Exhaust Gas Temperature Prediction of Aero-Engine via Enhanced Scale-Aware Efficient Transformer

Author:

Liu Sijie1ORCID,Zhou Nan1,Song Chenchen1,Chen Geng1ORCID,Wu Yafeng1ORCID

Affiliation:

1. School of Power and Energy, Northwestern Polytechnical University, Xi’an 710072, China

Abstract

This research introduces the Enhanced Scale-Aware efficient Transformer (ESAE-Transformer), a novel and advanced model dedicated to predicting Exhaust Gas Temperature (EGT). The ESAE-Transformer merges the Multi-Head ProbSparse Attention mechanism with the established Transformer architecture, significantly optimizing computational efficiency and effectively discerning key temporal patterns. The incorporation of the Multi-Scale Feature Aggregation Module (MSFAM) further refines 2 s input and output timeframe. A detailed investigation into the feature dimensionality was undertaken, leading to an optimized configuration of the model, thereby improving its overall performance. The efficacy of the ESAE-Transformer was rigorously evaluated through an exhaustive ablation study, focusing on the contribution of each constituent module. The findings showcase a mean absolute prediction error of 3.47∘R, demonstrating strong alignment with real-world environmental scenarios and confirming the model’s accuracy and relevance. The ESAE-Transformer not only excels in predictive accuracy but also sheds light on the underlying physical processes, thus enhancing its practical application in real-world settings. The model stands out as a robust tool for critical parameter prediction in aero-engine systems, paving the way for future advancements in engine prognostics and diagnostics.

Publisher

MDPI AG

Reference34 articles.

1. Aero-engine health monitoring with real flight data using whale optimization algorithm based artificial neural network technique;Balakrishnan;Opt. Mem. Neural Netw.,2021

2. A modeling method for aero-engine by combining stochastic gradient descent with support vector regression;Ren;Aerosp. Sci. Technol.,2020

3. Physics of failure-based reliability prediction of turbine blades using multi-source information fusion;Li;Appl. Soft Comput.,2018

4. A fault diagnosis approach for gas turbine exhaust gas temperature based on fuzzy c-means clustering and support vector machine;Wang;Math. Probl. Eng.,2015

5. Energy, environment and enviroeconomic analyses and assessments of the turbofan engine used in aviation industry;Tuzcu;Environ. Prog. Sustain. Energy,2021

Cited by 1 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

同舟云学术

1.学者识别学者识别

2.学术分析学术分析

3.人才评估人才评估

"同舟云学术"是以全球学者为主线,采集、加工和组织学术论文而形成的新型学术文献查询和分析系统,可以对全球学者进行文献检索和人才价值评估。用户可以通过关注某些学科领域的顶尖人物而持续追踪该领域的学科进展和研究前沿。经过近期的数据扩容,当前同舟云学术共收录了国内外主流学术期刊6万余种,收集的期刊论文及会议论文总量共计约1.5亿篇,并以每天添加12000余篇中外论文的速度递增。我们也可以为用户提供个性化、定制化的学者数据。欢迎来电咨询!咨询电话:010-8811{复制后删除}0370

www.globalauthorid.com

TOP

Copyright © 2019-2024 北京同舟云网络信息技术有限公司
京公网安备11010802033243号  京ICP备18003416号-3