一种燃气轮机冷却气流主动调节下涡轮叶片温度场快速预测的深度学习方法

IF 6.4 2区 工程技术 Q1 MECHANICS
Zhenhua Long , Bo Jiang , Minghao Ren , Xiangjiang He , Yang Bai , Fuxiang Dong , Jinfu Liu , Daren Yu
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引用次数: 0

摘要

风冷式涡轮机依靠从压缩机中抽出的冷却空气来确保安全运行。在部分负载条件下,热组件温度低于设计值,导致过度冷却和效率损失。主动调节涡轮冷却气流已被认为是提高效率的关键策略,但由于对调节后叶片温度场的理解有限,目前的开环系统缺乏精度。为了解决这个问题,本研究提出了一种深度学习方法,用于快速预测不同工况和冷却剂体积下的涡轮叶片温度场。建立了复杂冷却结构叶片的数值模型和三轴船用燃气轮机的热力学模型。采用拉丁超立方体采样和联合模拟,生成三维温度场数据集。利用L1和对抗损失的结合,开发和训练了一个具有注意机制的双分支条件生成对抗网络。该模型具有较高的精度,平均相对误差为0.1873%,结构相似度为0.9992。这种方法可以实现快速、准确的预测,并揭示操作和冷却剂调制条件对叶片温度的影响。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
A deep learning method for fast prediction of turbine vane temperature fields under active modulation of gas turbine cooling air flow
Air-cooled turbines rely on cooling air extracted from the compressor to ensure safe operation. Under partial load conditions, hot component temperatures fall below design values, causing excess cooling and efficiency losses. Actively modulating turbine cooling air flow has been recognized as a key strategy to enhance efficiency, yet current open-loop systems lack precision due to limited understanding of vane temperature fields after modulation. To address this, this study proposes a deep learning method for fast prediction of turbine vane temperature fields under varying operating conditions and coolant volumes. A numerical model of a vane with complex cooling structures and a thermodynamic model of a three-shaft marine gas turbine are established. Using Latin hypercube sampling and co-simulation, a dataset of three-dimensional temperature fields is generated. A dual-branch conditional generative adversarial network with an attention mechanism is developed and trained using a combination of L1 and adversarial losses. The model achieves high accuracy, with a mean relative error of 0.1873 % and structural similarity of 0.9992. This approach enables fast, accurate predictions and reveals the effects of operating and coolant modulation conditions on vane temperatures.
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来源期刊
CiteScore
11.00
自引率
10.00%
发文量
648
审稿时长
32 days
期刊介绍: International Communications in Heat and Mass Transfer serves as a world forum for the rapid dissemination of new ideas, new measurement techniques, preliminary findings of ongoing investigations, discussions, and criticisms in the field of heat and mass transfer. Two types of manuscript will be considered for publication: communications (short reports of new work or discussions of work which has already been published) and summaries (abstracts of reports, theses or manuscripts which are too long for publication in full). Together with its companion publication, International Journal of Heat and Mass Transfer, with which it shares the same Board of Editors, this journal is read by research workers and engineers throughout the world.
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