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Intelligent Engine Systems: Thermal Management and Advanced CoolingThe objective of the Advanced Turbine Cooling and Thermal Management program is to develop intelligent control and distribution methods for turbine cooling, while achieving a reduction in total cooling flow and assuring acceptable turbine component safety and reliability. The program also will develop embedded sensor technologies and cooling system models for real-time engine diagnostics and health management. Both active and passive control strategies will be investigated that include the capability of intelligent modulation of flow quantities, pressures, and temperatures both within the supply system and at the turbine component level. Thermal management system concepts were studied, with a goal of reducing HPT blade cooling air supply temperature. An assessment will be made of the use of this air by the active clearance control system as well. Turbine component cooling designs incorporating advanced, high-effectiveness cooling features, will be evaluated. Turbine cooling flow control concepts will be studied at the cooling system level and the component level. Specific cooling features or sub-elements of an advanced HPT blade cooling design will be downselected for core fabrication and casting demonstrations.
Document ID
20080025993
Acquisition Source
Glenn Research Center
Document Type
Contractor Report (CR)
Authors
Bergholz, Robert
(General Electric Aviation Cincinnati, OH, United States)
Date Acquired
August 24, 2013
Publication Date
June 1, 2008
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NASA/CR-2008-215238
E-16497
Report Number: NASA/CR-2008-215238
Report Number: E-16497
Funding Number(s)
CONTRACT_GRANT: NAS3-1135
WBS: WBS 984754.02.07.03.11.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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