This SBIR proposal is submitted in response to solicitation SBIR Topic A1.04. This project relates to development of cryogenic (rotor and stator) generators required for future thin/short haul aviation or commercial transport vehicles which use turboelectric, hybrid electric, or all electric power generation as part of the propulsion system. Turboelectric, hybrid electric and all electric power generation as well as distributed propulsive power have been identified as candidate transformative aircraft configurations with reduced fuel consumption/energy use and emissions. However, components and management methods for power generation, distribution and conversion are not currently available in the high-power ranges with the necessary efficiency, power density, electrical stability and safety required for thin haul/short haul, or transport-class aircraft. Specifically, motors/generators are desired with >98% efficiency, specific power >13 kW/kg, and total power >200 kW. For generators, high power density can be achieved if the rotational speed is high (15,000-30,000 rpm), however low AC loss conductors are required in the stator. This can be achieved by designing the stator with a high purity aluminum hyperconductor at cryogenic temperatures with a cryogenically cooled superconducting rotor. During the Phase I we will be investigating the use of cryogenic aluminum hyperconductor as a low AC loss conductor for stator coils. With the development of low AC loss aluminum hyperconductor wire by Hyper Tech, we can achieve high speed cryogenically cooled generators with power densities over 30 kW/kg for aircraft. During the Phase I we intend to demonstrate approaches for manufacturing aluminum hyperconductor strands and cables suitable for high speed machines (500-600 Hz, 15,000-25,000 rpm), and analyze the AC losses of the conductors in applied magnetic fields for developing generator conceptual designs with high speed rotors. Potential NASA Applications (Limit 1500 characters, approximately 150 words): Besides electric passenger aircraft, NASA can benefit from many applications where lightweight power components are required such as smaller land-based generators, invertor type transformers, inductors and higher frequency power conditioning equipment. Potential Non-NASA Applications (Limit 1500 characters, approximately 150 words): Hyperconductor aluminum is a solution for manufacturers of invertor transformers, high speed motors and high speed generators (10,000 - 30,000 rpm) requiring high power density who seek lighter weight and higher efficiency 4-20 MW class aircraft turbo-generators, offshore oil platform motors, marine propulsion and generation and portable emergency power systems. Duration: 6
