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Article

Aircraft Engine Bleed Valve Prognostics Using Multiclass Gated Recurrent Unit

by
Marcia L. Baptista
1,* and
Helmut Prendinger
2
1
Air Transport and Operations, Faculty of Aerospace Engineering, Delft University of Technology (TU Delft), 2628 CD Delft, The Netherlands
2
National Institute of Informatics, Tokyo 1018430, Japan
*
Author to whom correspondence should be addressed.
Aerospace 2023, 10(4), 354; https://doi.org/10.3390/aerospace10040354
Submission received: 19 January 2023 / Revised: 8 March 2023 / Accepted: 10 March 2023 / Published: 3 April 2023
(This article belongs to the Special Issue Aerospace Prognosis Technology)

Abstract

Prognostics and health management is an engineering discipline that aims to support system operation while ensuring maximum safety and performance. Prognostics is a key step of this framework, focusing on developing effective maintenance policies based on predictive methods. Traditionally, prognostics models forecast the degradation process using regression techniques that approximate a mapping function from input to continuous remaining useful life estimates. These models are typically of high complexity and low interpretability. Classification approaches are an alternative solution to these types of models. We propose a predictive classification model that translates the input into discrete output variables instead of mapping the input to a single remaining useful life estimate. Each discrete output variable corresponds to a range of remaining useful life values. In other words, each output class variable represents the likelihood or risk of failure within a specific time range. We apply this model to a real-world case study involving the unscheduled and scheduled removals of a set of engine bleed valves from a fleet of Boeing 737 aircraft. The model can reach an area under the (micro-average) receiver operating characteristic curve of 72%. Our results suggest that the proposed multiclass gated recurrent unit network can provide valuable information about the different fault stages (corresponding to intervals of residual lives) of the studied valves.
Keywords: prognostics; data-driven; multiclassification; degradation stages; gated recurrent unit prognostics; data-driven; multiclassification; degradation stages; gated recurrent unit

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MDPI and ACS Style

Baptista, M.L.; Prendinger, H. Aircraft Engine Bleed Valve Prognostics Using Multiclass Gated Recurrent Unit. Aerospace 2023, 10, 354. https://doi.org/10.3390/aerospace10040354

AMA Style

Baptista ML, Prendinger H. Aircraft Engine Bleed Valve Prognostics Using Multiclass Gated Recurrent Unit. Aerospace. 2023; 10(4):354. https://doi.org/10.3390/aerospace10040354

Chicago/Turabian Style

Baptista, Marcia L., and Helmut Prendinger. 2023. "Aircraft Engine Bleed Valve Prognostics Using Multiclass Gated Recurrent Unit" Aerospace 10, no. 4: 354. https://doi.org/10.3390/aerospace10040354

APA Style

Baptista, M. L., & Prendinger, H. (2023). Aircraft Engine Bleed Valve Prognostics Using Multiclass Gated Recurrent Unit. Aerospace, 10(4), 354. https://doi.org/10.3390/aerospace10040354

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