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The data driven surrogate model based dynamic design of aero-engine fan systems

The data driven surrogate model based dynamic design of aero-engine fan systems
The data driven surrogate model based dynamic design of aero-engine fan systems

High cycle fatigue failures of fan blade systems due to vibrational loads are of great concern in the design of aero engines, where energy dissipation by the relative frictional motion in the dovetail joints provides the main damping to mitigate the vibrations. The performance of such a frictional damping can be enhanced by suitable coatings. However, the analysis and design of coated joint roots of gas turbine fan blades are computationally expensive due to strong contact friction nonlinearities and also complex physics involved in the dovetail. In this study, a data driven surrogate model, known as the Nonlinear in Parameter AutoRegressive with eXegenous input (NP-ARX) model, is introduced to circumvent the difficulties in the analysis and design of fan systems. The NP-ARX model is a linear input-output model, where the model coefficients are nonlinear functions of the design parameters of interest, such that the Frequency Response Function (FRF) can be directly obtained and used in the system analysis and design. A simplified fan bladed disc system is considered as the test case. The results show that by using the data driven surrogate model, an efficient and accurate design of aero-engine fan systems can be achieved. The approach is expected to be extended to solve the analysis and design problems of many other complex systems.

The American Society of Mechanical Engineers
Zhu, Yun-Peng
0a20e7fa-d9aa-48d2-bcd5-233d4cf7ae76
Yuan, Jie
4bcf9ce8-3af4-4009-9cd0-067521894797
Lang, Z.Q.
40fdc555-bde8-49e9-adb8-5d7b6fc34f9c
Schwingshackl, C.W.
eb4a74ba-0670-4d94-a950-2031d54d4576
Salles, Loic
1b179daa-7bb9-4f34-8b5f-dfc05b496969
Kadirkamanathan, V.
944ce8e4-3f64-4e0a-9809-29355ee6294b
Zhu, Yun-Peng
0a20e7fa-d9aa-48d2-bcd5-233d4cf7ae76
Yuan, Jie
4bcf9ce8-3af4-4009-9cd0-067521894797
Lang, Z.Q.
40fdc555-bde8-49e9-adb8-5d7b6fc34f9c
Schwingshackl, C.W.
eb4a74ba-0670-4d94-a950-2031d54d4576
Salles, Loic
1b179daa-7bb9-4f34-8b5f-dfc05b496969
Kadirkamanathan, V.
944ce8e4-3f64-4e0a-9809-29355ee6294b

Zhu, Yun-Peng, Yuan, Jie, Lang, Z.Q., Schwingshackl, C.W., Salles, Loic and Kadirkamanathan, V. (2021) The data driven surrogate model based dynamic design of aero-engine fan systems. In ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition. vol. 10B, The American Society of Mechanical Engineers. 10 pp . (doi:10.1115/GT2020-14272).

Record type: Conference or Workshop Item (Paper)

Abstract

High cycle fatigue failures of fan blade systems due to vibrational loads are of great concern in the design of aero engines, where energy dissipation by the relative frictional motion in the dovetail joints provides the main damping to mitigate the vibrations. The performance of such a frictional damping can be enhanced by suitable coatings. However, the analysis and design of coated joint roots of gas turbine fan blades are computationally expensive due to strong contact friction nonlinearities and also complex physics involved in the dovetail. In this study, a data driven surrogate model, known as the Nonlinear in Parameter AutoRegressive with eXegenous input (NP-ARX) model, is introduced to circumvent the difficulties in the analysis and design of fan systems. The NP-ARX model is a linear input-output model, where the model coefficients are nonlinear functions of the design parameters of interest, such that the Frequency Response Function (FRF) can be directly obtained and used in the system analysis and design. A simplified fan bladed disc system is considered as the test case. The results show that by using the data driven surrogate model, an efficient and accurate design of aero-engine fan systems can be achieved. The approach is expected to be extended to solve the analysis and design problems of many other complex systems.

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More information

e-pub ahead of print date: 11 January 2021
Venue - Dates: ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition, Virtual, 2020-09-21 - 2020-09-25

Identifiers

Local EPrints ID: 478904
URI: http://eprints.soton.ac.uk/id/eprint/478904
PURE UUID: 2b6a76b7-68a2-4611-8df5-d16d4b7f14b6
ORCID for Jie Yuan: ORCID iD orcid.org/0000-0002-2411-8789

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Date deposited: 12 Jul 2023 16:47
Last modified: 17 Mar 2024 04:20

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Contributors

Author: Yun-Peng Zhu
Author: Jie Yuan ORCID iD
Author: Z.Q. Lang
Author: C.W. Schwingshackl
Author: Loic Salles
Author: V. Kadirkamanathan

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