This is a report of design study on Dual-Mode Dynavector Actuator for use as control-surface actuator on aircraft. Actuator operates on pneumatic power and /or electric power. Operation within specifications continues despite loss of either electric or pneumatic power, providing survivability feature for aircraft. (Author)
Advanced Flight Control Actuation System (AFCAS-E/P). Feasibility Investigation of an Electro/Pneumatic Dual Power Driven Concept
1978
118 pages
Report
No indication
English
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