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(11) | EP 0 256 648 A3 |
(12) | EUROPEAN PATENT APPLICATION |
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(54) | Hydraulic control system |
(57) An hydraulic control system, for example for use in moving control surfaces of aircraft,
comprises first and second actuators (12A, 12B) operating in tandem. The two actuators
are supplied by independent hydraulic pathways (P1, P2), the fluid in each of these
pathways being controlled by a plurality of direct drive control valves (4) connected
across the two pathways. The system will therefore operate even if three of the control
valves, and one of the hydraulic supplies are non-operational. |