Accession Number : AD0724125
Title : Application of a Resonant Combustor to Army Aircraft Engine Starting.
Descriptive Note : Final technical rept. 1 Sep 69-30 Sep 70,
Corporate Author : ROCKETDYNE CANOGA PARK CALIF
Personal Author(s) : Binsley,R. L.
Report Date : FEB 1971
Pagination or Media Count : 89
Abstract : The report describes the results of a 13-month study of the feasibility of starting Army aircraft by means of starting systems utilizing a resonant combustor as the basic power source. Starting of both main engines and auxiliary power units (APU) was considered. Alternative starting techniques were assessed and compared with present techniques. The engine and APU starting starting techniques that best utilize the unique advantages of the resonant combustor were prepared to allow assessment of the characteristics and application problems of these systems. (Author)
Descriptors : (*ENGINE STARTERS, PERFORMANCE(ENGINEERING)), (*ARMY AIRCRAFT, STARTING), (*ARCTIC REGIONS, ARMY AIRCRAFT), GAS GENERATING SYSTEMS, GAS TURBINES, COMBUSTION, HYDRAULIC ACCUMULATORS, TORQUE, REACTION KINETICS, FEASIBILITY STUDIES
Subject Categories : Aircraft
Jet and Gas Turbine Engines
Distribution Statement : APPROVED FOR PUBLIC RELEASE