发明名称 Actuator system for aerospace controls and functions
摘要 The invention provides an actuator (12) having a piston (18) moveable within a cylinder (20), and a piston rod (22) extending from the piston and providing an actuator ram (14). The piston divides the cylinder into a cylindrical chamber (24) and an annular chamber (26), and a fluid direction control valve (34) controls the supply of fluid between these chambers and a fluid supply line (30) and a fluid return line (32). The actuator is arranged to have first and second modes of operation during extension of the piston rod, the actuator in the first mode having the fluid supply line in communication with the cylindrical chamber and the annular chamber in communication with the fluid return line and in the second mode having the fluid supply line in communication with the cylindrical chamber and the annular chamber connected directly or indirectly to the cylindrical chamber. The actuator system also includes means (36, 38; 102, 104, 106) for automatically switching the actuator from one mode to the other mode.
申请公布号 AU4381499(A) 申请公布日期 2000.01.10
申请号 AU19990043814 申请日期 1999.06.17
申请人 BRITISH AEROSPACE PLC 发明人 ANDREW EDWARD UTTLEY
分类号 B64C13/40;F15B11/024 主分类号 B64C13/40
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