Research on overall design of turboshaft engine based on data analysis method

Min Ze Chen; Yu Chun Chen; Wei Fan; Shao Feng Zhang; Xia Xin Li

doi:10.1109/ICMAE.2019.8880964

Research on overall design of turboshaft engine based on data analysis method

Min Ze Chen, Yu Chun Chen, Wei Fan, Shao Feng Zhang, Xia Xin Li

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

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.

Original language	English
Title of host publication	2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019
Publisher	Institute of Electrical and Electronics Engineers Inc.
Pages	158-163
Number of pages	6
ISBN (Electronic)	9781728155357
DOIs	https://doi.org/10.1109/ICMAE.2019.8880964
State	Published - Jul 2019
Externally published	Yes
Event	10th IEEE International Conference on Mechanical and Aerospace Engineering, ICMAE 2019 - Brussels, Belgium Duration: 22 Jul 2019 → 25 Jul 2019

Publication series

Name	2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019

Conference

Conference	10th IEEE International Conference on Mechanical and Aerospace Engineering, ICMAE 2019
Country/Territory	Belgium
City	Brussels
Period	22/07/19 → 25/07/19

Keywords

Balanced design
Coupling design
Data analysis
Overall design
Turboshaft engine

Access to Document

10.1109/ICMAE.2019.8880964

Cite this

Chen, M. Z., Chen, Y. C., Fan, W., Zhang, S. F., & Li, X. X. (2019). Research on overall design of turboshaft engine based on data analysis method. In 2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019 (pp. 158-163). Article 8880964 (2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019). Institute of Electrical and Electronics Engineers Inc.. https://doi.org/10.1109/ICMAE.2019.8880964

Chen, Min Ze ; Chen, Yu Chun ; Fan, Wei et al. / Research on overall design of turboshaft engine based on data analysis method. 2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019. Institute of Electrical and Electronics Engineers Inc., 2019. pp. 158-163 (2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019).

@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",

}

Chen, MZ, Chen, YC, Fan, W, Zhang, SF & Li, XX 2019, Research on overall design of turboshaft engine based on data analysis method. in 2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019., 8880964, 2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019, Institute of Electrical and Electronics Engineers Inc., pp. 158-163, 10th IEEE International Conference on Mechanical and Aerospace Engineering, ICMAE 2019, Brussels, Belgium, 22/07/19. https://doi.org/10.1109/ICMAE.2019.8880964

Research on overall design of turboshaft engine based on data analysis method. / Chen, Min Ze; Chen, Yu Chun; Fan, Wei et al.
2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019. Institute of Electrical and Electronics Engineers Inc., 2019. p. 158-163 8880964 (2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019).

Research output: Chapter in Book/Report/Conference proceeding › Conference contribution › peer-review

TY - GEN

T1 - Research on overall design of turboshaft engine based on data analysis method

AU - Chen, Min Ze

AU - Chen, Yu Chun

AU - Fan, Wei

AU - Zhang, Shao Feng

AU - Li, Xia Xin

PY - 2019/7

Y1 - 2019/7

N2 - 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.

AB - 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.

KW - Balanced design

KW - Coupling design

KW - Data analysis

KW - Overall design

KW - Turboshaft engine

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BT - 2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019

PB - Institute of Electrical and Electronics Engineers Inc.

T2 - 10th IEEE International Conference on Mechanical and Aerospace Engineering, ICMAE 2019

Y2 - 22 July 2019 through 25 July 2019

ER -

Chen MZ, Chen YC, Fan W, Zhang SF, Li XX. Research on overall design of turboshaft engine based on data analysis method. In 2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019. Institute of Electrical and Electronics Engineers Inc. 2019. p. 158-163. 8880964. (2019 IEEE 10th International Conference on Mechanical and Aerospace Engineering, ICMAE 2019). doi: 10.1109/ICMAE.2019.8880964

Research on overall design of turboshaft engine based on data analysis method

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Keywords

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