发明名称 COMMAND BAR MECHANISM FOR FLIGHT DIRECTOR INDICATOR AIRCRAFT INSTRUMENT
摘要 A compact positioning mechanism for an indicator assembly of the type comprising first and second bar members arranged in a V-like configuration and collectively defining a command plane which is both rotatable about and transversely displaceable with respect to a reference axis. A pair of ring members, each formed with a camming surface, carry the respective bar members on a cam follower pivotably mounted on one ring and in camming engagement with the cam surface on the other. Rotation of the command plane is achieved through like rotation of the two rings while displacement transverse of the reference axis is achieved by relative rotation between the two rings.
申请公布号 US3654597(A) 申请公布日期 1972.04.04
申请号 USD3654597 申请日期 1970.08.07
申请人 COLLINS RADIO CO. 发明人 RONALD E. COX
分类号 G01C19/32;G01C23/00;(IPC1-7):G08G5/02 主分类号 G01C19/32
代理机构 代理人
主权项
地址