Accession Number : ADA119003

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 : ADA119003

Report Date : Apr 1982

Pagination or Media Count : 56

Abstract : 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.

Descriptors :   *Flight control systems, *Pneumatic actuators, Aircraft control cables, Dual channel, Actuators, Electric power, Reliability(Electronics), Servomechanisms, Torque, Valves, Open loop systems, Fabrication, Validation

Subject Categories : Aircraft
      Hydraulic and Pneumatic Equipment

Distribution Statement : APPROVED FOR PUBLIC RELEASE