Accession Number : AD0849247
Title : Preliminary Design of a Prototype Flight Unit of a Heat-Actuated Environmental Control System for NAVY Aircraft.
Descriptive Note : Final rept. 16 Feb-16 Oct 68,
Corporate Author : CONDUCTRON CORP NORTHRIDGE CA WESTERN DEVELOPMENT CENTER
Personal Author(s) : Huber, Dieter D. ; Gorman, Alfred J.
Report Date : 16 NOV 1968
Pagination or Media Count : 130
Abstract : The report presents the results of a program for the detailed analysis and preliminary design of a full-scale prototype flight unit of a heat-actuated environmental control system for the cabin air conditioning requirements of Navy high-performance aircraft, as typified by the Navy F-4 fighter aircraft. Also part of this program was the identification of system components requiring development for adaptation to the aircraft flight environment and initiation of development testing. Test results are presented. The control concept is basically a vapor-compression system utilizing two thermodynamic cycles and a no-moving-parts device which replaces the conventional compressor. For this airborne application, main engine compressor bleed air is used as the heat source, although other heat sources, such as fuel burning, aare also suitable. (Author)
Descriptors : (*JET FIGHTERS, CONTROLLED ATMOSPHERES), (*AIRCRAFT CABINS, AIR CONDITIONING EQUIPMENT), NAVAL AIRCRAFT, CONTROL SYSTEMS, VAPORIZATION, HEAT EXCHANGERS, BOILERS, PRESSURIZATION, TEMPERATURE, CONDENSATION, VALVES, COOLING, HEATING, SOURCES, HEAT SINKS.
Subject Categories : Attack and Fighter Aircraft
Air Condition, Heating, Lighting & Ventilating
Distribution Statement : APPROVED FOR PUBLIC RELEASE