Accession Number : AD0910496
Title : Multi-Mission Turbine Engine Propulsion Simulator Users Console. Volume I. Operating Instructions and Test Plan.
Descriptive Note : Technical rept. 15 May 72-15 Jan 73,
Corporate Author : GENERAL ELECTRIC CO CINCINNATI OH AIRCRAFT ENGINE BUSINESS GROUP
Personal Author(s) : Delaney, B. R. ; West, H. ; Prather, J. G.
Report Date : MAY 1973
Pagination or Media Count : 34
Abstract : A Propulsion Simulator Users Control Console has been developed which will automatically or manually provide for remote control of two propulsion simulators simultaneously or independently in a wind tunnel or calibration test cell. It provides manual control of the turbine bleed valve to vary mixer flow and therefore exhaust nozzle pressure ratio and flow function while maintaining constant RPM. The console monitors vital simulator functions and provides automatic shutdown and fault annunciation in case preset limits are exceeded. Volume I describes how to operate the console and recommends a test plan for initial checkout. Volume II (AD-910 497) describes the systems specifications and design details of the console. (Author)
Descriptors : *CONTROL PANELS), (*SIMULATORS, (*GAS TURBINES, SIMULATORS), (*PROPULSION SYSTEMS, SIMULATORS), WIND TUNNELS, SUPERSONIC CHARACTERISTICS, TRANSONIC FLOW, CALIBRATION, TEST EQUIPMENT, EXHAUST NOZZLES, BLEED SYSTEMS, VALVES, REMOTE CONTROL, SUPERSONIC AIRCRAFT, TRANSONIC AIRCRAFT, TEST METHODS, OPERATION, INSTRUCTION MANUALS.
Subject Categories : Test Facilities, Equipment and Methods
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE