This is a report of the fabrication and design verification testing of a Dual Mode Electro/Pneumatic Actuator. Pneumatic mode open loop operation and control verified. Torque/Speed performance less than design goal due to excessive gear separation force.
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
56 pages
Report
No indication
English
Aircraft , Avionics , Flight control systems , Pneumatic actuators , Aircraft control cables , Dual channel , Actuators , Electric power , Reliability(Electronics) , Servomechanisms , Torque , Valves , Open loop systems , Fabrication , Validation , T-2C aircraft , Pneumatic motors , Epicyclic gear transmission