发明名称 Incremental optical coder for aircraft control panel
摘要 The coder has two coaxial control axes (2, 3). The first axis is a cylindrical rod which is engaged by the second axis with a tubular shape. Both axes are made of nickel-chrome steel. A coding disc (10A) is attached to the first axis, while a second disc (10B) is attached to the second axis. Both disc are made of aluminium. The axes are placed in a casing (45) which houses a PCB (11). Situated between the two discs. The PCB presents a number of emitter-receiver pairs (40, 60) which transmit/receive optical signals coded by the two discs.
申请公布号 FR2765679(A1) 申请公布日期 1999.01.08
申请号 FR19970008268 申请日期 1997.07.01
申请人 CELERC MICROTECHNIQUES 发明人 POUZAINT ROGER
分类号 G01D5/347;(IPC1-7):G01D5/34 主分类号 G01D5/347
代理机构 代理人
主权项
地址