DE2141371

A multiple channel redundant electro-hydraulic servo system for controlling an aircraft guidance element. This system is redundant so that upon failure of one or more channels of the system, the remaining active channels still maintain control of the guidance element with a minimum of transient shif...

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Bibliographische Detailangaben
Hauptverfasser:	TRACZYK, EDMOND M., VAL MORIN, P.QUEBEC, WALKER, COLIN G., LAVAL, DARLINGTON, RALPH F., LACHINE, LEADBEATER, EDWARD J., MONTREAL
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION CONTROL OR REGULATING SYSTEMS IN GENERAL CONTROLLING COSMONAUTICS FUNCTIONAL ELEMENTS OF SUCH SYSTEMS HELICOPTERS MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS ORELEMENTS PERFORMING OPERATIONS PHYSICS REGULATING SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES TRANSPORTING
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Beschreibung
Zusammenfassung:	A multiple channel redundant electro-hydraulic servo system for controlling an aircraft guidance element. This system is redundant so that upon failure of one or more channels of the system, the remaining active channels still maintain control of the guidance element with a minimum of transient shift during shutdown of the failed channel.