Translated System Requirements into PTO Design Requirements (in addition to Component-level metrics) for the HydroAir Power Take Off System

Awaiting release License 

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.

Citation Formats

Siemens Government Technologies, Inc.. (2020). Translated System Requirements into PTO Design Requirements (in addition to Component-level metrics) for the HydroAir Power Take Off System [data set]. Retrieved from https://mhkdr.openei.org/submissions/333.
Export Citation to RIS
Natanzi, Shahab, Hall, Russell. Translated System Requirements into PTO Design Requirements (in addition to Component-level metrics) for the HydroAir Power Take Off System. United States: N.p., 02 Oct, 2020. Web. https://mhkdr.openei.org/submissions/333.
Natanzi, Shahab, Hall, Russell. Translated System Requirements into PTO Design Requirements (in addition to Component-level metrics) for the HydroAir Power Take Off System. United States. https://mhkdr.openei.org/submissions/333
Natanzi, Shahab, Hall, Russell. 2020. "Translated System Requirements into PTO Design Requirements (in addition to Component-level metrics) for the HydroAir Power Take Off System". United States. https://mhkdr.openei.org/submissions/333.
@div{oedi_333, title = {Translated System Requirements into PTO Design Requirements (in addition to Component-level metrics) for the HydroAir Power Take Off System}, author = {Natanzi, Shahab, Hall, Russell.}, abstractNote = {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.}, doi = {}, url = {https://mhkdr.openei.org/submissions/333}, journal = {}, number = , volume = , place = {United States}, year = {2020}, month = {10}}

Details

Data from Oct 2, 2020

Last updated Jul 26, 2021

Submitted Jul 26, 2021

Organization

Siemens Government Technologies, Inc.

Contact

Paul Jenicek

720.327.6867

Authors

Shahab Natanzi

Siemens Energy

Russell Hall

Siemens Energy

DOE Project Details

Project Name HydroAir Power Take Off System

Project Lead Erik Mauer

Project Number EE0006609

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