Review of a Custom-Designed Optical Sensing System for Aero-Engine Applications

Abstract

Fibre bundle-based reflective optical sensors are good candidates for parameter monitorisation in aero engines. Tip clearance is one of those parameters of great concern that is necessary to monitor. Within this optical technology, the evolution experienced by a custom-designed optical sensor is presented from its first configuration up to the fifth one. The performance of the last configuration is compared with those of other two optical sensors that are also based on a fibre bundle design. The comparison has been carried out in an experimental program in a transonic wind tunnel for aero engines. The proven high resolution and sensitivity of the last configuration of the optical sensor opens up the possibility to detect blade defects, cracks, etc. that could otherwise be hard to track.This work was supported in part by the European Regional Development Fund, in part by the Ministerio de Economía y Competitividad under project RTI2018-094669-B-C31, and in part by the Gobierno Vasco/Eusko Jaurlaritza under projects IT933-16, ELKARTEK (KK-2018/00078 and KK-2019/00051), EKINTZAILE 01560/2019 and HAZITEK (ZL-2020/00380). The work of J. Amorebieta is supported in part by a PhD fellowship from the University of the Basque Country (UPV/EHU), Vicerrectorado de Euskera y Formación Continua