Accession Number : ADA119627

Title :   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.

Descriptive Note : Final rept. Sep 78-Apr 81,

Corporate Author : BENDIX CORP TETERBORO N J FLIGHT SYSTEMS DIV

Personal Author(s) : Kineyko,Wallace

PDF Url : ADA119627

Report Date : Apr 1982

Pagination or Media Count : 55

Abstract : 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)

Descriptors :   *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

Subject Categories : Training Aircraft
      Hydraulic and Pneumatic Equipment

Distribution Statement : APPROVED FOR PUBLIC RELEASE