Report of the fabrication and design verification testing of a Dual Mode Electro/Pneumatic Actuator. Pneumatic model open loop operation and control verified. Torque/Speed performance less than design goal due to excessive gear separation force. (Author)
Advanced Flight Control Actuation System (AFCAS - E/P). Fabrication and Design Verification Testing of a Dual Mode Electro/Pneumatic Actuator for the T-2C Aircraft
1982
55 pages
Report
Keine Angabe
Englisch
Aircraft , Avionics , Flight control systems , Pneumatic actuators , Aircraft control cables , Dual channel , Actuators , Servomechanisms , Electric power , Survival(General) , Reliability(Electronics) , Gears , Transmissions(Mechanical) , Valves , Torque , Velocity , Training aircraft , Epicyclic gear transmission , Servovalve , T-2C aircraft