发明名称 Trim tab control mechanism
摘要 Apparatus for controlling the movement and positioning of an aircraft trim tab comprising: an elongated stabilizer member mounted in the cockpit of the aircraft for reciprocal forward and aft movement and having a threaded portion thereon; a cable member connecting the stabilizer member to the trim tab for movement and positioning thereof in response to reciprocal movement of the stabilizer member; and a control member threadedly engaging the threaded portion of the stabilizer member and manually engageable and rotatable from inside the cockpit for translating rotation of the control member to reciprocal movement of the stabilizer member.
申请公布号 US4175721(A) 申请公布日期 1979.11.27
申请号 US19770811907 申请日期 1977.06.30
申请人 LEMPA, BERNARD J JR 发明人 LEMPA, BERNARD J JR
分类号 B64C13/04;B64C13/30;(IPC1-7):B64C13/04 主分类号 B64C13/04
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