The effect of environment on TBC lifetime

Bruce A. Pint, Kinga A. Unocic, J. Allen Haynes

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

2 Scopus citations

Abstract

While the water vapor content of the combustion gas in natural gas-fired land based turbines is ∼10%, it can be 20-85% with coal-derived (syngas or H2) fuels or innovative turbine concepts for more efficient carbon capture. Additional concepts envisage working fluids with high CO2 contents to facilitate carbon capture and sequestration. To investigate the effects of changes in the gas composition on thermal barrier coating (TBC) lifetime, furnace cycling tests (1 and 100h cycles) were performed in air with 10, 50 and 90 vol.% water vapor and CO2-10%H2O and compared to prior results in dry air or O2. Two types of TBC?s were investigated: (1) diffusion bond coatings (Pt diffusion or Pt-modified aluminide) with commercial electron-beam physical vapor-deposited yttria-stabilized zirconia (YSZ) top coatings on second-generation superalloy N5 and N515 substrates and (2) high velocity oxygen fuel (HVOF) sprayed MCrAlYHfSi bond coatings with air-plasma sprayed YSZ top coatings on superalloys X4, 1483 or 247 substrates. For both types of coatings exposed in 1h cycles, the addition of water vapor resulted in a decrease in coating lifetime, except for Pt diffusion coatings which were unaffected by the environment. In 100h cycles, environment was less critical, perhaps because coating failure was chemical (i.e. due to interdiffusion) rather than mechanical. In both 1h and 100h cycles, CO2 did not appear to have any negative effect on coating lifetime.

Original languageEnglish
Title of host publicationCeramics; Controls, Diagnostics and Instrumentation; Education; Manufacturing Materials and Metallurgy; Honors and Awards
PublisherAmerican Society of Mechanical Engineers (ASME)
ISBN (Electronic)9780791856758
DOIs
StatePublished - 2015
EventASME Turbo Expo 2015: Turbine Technical Conference and Exposition, GT 2015 - Montreal, Canada
Duration: Jun 15 2015Jun 19 2015

Publication series

NameProceedings of the ASME Turbo Expo
Volume6

Conference

ConferenceASME Turbo Expo 2015: Turbine Technical Conference and Exposition, GT 2015
Country/TerritoryCanada
CityMontreal
Period06/15/1506/19/15

Funding

The authors would like to thank G. W. Garner, T. M. Lowe, K. M. Cooley, H. Longmire, T. Jordan and D. Leonard for assistance with the experimental work. Plating of Pt was conducted at Tennessee Tech. University by Prof. Y. Zhang. B. Hazel and B. Nagaraj at General Electric Aircraft Engines provided the N5 and N515 substrate materials and coated the specimens with EB-PVD YSZ and Stonybrook Univ. applied the HVOF and APS coatings. The X4 substrates were provided by K. Murphy at Alcoa Howmet, the 1483 substrates by A. Kulkarni at Siemens and the 247 substrates by Capstone Turbine Corp. P. F. Tortorelli provided helpful comments on the manuscript. This research was sponsored by the U.S. Department of Energy, Office of Coal and Power R&D, Office of Fossil Energy, (R. Dennis program manager). This manuscript has been authored by UT-Battelle, LLC under Contract No. DE-AC05-00OR22725 with the U.S. Department of Energy. The United States Government retains and the publisher, by accepting the article for publication, acknowledges that the United States Government retains a nonexclusive, paid-up, irrevocable, world-wide license to publish or reproduce the published form of this manuscript, or allow others to do so, for United States Government purposes. The Department of Energy will provide public access to these results of federally sponsored research in accordance with the DOE Public Access Plan (http://energy.gov/downloads/doe-publicaccess-plan).

FundersFunder number
DOE Public Access Plan
LLCDE-AC05-00OR22725
Office of Coal and Power R&D
UT-Battelle
United States Government
U.S. Department of Energy
General ElectricN5, N515
Alcoa
Siemens Foundation
Office of Fossil Energy
American Pain Society

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