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