Nonlinear modal analysis of frictional ring damper for compressor blisk
Nonlinear modal analysis of frictional ring damper for compressor blisk
The use of integrally blisk is becoming popular because of the advantages in aerodynamic efficiency and mass reduction. However, in an integrally blisk, the lack of the contact interface leads to a low structural damping compared to an assembled bladed-disk. One emerging damping technique for the integrally blisk is based on the use of friction ring damper which exploits the contact interfaces at the underneath of the disk. In this paper, three different geometries of the ring dampers are investigated for damping enhancement of a blisk. A full-scale compressor blisk is considered as a case study where a node to node contact model is used to compute the contact forces. The dynamic behaviour of the blisk with the ring damper is investigated by using nonlinear modal analysis which allows a direct estimation of the damping generated by the friction interface. The damping performance for the different ring dampers are evaluated and compared. It appears that the damping efficiency as well as the shift in the resonant frequency for the different geometries are highly related to the nodal diameter and contact pressure/gap distributed within contact interface. The geometry of the ring damper has significant impact on the damping performance.
The American Society of Mechanical Engineers
Sun, Yekai
181c2a74-70e7-40ba-a016-664fb87dd74f
Yuan, Jie
4bcf9ce8-3af4-4009-9cd0-067521894797
Denimal, Enora
49fe7e8d-c02b-4ebe-b126-4ca1000c939d
Salles, Loïc
7c9f2690-2631-4f32-9c2f-07659cf3f19c
Sun, Yekai
181c2a74-70e7-40ba-a016-664fb87dd74f
Yuan, Jie
4bcf9ce8-3af4-4009-9cd0-067521894797
Denimal, Enora
49fe7e8d-c02b-4ebe-b126-4ca1000c939d
Salles, Loïc
7c9f2690-2631-4f32-9c2f-07659cf3f19c
Sun, Yekai, Yuan, Jie, Denimal, Enora and Salles, Loïc
(2021)
Nonlinear modal analysis of frictional ring damper for compressor blisk.
In Proceedings of the ASME Turbo Expo 2020: Turbomachinery Technical Conference and Exposition: Structures and Dynamics: Structural Mechanics, Vibration, and Damping; Supercritical CO2.
vol. 11,
The American Society of Mechanical Engineers.
10 pp
.
(doi:10.1115/GT2020-14277).
Record type:
Conference or Workshop Item
(Paper)
Abstract
The use of integrally blisk is becoming popular because of the advantages in aerodynamic efficiency and mass reduction. However, in an integrally blisk, the lack of the contact interface leads to a low structural damping compared to an assembled bladed-disk. One emerging damping technique for the integrally blisk is based on the use of friction ring damper which exploits the contact interfaces at the underneath of the disk. In this paper, three different geometries of the ring dampers are investigated for damping enhancement of a blisk. A full-scale compressor blisk is considered as a case study where a node to node contact model is used to compute the contact forces. The dynamic behaviour of the blisk with the ring damper is investigated by using nonlinear modal analysis which allows a direct estimation of the damping generated by the friction interface. The damping performance for the different ring dampers are evaluated and compared. It appears that the damping efficiency as well as the shift in the resonant frequency for the different geometries are highly related to the nodal diameter and contact pressure/gap distributed within contact interface. The geometry of the ring damper has significant impact on the damping performance.
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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
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Local EPrints ID: 479405
URI: http://eprints.soton.ac.uk/id/eprint/479405
PURE UUID: 650a721a-b411-4e42-85bd-ecb233eb0442
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Date deposited: 21 Jul 2023 16:33
Last modified: 17 Mar 2024 04:20
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Author:
Yekai Sun
Author:
Jie Yuan
Author:
Enora Denimal
Author:
Loïc Salles
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