Title :
Electrically Driven Environmental Control System
Author :
McNamara, James E.
Author_Institution :
Naval Air Development Center
fDate :
5/1/1984 12:00:00 AM
Abstract :
An environmental control system (ECS) being developed under the title of energy efficient environmental control system is described. The ECS is a closed-loop, electrically driven, vapor cycle system. The vapor cycle will have a compressor driven by a variable speed, high-voltage dc motor. The reasons for selecting this type of system are discussed here. Breadboard testing of a variable speed compressor to demonstrate the feasibility of such an approach has been completed. The testing results were used to develop a preliminary design of a prototype compressor. In future phases of the program, the prototype compressor will be developed; a prototype system will be constructed and laboratory tested; and finally the prototype system will be flight demonstrated.
Keywords :
Aerospace control; Aerospace electronics; Aircraft propulsion; Control systems; Cooling; Electric variables control; Engines; Military aircraft; Prototypes; Testing;
Journal_Title :
Aerospace and Electronic Systems, IEEE Transactions on
DOI :
10.1109/TAES.1984.310508