Research Papers: Gas Turbines: Controls, Diagnostics, and Instrumentation

Data-Driven Fault Detection in Aircraft Engines With Noisy Sensor Measurements

[+] Author and Article Information
Soumik Sarkar

Department of Mechanical Engineering, Pennsylvania State University, University Park, PA 16802szs200@psu.edu

Xin Jin

Department of Mechanical Engineering, Pennsylvania State University, University Park, PA 16802xuj103@psu.edu

Asok Ray

Department of Mechanical Engineering, Pennsylvania State University, University Park, PA 16802axr2@psu.edu

J. Eng. Gas Turbines Power 133(8), 081602 (Apr 06, 2011) (10 pages) doi:10.1115/1.4002877 History: Received March 12, 2010; Revised September 02, 2010; Published April 06, 2011; Online April 06, 2011

An inherent difficulty in sensor-data-driven fault detection is that the detection performance could be drastically reduced under sensor degradation (e.g., drift and noise). Complementary to traditional model-based techniques for fault detection, this paper proposes symbolic dynamic filtering by optimally partitioning the time series data of sensor observation. The objective here is to mask the effects of sensor noise level variation and magnify the system fault signatures. In this regard, the concepts of feature extraction and pattern classification are used for fault detection in aircraft gas turbine engines. The proposed methodology of data-driven fault detection is tested and validated on the Commercial Modular Aero-Propulsion System Simulation (C-MAPSS ) test-bed developed by NASA for noisy (i.e., increased variance) sensor signals.

Copyright © 2011 by American Society of Mechanical Engineers
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Figure 6

Revised class assignment for fault detection

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Figure 9

Feature space of training set: uniform partitioning (UP)

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Figure 10

Feature space of training set: maximum entropy partitioning (MEP)

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Figure 11

Representative sensor T48 observation

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Figure 1

Gas turbine engine schematic (17)

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Figure 2

Schematic diagram of the C-MAPSS engine model

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Figure 3

Original class labels for data collection

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Figure 4

Profile of throttle resolving angle (TRA)

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Figure 5

Representative time series data for HPC fault and Ps30 degradation conditions

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Figure 7

General framework for optimization of feature extraction

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Figure 8

Feature space of the training set using optimal partitioning



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