Development of temperature-sensitive paints for high-temperature aeropropulsion applications

S. W. Allison, D. L. Beshears, T. Benic, W. A. Hollerman, P. Boudreaux

Research output: Contribution to conferencePaperpeer-review

15 Scopus citations

Abstract

Fluorescence from a phosphor coating will indicate the temperature of the substrate to which it is attached, assuming thermal equilibrium is achieved. The goal of this investigation is to identify phosphors for making temperature measurements on aerospace surfaces with temperatures varying from ambient to 1000°C and to identify and test binders/adhesives that may be mixed with thermographic phosphors and sprayed onto surfaces of interest to provide a durable and uniform coating. The surfaces of interest include various high-strength metal alloys, such as stainless steel and nickel with and without thermal barrier coats, ceramics, carbon/carbon composites, and copper. Our initial efforts have concentrated on the most challenging substrates, the high-strength nickel alloy without the thermal barrier coating. Several candidate phosphors have been identified, and we are considering mixing two or more phosphors to cover the full temperature range. The phosphors being considered are Y2O3:Eu, YAG:Eu, YAG:Dy, YAG:Cr, and YPO4:Eu,Dy. The initial results indicate that two binders-Sauereisen's Thinning Liquid #14 and a mix of ZYP, Inc.'s, LK and HPC will function well on high-strength nickel alloys to 800°C. Furthermore, the LK and HPC mix performed well on high-strength stainless steel substrates coated with a thermal barrier coat to a temperature of 1000°C.

Original languageEnglish
StatePublished - 2001
Externally publishedYes
Event37th Joint Propulsion Conference and Exhibit 2001 - Salt Lake City, UT, United States
Duration: Jul 8 2001Jul 11 2001

Conference

Conference37th Joint Propulsion Conference and Exhibit 2001
Country/TerritoryUnited States
CitySalt Lake City, UT
Period07/8/0107/11/01

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