Electromechanical actuation of primary flight control surfaces has been demonstrated by the development of an integrated rotary hinge-line dual-redundant actuation unit. The controller power level of 30 amp at 270 vdc was demonstrated. Thermal characteristics of the motor and actuator were evaluated at ambient temperatures ranging from -65 F to 250 F. (Author)
Electromechanical Actuation Development
1980
122 pages
Report
No indication
English
Avionics , Aircraft , Actuators , Electromechanical devices , Fly by wire control , Flight control systems , Servomechanisms , Redundant components , Logic circuits , Pulse duration modulation , Electric motors , Permanent magnets , Actuation , Systems(Electromechanical) , Ambient temperatures , Brushes motors , Electromechanical actuators , Flight control surfaces , Dc motors , Power by wire control , Cobalt magnets
Electromechanical flight control actuation
Tema Archive | 1977
|Electromechanical Flight Control Actuation
SAE Technical Papers | 1977
|The Development of Electromechanical Actuation for Aircraft Systems
Emerald Group Publishing | 1987
|