Translated System Requirements into PTO Design Requirements (in addition to Component-level metrics) for the HydroAir Power Take Off System
Includes Maximum Cost, Critical Dimensions and Weights, Damping Curve, Rotor Speed Profile Changes, Mechanical Power for a given pressure and airflow, Turbine rpm range and power, Generator input torque, Torque speed curves/profile, Generated electrical power for given input torque, Generated Load Cycles, Variation in generator speed, Conversion efficiencies for pressure to mechanical, mechanical to electrical: losses due to conditioning, Generator temperatures, Vibration/acceleration, Operating angle, Shaft strain, and Noise level.
DOE Project Number: EE0006609
DOE Project Lead: Erik Mauer
Submitted Jul 26, 2021
Siemens Government Technologies, Inc.