This proposal addresses the development of a hybrid chemical/mechanical heat pump, using environmentally acceptable absorbent/refrigerant pairs, for more electric aircraft thermal control systems. Mainstream's chemical/mechanical heat pump incorporates the advantages of both the chemical and mechanical vapor compression systems. The objective of the Phase II effort is to demonstrate the energy savings of the chemical/mechanical heat pump, using an environmentally-acceptable absorbent/HFC-134a working fluid pair, for more electric aircraft. This will be accomplished by designing and fabricating a breadboard demonstration unit, investigating various operational parameters, absorbent/HFC-134a pairs (a short list), and component designs in the breadboard demonstration unit, performing life-testing of the two-phase compressor, selecting a specific application for a field demonstration unit, designing and fabricating a high-efficiency field demonstration unit, and extensive testing of the high-efficiency field demonstration unit.
Keywords: Room-Temperature Superconductor Zero Resistance Fuzes Ambient-Temperature Superconducting Polymers