skip to main content
OSTI.GOV title logo U.S. Department of Energy
Office of Scientific and Technical Information

Title: Effect of CMAS viscosity on the infiltration depth in thermal barrier coatings of different microstructures

Journal Article · · Surface and Coatings Technology
 [1];  [2];  [1];  [1]
  1. Solutions Spray Technologies LLC, Storrs, CT (United States)
  2. Institute of Materials Science, Storrs, CT (United States)

Calcium magnesium aluminum silicate (CMAS) is one of the leading concerns for the gas turbine industry. The effects of CMAS viscosity and the coating microstructure on CMAS infiltration depth were explored by conducting a time dependent interaction study. Three CMAS compositions were used from literature, and their viscosities predicted through FactSage viscosity module were drastically different. The interaction was carried out on three different TBCs synthesized using the solution precursor plasma spray process (SPPS): two of the TBCs were made of yttrium aluminum garnet (YAG) having different microstructures that promote different modes of CMAS infiltration, and one TBC was made of gadolinium zirconate (GZO). All samples had stress relieving vertical cracks and different intensities of horizontally banded porosity, (inter pass boundaries IPBs). A concentration of 100 mg/cm2 of CMAS was applied on the TBCs which were then subjected to a 5-minute interaction at 1300 °C. Samples were analyzed using scanning electron microscopy (SEM), electron dispersive X-ray spectroscopy (EDXS), and transmission electron microscopy (TEM). Low viscosity CMAS readily penetrated the TBCs while more viscous CMAS showed less penetration. The depth of CMAS infiltration depended on the coating microstructure. In the YAG with IPBs, the CMAS spread horizontally in the IPBs before infiltrating deeper, resulting in reduced infiltration depth compared to other samples in spite of having wider vertical cracks. TEM and EDXS analysis were performed to investigate the phases present in the CMAS-TBC interaction region in YAG. Two regions were chosen, the top TBC surface in direct contact with the sea of CMAS, and the region at the CMAS penetration ended within the coating. Finally, the results showed that no secondary phases like apatite were observed in YAG, thus it can be concluded that the arrest of CMAS happened solely because of CMAS viscosity and the short infiltration time.

Research Organization:
HiFunda LLC, Salt Lake City, UT (United States)
Sponsoring Organization:
USDOE Office of Science (SC), Office of SBIR/STTR Programs (SBIR/STTR); USDOE
Grant/Contract Number:
SC0007544
OSTI ID:
1977676
Alternate ID(s):
OSTI ID: 1838900
Journal Information:
Surface and Coatings Technology, Vol. 432, Issue C; ISSN 0257-8972
Publisher:
ElsevierCopyright Statement
Country of Publication:
United States
Language:
English

References (47)

A delamination mechanism for thermal barrier coatings subject to calcium–magnesium–alumino-silicate (CMAS) infiltration journal February 2005
CMAS corrosion of EB PVD TBCs: Identifying the minimum level to initiate damage journal January 2010
Role of environment deposits and operating surface temperature in spallation of air plasma sprayed thermal barrier coatings journal December 1996
Plasma sprayed gadolinium zirconate thermal barrier coatings that are resistant to damage by molten Ca–Mg–Al–silicate glass journal May 2012
A coupled theory for deformation and phase transformation due to CMAS infiltration and corrosion of thermal barrier coatings journal September 2021
Factors influencing the penetration depth of molten volcanic ash in thermal barrier coatings: Theoretical calculation and experimental testing journal June 2019
Effects of yttria content on the CMAS infiltration resistance of yttria stabilized thermal barrier coatings system journal April 2020
Mechanisms controlling the durability of thermal barrier coatings journal January 2001
Investigation of the thermal conductivity of selected compounds of lanthanum, samarium and europium journal May 1998
Emerging materials and processes for thermal barrier systems journal January 2004
Low Thermal Conductivity Yttrium Aluminum Garnet Thermal Barrier Coatings Made by the Solution Precursor Plasma Spray: Part II—Planar Pore Formation and CMAS Resistance journal June 2018
Composition effects of thermal barrier coating ceramics on their interaction with molten Ca–Mg–Al–silicate (CMAS) glass journal September 2012
Low Thermal Conductivity Yttrium Aluminum Garnet Thermal Barrier Coatings Made by the Solution Precursor Plasma Spray: Part I—Processing and Properties journal May 2018
Recent Developments in the Field of Thermal Barrier Coatings journal March 2009
Zirconates as New Materials for Thermal Barrier Coatings journal August 2000
Thermal-barrier coatings for more efficient gas-turbine engines journal October 2012
Influence of microstructure on the durability of gadolinium zirconate thermal barrier coatings using APS & SPPS processes journal March 2018
Thermochemical Interaction of Thermal Barrier Coatings with Molten CaO?MgO?Al 2 O 3 ?SiO 2 (CMAS) Deposits journal October 2006
Phase composition and its changes during annealing of plasma-sprayed YSZ journal May 2000
Failure of Thermal Barrier Coatings Subjected to CMAS Attack journal July 2009
Environmental degradation of thermal-barrier coatings by molten deposits journal October 2012
Low Thermal Conductivity Yttria-Stabilized Zirconia Thermal Barrier Coatings Using the Solution Precursor Plasma Spray Process journal February 2014
2ZrO 2 ·Y 2 O 3 Thermal Barrier Coatings Resistant to Degradation by Molten CMAS: Part II, Interactions with Sand and Fly Ash journal September 2014
Ceramic materials for thermal barrier coatings journal January 2004
Phase diagram of the ZrO2–Gd2O3–Al2O3 system journal January 2006
Calcium-rich CMAS corrosion induced microstructure development of thermal barrier coatings journal September 2017
Thermal Conductivity, Phase Stability, and Oxidation Resistance of Y 3 Al 5 O 12 (YAG)/Y 2 O 3 –ZrO 2 (YSZ) Thermal-Barrier Coatings journal April 2004
2ZrO 2 ·Y 2 O 3 Thermal Barrier Coatings Resistant to Degradation by Molten CMAS: Part I, Optical Basicity Considerations and Processing journal September 2014
Mitigation of damage from molten fly ash to air-plasma-sprayed thermal barrier coatings journal September 2011
An investigation of phase stability in the Y2O3-Al2O3 system journal April 1974
The Dynamics of Capillary Flow journal March 1921
Phase Transformation in EB-PVD Yttria Partially Stabilized Zirconia Thermal Barrier Coatings during Annealing journal April 2000
Effects of surface wettability and liquid viscosity on the dynamic wetting of individual drops journal August 2014
Processing–microstructure relationships for plasma-sprayed yttrium aluminum garnet journal August 2008
Infiltration-Inhibiting Reaction of Gadolinium Zirconate Thermal Barrier Coatings with CMAS Melts journal February 2008
A chemo-thermo-mechanically constitutive theory for thermal barrier coatings under CMAS infiltration and corrosion journal December 2019
Thermal barrier coatings for aircraft engines: history and directions journal March 1997
Equilibrium relationships between thermal barrier oxides and silicate melts journal November 2016
Yttrium Aluminum Garnet Powder Feedstock for Atmospheric Plasma Spray journal April 2020
Melting and Crystallization of Silicate Systems Relevant to Thermal Barrier Coating Damage journal January 2015
New material concepts for the next generation of plasma-sprayed thermal barrier coatings journal March 2004
CMAS behavior of yttrium aluminum garnet (YAG) and yttria-stabilized zirconia (YSZ) thermal barrier coatings journal October 2017
The Hotter the Engine, the Better journal November 2009
Thermal barrier coating materials journal June 2005
Jet Engine Coatings for Resisting Volcanic Ash Damage journal April 2011
Thermal Barrier Coatings for Gas-Turbine Engine Applications journal April 2002
Modeling stress evolution in porous ceramics subjected to molten silicate infiltration and corrosion journal October 2021