发明名称 Rotation lock mechanism for aircraft seat
摘要 A braking mechanism to control rotational movement of a seat is disclosed. The braking mechanism may comprise a circular member (e.g., a disc or ring) that is coupled to a base assembly and a caliper, coupled to a seat assembly, to engage the circular member. In a biased position, a braking element of the caliper applies a braking force to the circular member. A user can reduce the braking force by increasing the tension on a cable coupled to the caliper. Once the braking force is sufficiently reduced, the user may rotate the seat until the desired rotational orientation is attained. Upon release of the cable, the braking mechanism re-engages to prevent further rotational movement.
申请公布号 US2004195886(A1) 申请公布日期 2004.10.07
申请号 US20030409976 申请日期 2003.04.07
申请人 BEATTY GEORGE T.;HEMMER NATHAN A.;TRAUBE JOHN H.;HUTCHISON CARL R. 发明人 BEATTY GEORGE T.;HEMMER NATHAN A.;TRAUBE JOHN H.;HUTCHISON CARL R.
分类号 B60N2/06;B60N2/14;B60N2/44;B64D11/06;(IPC1-7):A47C1/032 主分类号 B60N2/06
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