发明名称 Aircraft control lever vernier
摘要 According to the present invention, there is provided an aircraft control including a control lever having a handle and a base, where the base is operatively mountable for movement between predetermined control lever positions, and a vernier adjusting mechanism for incrementally displacing the control lever between the positions. Additionally, the present invention provides for a vernier adjusting mechanism including a friction drive mechanism for finely adjusting the control lever's position.
申请公布号 US6488239(B2) 申请公布日期 2002.12.03
申请号 US20010872371 申请日期 2001.06.01
申请人 SPITZER A. ROBERT 发明人 SPITZER A. ROBERT
分类号 B64C13/04;(IPC1-7):B64C13/28 主分类号 B64C13/04
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