bearing track (224), wherein the helical track (112) and the second translation bearing track (224) form a second translation bearing raceway (452) in which a plurality of second translation bearing balls (422) having a second diameter are disposed, wherein the first diameter and the second diameter are not equal.
申请公布号 EP3121476(A1) 申请公布日期 2017.01.25
申请号 EP20160180575 申请日期 2016.07.21
申请人 Goodrich Corporation 发明人 REHFUS, Kevin;DRENNEN, David;KLODE, Harald
分类号 F16D65/18;B60T7/10;B60T13/74;F16H25/22 主分类号 F16D65/18
代理机构 代理人
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