NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Low Conductivity Thermal Barrier CoatingsThermal barrier coatings will be more aggressively designed to protect gas turbine engine hot-section components in order to meet future engine higher fuel efficiency and lower emission goals. In this presentation, thermal barrier coating development considerations and requirements will be discussed. An experimental approach is established to monitor in real time the thermal conductivity of the coating systems subjected to high-heat-flux, steady-state and cyclic temperature gradients. Advanced low conductivity thermal barrier coatings have also been developed using a multi-component defect clustering approach, and shown to have improved thermal stability. The durability and erosion resistance of low conductivity thermal barrier coatings have been improved utilizing advanced coating architecture design, composition optimization, in conjunction with more sophisticated modeling and design tools.
Document ID
20050216393
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Zhu, Dong-Ming
(Army Research Lab. Cleveland, OH, United States)
Date Acquired
September 7, 2013
Publication Date
September 1, 2005
Subject Category
Composite Materials
Report/Patent Number
NASA/TM-2005-213857
E-15227
Meeting Information
Meeting: School of Materials Engineering Seminar
Location: West Lafayette, IN
Country: United States
Start Date: February 28, 2005
Funding Number(s)
WBS: WBS 22-714-20-09
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available