Abstract

The aircraft auxiliary power unit (APU) is responsible for environmental control in the cabin and the main engines starting the aircraft. The prediction of its performance sensing data is significant for condition-based maintenance. As a complex system, its performance sensing data have a typically nonlinear feature. In order to monitor this process, a model with strong nonlinear fitting ability needs to be formulated. A neural network has advantages of solving a nonlinear problem. Compared with the traditional back propagation neural network algorithm, an extreme learning machine (ELM) has features of a faster learning speed and better generalization performance. To enhance the training of the neural network with a back propagation algorithm, an ELM is employed to predict the performance sensing data of the APU in this study. However, the randomly generated weights and thresholds of the ELM often may result in unstable prediction results. To address this problem, a restricted Boltzmann machine (RBM) is utilized to optimize the ELM. In this way, a stable performance parameter prediction model of the APU can be obtained and better performance parameter prediction results can be achieved. The proposed method is evaluated by the real APU sensing data of China Southern Airlines Company Limited Shenyang Maintenance Base. Experimental results show that the optimized ELM with an RBM is more stable and can obtain more accurate prediction results.

Highlights

  • The aircraft auxiliary power unit (APU) is designed to provide power for the aircraft independently [1]

  • The condition monitoring data of the APU were from the aircraft communications addressing and reporting system, which mainly consist of four segments

  • The operating parameters are comprised of control command, exhaust gas temperature, guide vane opening angle, compressor inlet pressure, load compressor inlet port temperature, bleed air flow, bleed air pressure, oil temperature, and generator load

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Summary

Introduction

The aircraft auxiliary power unit (APU) is designed to provide power for the aircraft independently [1]. The core of the APU is a small gas turbine engine providing power and compressed air [2,3]. Before the aircraft takes off, the APU provides power for lighting and air conditioning in the cabin, and provides the compressed air for starting the main engines of the aircraft. When an emergency situation occurs (e.g., fault of the main engine), the APU can be started again to help restart the main engines. The APU supplies power for lighting and air conditioning again. In this way, the main engines can be turned off earlier to save fuel and reduce noise and emissions

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