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
6-18-2024
Patent Number
US 12012895 [ 12,012,895 ] ; US12012895B1
CPC Classification
F 01 D 5/186
Application number
17/879016
Assignees
United States of America as represented by the Secretary of the Air Force, Wright-Patterson AFB
Filing Date
8-2-2022
Recommended Citation
Rutledge, J. L., Fuqua, M., & Bryant, C. M. (2024). Turbine Cooling System with Energy Separation (United States Patent No. US12012895B1). https://scholar.afit.edu/patents/109