F - Mech Eng,Light,Heat,Weapons – 15 – B
Patent
F - Mech Eng,Light,Heat,Weapons
15
B
341/103
F15B 9/03 (2006.01) F15B 9/09 (2006.01) F15B 18/00 (2006.01) G05B 9/03 (2006.01) G05D 1/00 (2006.01)
Patent
CA 1197918
MULTIPLE LOOP CONTROL SYSTEM ABSTRACT OF THE DISCLOSURE A redundant, dual-fail/operate fly-by-wire control system actuates a redundant tandem piston actuator (10) to provide a single composite output evidenced by movement of a piston rod (12). The basic fault-tolerate actuation system consists of dual hydraulic primary actuators, quadruplex electrical control loops (14-17), and control servo valves (22-25). A failure management system connects to the actuation system by means of lines (18-21) to control the servo valves (22-25). The four control loops (14-17) connect to a pilot controller that provides pilot individual input signals to amplifiers (26-29) for each of the control loops.
396332
Haskins Delbert E. Jr.
Murphy Milford R.
Bell Helicopter Textron Inc.
Kirby Eades Gale Baker
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