DUAL-CONCENTRIC CONTROL VALVE WITH DIRECT DRIVE CONTROL AND FAILED MOTOR PROTECTION

The present disclosure relates to a dual-concentric control valve with direct drive control and failed motor protection. Systems and methods include providing an aircraft with a direct drive dual-concentric valve (D3V) having a body, an outer secondary spool coaxially located within a bore of the bo...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	ATKINS BRADY GARRETT, COVINGTON CHARLES ERIC, FENNY CARLOS ALEXANDER, REYNOLDS ROBERT PAUL
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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