Abstract
A method and system for cooling an engine and/or vehicle using energy separation is disclosed herein. An energy separation device is operable for separating a compressed gaseous coolant stream into a first relatively cooler coolant flow stream and a second relatively hotter coolant flow stream. The relative cooler coolant flow stream is directed to a first region requiring increased cooling and the relative hotter coolant flow stream is directed to a second region requiring lower cooling than the first region in the engine or vehicle.
Document Type
Patent
Status
Issued
Issue Date
9-27-2022
Patent Number
US 11454171 B1 [ 11,454,171 ]
CPC Classification
F02C7/18
Application number
16/892496
Assignees
Government of the United States, as represented by the Secretary of the Air Force, Wright-Patterson AFB, OH (US)
Filing Date
6-4-2020
Recommended Citation
Rutledge, James L., Matthew Fuqua, and Carol M. Bryant. Turbine Cooling System With Energy Separation. United States Patent 11454171 (B1), issued 27 September 2022, https://scholar.afit.edu/patents/22