发明名称 Electric actuator for aircraft flight control
摘要 The invention relates to an actuator (9) comprising a rotary electric motor (12) a screw Old) driven in rotation by the motor, a mechanical member (15) driven in translation by the screw, a first position sensor (40) sensitive to a position of the electric motor and/or of the screw, a second position sensor (41) sensitive to a position of the mechanical member, and a servo-control circuit (11) connected to both of the position sensors and to the motor, this circuit delivering a power supply signal to the motor that varies as a function of a position setpoint signal (23) and as a function of signals delivered by the two position sensors; the second position sensor presents a resolution that is at least equivalent to the resolution of the first position sensor, and the servo-control circuit includes redundant modules (19, 22) for calculating the position of the mechanical member as a function of the signals/data delivered by the two sensors, together with at least two modules (17, 18) for mutual surveillance of the results delivered by the calculation modules.
申请公布号 US7764035(B2) 申请公布日期 2010.07.27
申请号 US20080031059 申请日期 2008.02.14
申请人 EUROCOPTER 发明人 KIRCHHOFER ALAIN;HONNORAT OLIVIER
分类号 G05D3/00 主分类号 G05D3/00
代理机构 代理人
主权项
地址