Mapping the surface temperature of ceramic and superalloy turbine engine components using laser-induced fluorescence of thermographic phosphor

被引：32

作者：

Alaruri, S ^{[1
]}

Bonsett, T ^{[1
]}

Brewington, A ^{[1
]}

McPheeters, E ^{[1
]}

Wilson, M ^{[1
]}

机构：

[1] Allison Engine Co, Rolls Royce Aerosp Grp, Indianapolis, IN 46206 USA

来源：

OPTICS AND LASERS IN ENGINEERING | 1999年 / 31卷 / 05期

关键词：

D O I：

10.1016/S0143-8166(99)00031-7

中图分类号：

O43 [光学];

学科分类号：

070207 [光学]; 0803 [光学工程];

摘要：

An excimer laser-based system for mapping the surface temperature of turbine engine parts coated with thermographic phosphors has been developed. The intensities measured for Y2O3:Eu over the temperature range similar to 500-750 degrees C are presented. In addition, the data correction and error analysis algorithm is discussed. The overall accuracy of this intensity-based surface temperature measurement technique was estimated to be +/-5%. Furthermore, surface temperature measurements obtained from a ceramic matrix composite and superalloy components are presented. (C) 1999 Elsevier Science Ltd. All rights reserved.

引用

页码：345 / 351

页数：7

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