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Technological assessment of high temperature sensing systems under extreme environment

Anindya Ghoshal (Prognostics and Diagnostics Team, United States Army Research Laboratory, Adelphi, Maryland, USA)
Dy Le (Prognostics and Diagnostics Team, United States Army Research Laboratory, Adelphi, Maryland, USA)
HeungSoo Kim (Department of Mechanical, Robotics and Energy Engineering, Dongguk University, Seoul, Republic of Korea)

Sensor Review

ISSN: 0260-2288

Article publication date: 20 January 2012

583

Abstract

Purpose

Presently there exists no way to directly measure strain at high temperatures in engine components such as the combustion chamber, exhaust nozzle, propellant lines, and turbine blades and shaft. The purpose of this paper is to address this issue.

Design/methodology/approach

Thermomechanical fatigue (TMF) prediction, which is a critical element for a blade design, is a strong function of the temperature and strain profiles. Major uncertainties arise from the inability of current instrumentation to measure temperature and strain at critical locations. This prevents the structural designer from optimizing the blade design for high temperature environments, which is a significantly challenging problem in engine design.

Findings

Being able to directly measure strains in different high temperature zones would deeply enhance the effectiveness of aircraft propulsion systems for fatigue damage assessment and life prediction. The state of the art for harsh environment, high temperature sensors has improved considerably over the past few years.

Originality/value

This paper lays down specifications for high temperature sensors and provides a technological assessment of these new sensing technologies. The paper also reviews recent advances made in harsh environment sensing systems and takes a peek at the future of such technologies.

Keywords

Citation

Ghoshal, A., Le, D. and Kim, H. (2012), "Technological assessment of high temperature sensing systems under extreme environment", Sensor Review, Vol. 32 No. 1, pp. 66-71. https://doi.org/10.1108/02602281211198476

Publisher

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Emerald Group Publishing Limited

Copyright © 2012, Emerald Group Publishing Limited

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