发明名称 Control mechanism.
摘要 <p>A control mechanism for a displaceable control member such as an aircraft pilot's "joystick" includes an array of pressure transducers (20) in contact with a pressure plate (22) which in turn is in pivotal connection with the control member (10) operated by the pilot. Adjustable springs (26) bias the pressure plate (22) towards the transducers (20). Pivotal movement of the control member (10) tends to compress the springs (26) and to cause the transducers (20) to generate output signals representative of differential pressure. The signals are then processed by circuitry (34) to provide inputs to flight control computers. <IMAGE></p>
申请公布号 EP0438919(A2) 申请公布日期 1991.07.31
申请号 EP19900314347 申请日期 1990.12.27
申请人 BRITISH AEROSPACE PLC 发明人 KAYE, ARTHUR
分类号 B64C13/04;G01L5/22;G05G9/047 主分类号 B64C13/04
代理机构 代理人
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