返回
Multi-objective optimization for impeller structure parameters of fuel cell air compressor using linear-based boosting model and reference vector guided evolutionary algorithm
DOI:10.1016/j.apenergy.2024.123057.png)
摘要
En 中文
As a pivotal part of cathode air supply system, centrifugal air compressors play a central position in ensuring efficient operations of onboard fuel cells. To improve the overall performance of compressors, comprehensive performance tests were conducted and an integrated simulation model was developed by using computational fluid dynamics (CFD) methods. On this basis, the prediction performance of Linear -based Boosting models was investigated, and multi -objective optimization of impeller structural parameters was carried out through the Reference Vector Guided Evolutionary Algorithm (RVEA). Simulation results indicate that the impeller of the original compressor exhibits significant entropy increase, insufficient gas compression and serious energy dissipation, highlighting considerable room for design optimization. The eXtreme Gradient Boosting (XGBoost) model with 29 estimators has superior generalization ability and prediction performance, making it the preferred Boosting model for the compressor. Multi -objective optimizations have strong universality and rationality, resulting in a well -distributed and diversified final non -dominated solution set. The isentropic efficiency and pressure ratio of the Max_sigma solution are improved by 18.7% and 70.1%, while those of the Max_eta c solution are enhanced by 23.0% and 48.9%, respectively. After optimization, the gas experiences reduced shock loss, diminished entropy increase and enhanced flow stability. These findings can provide data support, theoretical basis and directional guidance for performance improvement of centrifugal air compressors.
Keyword:
Fuel cell
Centrifugal air compressor
CFD
XGBoost
RVEA
Multi -objective optimization
期刊
IF:
11
论文数:
2.6W
被引数:
17.8W
机构
引用论文
Crude oil time series prediction model based on LSTM network with chaotic Henry gas solubility optimization
ENERGY
IF9.4
Optimization of operating conditions for compressor performance by means of neural network inverse
APPLIED ENERGY
IF11
Computational fluid-dynamic investigation of a centrifugal compressor with inlet guide vanes for supercritical carbon dioxide power systems用于超临界二氧化碳动力系统的带有入口导叶的离心压缩机的计算流体动力学研究
ENERGY
IF9.4
Aerodynamic design and multi-dimensional performance optimization of supercritical CO2 centrifugal compressor超临界CO2离心压缩机气动设计及多维性能优化
Optimizing the performance of a single-shaft micro gas turbine engine by modifying its centrifugal compressor design通过修改其离心压缩机设计来优化单轴微型燃气涡轮发动机的性能
Numerical simulation of air flow through turbocharger compressors with dual volute design
APPLIED ENERGY
IF11

