Title: Research supported by the Office of Naval Research
1Experiences from the ONR-MURI Program on TBCs for
Aeroengines (Science Underpinning Prime Reliant
Coatings)
D.R. Clarke, A.G. Evans, C.G. Levi Materials
Department, University of California, Santa
Barbara
In collaboration with G.H. Meier and F. Pettit
(Pittsburg), J.W. Hutchinson and Z. Suo
(Harvard), A.H. Heuer (CWRU), H.N.G. Wadley
(Virginia), B. Gleeson (Iowa), R. Darolia and D.
Wortman (GE), M. Maloney (PW) and colleagues in
the NSF-HIPERCOAT and AFOSR-MEANS programs.
Workshop on Improving Ship Capabilities by
Insertion of Materials into Marine Gas Turbine
Engines Columbus, OH, May 24, 2006
Research supported by the Office of Naval
Research (Dr. S.G. Fishman/Dr. D. Shifler)
2Multidisciplinary Research on TBCs Overarching
Goals
- Extend the durability and reliability of TBCs by
establishing an understanding of the mechanisms
of failure, including the underlying phenomena
and their associated dynamics. - Enhance performance of TBCs, notably their
ability to operate at higher temperatures and in
more aggressive environments, by understanding
the evolution of their structure and associated
thermodynamic and kinetic fundamentals, and
using that understanding to identify and develop
potential alternative materials. - Respond to problems identified by industry and/or
the Navy that may arise in the course of the
program notable examples are CMAS and
Erosion/FOD.
3Mechanisms Limiting Durability in TBCs
A multidimensional problem, requiring an
interdisciplinary research effort
4TBC Failure Driven by TGO Rumpling
- TGO growth provides strain energy available to
drive spallation upon thermal cycling
5Development of Mechanism Maps
Thermal Expansion Bond Coat Swelling
Micromechanics modeling essential to
understanding failure modes
6Balint-Hutchinson model
Thermal Cycling Induced Rumpling
TGO
BC
Substrate
A multidisciplinary collaboration leading to the
development of a mechanics model that predicts
experimental findings
7Erosion and FOD Mechanisms
8Cracking/Erosion Threshold Map
ELASTO- DYNAMIC DOMAIN
High Toughness Soft at High Temperature
9t toughnessthe key to durability?
10 Ferroelastic Switching
11Faulhaber, Krämer
Specimen provided by R. Darolia (GE)
TBC Degradation by CMAS
Airfoil
Shroud
Specimen provided by R. Kowalik (Navy)
Faulhaber, Krämer
12Delamination Caused by Thermal Gradients
Raman piezo-spectroscopic measurement of stresses
in CMAS penetrated TBC on shroud, resulting from
rapid thermal cooling and alloy constraint.
13Isothermal Infiltration with Model CMAS
7YSZ, 10mg, 7mm diam. pellet, 1300C Treatment
15 min
4h
14Gd2Zr2O7 A CMAS Resistant TBC?
15Leverage for Marine Turbines
- Outcomes that may help developments in Marine
Turbines - Models that incorporate the interaction between
thermal, mechanical and chemical phenomena, e.g.
cyclic oxidation, penetration by molten deposits.
- Microstructure science base, including phase
stability in oxides and bond coats, morphological
evolution of layered and porous systems,
interdiffusion between BCs and superalloys. - Concepts to guide material design, e.g. effect of
dopants on toughness and phase stability in
thermal barrier oxides. - NDE and sensing concepts, e.g. those based on
luminescence. - Testing methods and implications.
- Synthesis and processing experiences.
16Broader Lessons
- Experiences with materials challenges in aircraft
engines highlight the complex and multifaceted
nature of these problems as well as the need for
a systems perspective and a multidisciplinary
approach in searching for solutions. The added
chemical complexity of the marine turbine
environment make those needs even more evident. - A fundamental, mechanism-based approach is
essential in understanding the performance and
durability of materials in gas turbines, and in
guiding the development of new materials systems
that enable further advances in engine
technology. - Effective integration of modeling and experiments
in a collaborative research environment
accelerate the learning process and help develop
new solutions.