IGF::OT::IGF TURBOELECTRIC AIRCRAFT WITH GAS TURBINES DRIVING ELECTRIC GENERATORS CONNECTED TO ELECTRIC PRO…

Public award description

IGF::OT::IGF TURBOELECTRIC AIRCRAFT WITH GAS TURBINES DRIVING ELECTRIC GENERATORS CONNECTED TO ELECTRIC PROPULSION MOTORS HAVE THE POTENTIAL TO TRANSFORM THE AIRCRAFT DESIGN SPACE BY DECOUPLING POWER GENERATION FROM PROPULSION. RESULTING AIRCRAFT DESIGNS SUCH AS BLENDED-WING BODIES WITH DISTRIBUTED PROPULSION CAN PROVIDE THE LARGE REDUCTIONS IN EMISSIONS, FUEL BURN, AND NOISE REQUIRED TO MAKE AIR TRANSPORTATION GROWTH PROJECTIONS SUSTAINABLE. THE POWER DENSITY REQUIREMENTS FOR THESE ELECTRIC MACHINES CAN ONLY BE ACHIEVED WITH SUPERCONDUCTORS, WHICH IN TURN REQUIRE LIGHTWEIGHT, HIGH-CAPACITY CRYOCOOLERS. CREARE HAS PREVIOUSLY DEVELOPED A CRYOFLIGHT TURBO-BRAYTON CRYOCOOLER CONCEPT THAT EXCEEDS THE MASS AND PERFORMANCE TARGETS IDENTIFIED BY NASA FOR SUPERCONDUCTING AIRCRAFT WITH HIGH-TEMPERATURE SUPERCONDUCTING (HTS) MATERIALS REQUIRING COOLING TO 50 K. HERE, WE PROPOSE TO EXTEND THE TEMPERATURE RANGE OF OUR CRYOCOOLER WITH AN INNOVATIVE NEW CYCLE CONCEPT TO PROVIDE COOLING TO 15 K FOR MGB2 SUPERCONDUCTORS, WHICH OFFER PRICE AND PERFORMANCE ADVANTAGES FOR CERTAIN SUPERCONDUCTING MACHINES. IN PHASE I OF THIS PROJECT, WE WILL EVALUATE THE PERFORMANCE ADVANTAGES OF OUR CONCEPT THROUGH MODELING AND PRELIMINARY COMPONENT DESIGNS. IN PHASE II, WE WILL FABRICATE AND TEST THE HIGHEST-RISK COMPONENTS TO BRING THE OVERALL TRL TO 4. IN PHASE III, WE WILL BUILD AND TEST A COMPLETE CRYOCOOLER TO SUPPORT EXTENDED PERFORMANCE TESTING WITH MGB2 SYSTEMS. THIS DEVELOPMENT EFFORT WILL PROVIDE AN ENABLING TECHNOLOGY FOR THE SUPERCONDUCTING SYSTEMS NEEDED TO MAKE TURBOELECTRIC AIRCRAFT FEASIBLE.