Accession Number : AD0503309
Title : Advanced Fluidic Controls for Integrated Propulsion Systems. Part IV. Demonstration of an Integrated Propulsion System Control at Simulated Flight Conditions Using Fluidic Control Techniques.
Descriptive Note : Final rept. Apr 65-May 68.
Corporate Author : HONEYWELL INC MINNEAPOLIS MINN AEROSPACE DIV
Personal Author(s) : Pamperin,Ralph H. ; Schmidt,Ross D.
Report Date : SEP 1968
Pagination or Media Count : 164
Abstract : Feasibility of a fluidic control system for advanced integrated propulsion system control was demonstrated at simulated flight conditions in an altitude engine test cell. System studies were conducted using control and engine computer simulations to develop advanced propulsion system control modes. Using fluidic sensors and computational elements developed under this program, a fluidic integrated propulsion control system was mechanized and evaluated on a J95-GE-5 engine at the Air Force Aero Propulsion Laboratory at simulated Mach numbers and altitudes. Performance capability was demonstrated in the areas of start up, speed control, transient control, compressor stability control, turbine overtemperature control, overspeed control and variable engine geometry control. (Author)
Descriptors : (*TURBOJET ENGINES, CONTROL SYSTEMS), (*FLUID AMPLIFIERS, TURBOJET ENGINES), (*CONTROL SYSTEMS, *FLUIDICS), TURBOJET EXHAUST NOZZLES, TURBOJET INLETS, ALTITUDE CHAMBERS, SIMULATION, COMPUTER PROGRAMS, DETECTORS, FLIGHT SPEEDS, TEMPERATURE CONTROL, ENGINE SURGE, FEASIBILITY STUDIES, DESIGN, PERFORMANCE(ENGINEERING), POWER SUPPLIES, FUEL PUMPS, STARTING, FUEL CONSUMPTION, FUEL SYSTEMS
Subject Categories : Fluidics and Fluerics
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE