Vibration Optimization Design and Experiment for Support of Aeroengine High-Speed Rotor System

Weijian Nie; Xiaoguang Yang; Wangqun Deng; Hubiao Tang

doi:10.1007/978-981-99-8048-2_96

Vibration Optimization Design and Experiment for Support of Aeroengine High-Speed Rotor System

Weijian Nie^*
, Xiaoguang Yang
, Wangqun Deng
, Hubiao Tang

^*Corresponding author for this work

School of Energy and Power Engineering

Beihang University
AECC Hunan Aviation Powerplant Research Institute
Aero Engine Corporation of China

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

1 Scopus citations

Abstract

In view of the phenomenon that the vibration acceleration of the adapter support was too large during the dynamic characteristic test of a gas generator rotor, the cause analysis and vibration optimization research of the adapter support were carried out. The finite element method was used to establish the support modal calculation model, and the first five stages modal vibration modes and frequencies were obtained. It was determined that the main reason for the excessive vibration of the support was that there were multiple harmful resonance frequencies within the operating speed range of the rotor. Three kinds of test support structure were designed and compared, and the preferred scheme was verified by tests without gas generator rotor and with gas generator rotor respectively. The results indicate that the selected support does not have harmful resonance frequencies within the operating speed range of the rotor, and the vibration acceleration at high speeds is significantly reduced. The research provides a guarantee for the rotor dynamics test of aircraft engines and can be extended to the design of other test supports.

Original language	English
Title of host publication	Proceedings of the 2nd International Conference on Mechanical System Dynamics - ICMSD 2023
Editors	Xiaoting Rui, Caishan Liu
Publisher	Springer Science and Business Media Deutschland GmbH
Pages	1413-1424
Number of pages	12
ISBN (Print)	9789819980475
DOIs	https://doi.org/10.1007/978-981-99-8048-2_96
State	Published - 2024
Event	2nd International Conference of Mechanical System Dynamics, ICMSD 2023 - Beijing, China Duration: 1 Sep 2023 → 5 Sep 2023

Publication series

Name	Lecture Notes in Mechanical Engineering
ISSN (Print)	2195-4356
ISSN (Electronic)	2195-4364

Conference

Conference	2nd International Conference of Mechanical System Dynamics, ICMSD 2023
Country/Territory	China
City	Beijing
Period	1/09/23 → 5/09/23

Keywords

Aero-engine
Experimental verification
Finite element
High-speed rotor
Test support
Vibration modal

Access to Document

10.1007/978-981-99-8048-2_96

Cite this

Nie, W., Yang, X., Deng, W., & Tang, H. (2024). Vibration Optimization Design and Experiment for Support of Aeroengine High-Speed Rotor System. In X. Rui, & C. Liu (Eds.), Proceedings of the 2nd International Conference on Mechanical System Dynamics - ICMSD 2023 (pp. 1413-1424). (Lecture Notes in Mechanical Engineering). Springer Science and Business Media Deutschland GmbH. https://doi.org/10.1007/978-981-99-8048-2_96

Nie, Weijian ; Yang, Xiaoguang ; Deng, Wangqun et al. / Vibration Optimization Design and Experiment for Support of Aeroengine High-Speed Rotor System. Proceedings of the 2nd International Conference on Mechanical System Dynamics - ICMSD 2023. editor / Xiaoting Rui ; Caishan Liu. Springer Science and Business Media Deutschland GmbH, 2024. pp. 1413-1424 (Lecture Notes in Mechanical Engineering).

@inproceedings{fd45434cfad44e3e908efa15c8939860,

title = "Vibration Optimization Design and Experiment for Support of Aeroengine High-Speed Rotor System",

abstract = "In view of the phenomenon that the vibration acceleration of the adapter support was too large during the dynamic characteristic test of a gas generator rotor, the cause analysis and vibration optimization research of the adapter support were carried out. The finite element method was used to establish the support modal calculation model, and the first five stages modal vibration modes and frequencies were obtained. It was determined that the main reason for the excessive vibration of the support was that there were multiple harmful resonance frequencies within the operating speed range of the rotor. Three kinds of test support structure were designed and compared, and the preferred scheme was verified by tests without gas generator rotor and with gas generator rotor respectively. The results indicate that the selected support does not have harmful resonance frequencies within the operating speed range of the rotor, and the vibration acceleration at high speeds is significantly reduced. The research provides a guarantee for the rotor dynamics test of aircraft engines and can be extended to the design of other test supports.",

keywords = "Aero-engine, Experimental verification, Finite element, High-speed rotor, Test support, Vibration modal",

author = "Weijian Nie and Xiaoguang Yang and Wangqun Deng and Hubiao Tang",

note = "Publisher Copyright: {\textcopyright} The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd. 2024.; 2nd International Conference of Mechanical System Dynamics, ICMSD 2023 ; Conference date: 01-09-2023 Through 05-09-2023",

year = "2024",

doi = "10.1007/978-981-99-8048-2\_96",

language = "英语",

isbn = "9789819980475",

series = "Lecture Notes in Mechanical Engineering",

publisher = "Springer Science and Business Media Deutschland GmbH",

pages = "1413--1424",

editor = "Xiaoting Rui and Caishan Liu",

booktitle = "Proceedings of the 2nd International Conference on Mechanical System Dynamics - ICMSD 2023",

address = "德国",

}

Nie, W, Yang, X, Deng, W & Tang, H 2024, Vibration Optimization Design and Experiment for Support of Aeroengine High-Speed Rotor System. in X Rui & C Liu (eds), Proceedings of the 2nd International Conference on Mechanical System Dynamics - ICMSD 2023. Lecture Notes in Mechanical Engineering, Springer Science and Business Media Deutschland GmbH, pp. 1413-1424, 2nd International Conference of Mechanical System Dynamics, ICMSD 2023, Beijing, China, 1/09/23. https://doi.org/10.1007/978-981-99-8048-2_96

Vibration Optimization Design and Experiment for Support of Aeroengine High-Speed Rotor System. / Nie, Weijian; Yang, Xiaoguang; Deng, Wangqun et al.
Proceedings of the 2nd International Conference on Mechanical System Dynamics - ICMSD 2023. ed. / Xiaoting Rui; Caishan Liu. Springer Science and Business Media Deutschland GmbH, 2024. p. 1413-1424 (Lecture Notes in Mechanical Engineering).

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

TY - GEN

T1 - Vibration Optimization Design and Experiment for Support of Aeroengine High-Speed Rotor System

AU - Nie, Weijian

AU - Yang, Xiaoguang

AU - Deng, Wangqun

AU - Tang, Hubiao

N1 - Publisher Copyright: © The Author(s), under exclusive license to Springer Nature Singapore Pte Ltd. 2024.

PY - 2024

Y1 - 2024

N2 - In view of the phenomenon that the vibration acceleration of the adapter support was too large during the dynamic characteristic test of a gas generator rotor, the cause analysis and vibration optimization research of the adapter support were carried out. The finite element method was used to establish the support modal calculation model, and the first five stages modal vibration modes and frequencies were obtained. It was determined that the main reason for the excessive vibration of the support was that there were multiple harmful resonance frequencies within the operating speed range of the rotor. Three kinds of test support structure were designed and compared, and the preferred scheme was verified by tests without gas generator rotor and with gas generator rotor respectively. The results indicate that the selected support does not have harmful resonance frequencies within the operating speed range of the rotor, and the vibration acceleration at high speeds is significantly reduced. The research provides a guarantee for the rotor dynamics test of aircraft engines and can be extended to the design of other test supports.

AB - In view of the phenomenon that the vibration acceleration of the adapter support was too large during the dynamic characteristic test of a gas generator rotor, the cause analysis and vibration optimization research of the adapter support were carried out. The finite element method was used to establish the support modal calculation model, and the first five stages modal vibration modes and frequencies were obtained. It was determined that the main reason for the excessive vibration of the support was that there were multiple harmful resonance frequencies within the operating speed range of the rotor. Three kinds of test support structure were designed and compared, and the preferred scheme was verified by tests without gas generator rotor and with gas generator rotor respectively. The results indicate that the selected support does not have harmful resonance frequencies within the operating speed range of the rotor, and the vibration acceleration at high speeds is significantly reduced. The research provides a guarantee for the rotor dynamics test of aircraft engines and can be extended to the design of other test supports.

KW - Aero-engine

KW - Experimental verification

KW - Finite element

KW - High-speed rotor

KW - Test support

KW - Vibration modal

UR - https://www.scopus.com/pages/publications/85197350445

U2 - 10.1007/978-981-99-8048-2_96

DO - 10.1007/978-981-99-8048-2_96

M3 - 会议稿件

AN - SCOPUS:85197350445

SN - 9789819980475

T3 - Lecture Notes in Mechanical Engineering

SP - 1413

EP - 1424

BT - Proceedings of the 2nd International Conference on Mechanical System Dynamics - ICMSD 2023

A2 - Rui, Xiaoting

A2 - Liu, Caishan

PB - Springer Science and Business Media Deutschland GmbH

T2 - 2nd International Conference of Mechanical System Dynamics, ICMSD 2023

Y2 - 1 September 2023 through 5 September 2023

ER -

Nie W, Yang X, Deng W, Tang H. Vibration Optimization Design and Experiment for Support of Aeroengine High-Speed Rotor System. In Rui X, Liu C, editors, Proceedings of the 2nd International Conference on Mechanical System Dynamics - ICMSD 2023. Springer Science and Business Media Deutschland GmbH. 2024. p. 1413-1424. (Lecture Notes in Mechanical Engineering). doi: 10.1007/978-981-99-8048-2_96

Vibration Optimization Design and Experiment for Support of Aeroengine High-Speed Rotor System

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