@inproceedings{9f435dd41e644176bdd7fe747a85b7fc,
title = "Research on overall design of turboshaft engine based on data analysis method",
abstract = "In order to improve the reliability of the overall integrated design of the turboshaft engine, the overall performance and component design calculation model of the turboshaft engine is improved. Using coupling design as a medium, based on the existing turbo-engine database and technical data, the overall/component coupling design calculation model is established. According to the vortex engine parameter change trend database, the equilibrium design independent variables are selected, and the balance design constraints and targets are determined. By classifying the technical parameters, the turbo engine balance design method is explored and the turbo engine balance design is established. The results show that the design method has fast response speed and high reliability, and can obtain accurate coupling design feasible domain. The established balance design coefficient scheme optimization method provides a reference for optimizing the final design result by quantifying the balance coefficient. Using this method, a new generation of turboshaft engine with shaft power of 1566kw was designed. The fuel consumption rate was 0.255kg/(kW.h) and the power-to-mass ratio was 10.26kW/kg.",
keywords = "Balanced design, Coupling design, Data analysis, Overall design, Turboshaft engine",
author = "Chen, {Min Ze} and Chen, {Yu Chun} and Wei Fan and Zhang, {Shao Feng} and Li, {Xia Xin}",
note = "Publisher Copyright: {\textcopyright} 2019 IEEE.; 10th IEEE International Conference on Mechanical and Aerospace Engineering, ICMAE 2019 ; Conference date: 22-07-2019 Through 25-07-2019",
year = "2019",
month = jul,
doi = "10.1109/ICMAE.2019.8880964",
language = "英语",
series = "2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019",
publisher = "Institute of Electrical and Electronics Engineers Inc.",
pages = "158--163",
booktitle = "2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019",
}