Transient resonance passage of a mistuned bladed disk with and without underplatform dampers

Research output: Chapter in book/report/conference proceedingConference contributionResearchpeer review

Authors

  • K. Brinkmann
  • T. Hoffmann
  • L. Panning-Von Scheidt
  • H. Stüer

External Research Organisations

  • Siemens AG
View graph of relations

Details

Original languageEnglish
Title of host publicationConferece Proceedings - European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC
Publication statusPublished - 23 Apr 2023
Event15th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics 2023, ETC 2023 - Budapest, Hungary
Duration: 24 Apr 202328 Apr 2023

Publication series

NameProceedings of ...European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC
ISSN (Print)2313-0067

Abstract

In this work, the vibration response of an academic free-standing turbine blisk is analysed regarding transient resonance passages. Measurement data is recorded using strain gauges and tip timing to evaluate the blades first bending mode both linearly and with two types of underplatform dampers. These results are validated against steady-state responses and show good agreement towards each other. To examine the effects of a transient resonance passage, response functions of each blade are evaluated both with and without the underplatform dampers. It is shown that friction damping is able to inhibit any appearance of a transient ring-down. Additionally a multi-mass oscillator model with frictional contacts is analysed, that qualitatively exhibits the same dynamics as the measurements. Due to geometric mistuning all blades exhibit different vibration responses. This can lead to a transient amplitude amplification, which is observed on several blades. Analogously, this phenomenon can be mitigated by friction damping.

Keywords

    GEOMETRIC MISTUNING, TRANSIENT RESONANCE PASSAGE, TURBINE BLADE VIBRATION MEASUREMENT, UNDERPLATFORM DAMPER

ASJC Scopus subject areas

Cite this

Transient resonance passage of a mistuned bladed disk with and without underplatform dampers. / Brinkmann, K.; Hoffmann, T.; Panning-Von Scheidt, L. et al.
Conferece Proceedings - European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC. 2023. (Proceedings of ...European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC).

Research output: Chapter in book/report/conference proceedingConference contributionResearchpeer review

Brinkmann, K, Hoffmann, T, Panning-Von Scheidt, L & Stüer, H 2023, Transient resonance passage of a mistuned bladed disk with and without underplatform dampers. in Conferece Proceedings - European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC. Proceedings of ...European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC, 15th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics 2023, ETC 2023, Budapest, Hungary, 24 Apr 2023.
Brinkmann, K., Hoffmann, T., Panning-Von Scheidt, L., & Stüer, H. (2023). Transient resonance passage of a mistuned bladed disk with and without underplatform dampers. In Conferece Proceedings - European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC (Proceedings of ...European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC).
Brinkmann K, Hoffmann T, Panning-Von Scheidt L, Stüer H. Transient resonance passage of a mistuned bladed disk with and without underplatform dampers. In Conferece Proceedings - European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC. 2023. (Proceedings of ...European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC).
Brinkmann, K. ; Hoffmann, T. ; Panning-Von Scheidt, L. et al. / Transient resonance passage of a mistuned bladed disk with and without underplatform dampers. Conferece Proceedings - European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC. 2023. (Proceedings of ...European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC).
Download
@inproceedings{535b94e259ea4475831c19ca07ff7e48,
title = "Transient resonance passage of a mistuned bladed disk with and without underplatform dampers",
abstract = "In this work, the vibration response of an academic free-standing turbine blisk is analysed regarding transient resonance passages. Measurement data is recorded using strain gauges and tip timing to evaluate the blades first bending mode both linearly and with two types of underplatform dampers. These results are validated against steady-state responses and show good agreement towards each other. To examine the effects of a transient resonance passage, response functions of each blade are evaluated both with and without the underplatform dampers. It is shown that friction damping is able to inhibit any appearance of a transient ring-down. Additionally a multi-mass oscillator model with frictional contacts is analysed, that qualitatively exhibits the same dynamics as the measurements. Due to geometric mistuning all blades exhibit different vibration responses. This can lead to a transient amplitude amplification, which is observed on several blades. Analogously, this phenomenon can be mitigated by friction damping.",
keywords = "GEOMETRIC MISTUNING, TRANSIENT RESONANCE PASSAGE, TURBINE BLADE VIBRATION MEASUREMENT, UNDERPLATFORM DAMPER",
author = "K. Brinkmann and T. Hoffmann and {Panning-Von Scheidt}, L. and H. St{\"u}er",
note = "Publisher Copyright: Copyright {\textcopyright} by the Authors.; 15th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics 2023, ETC 2023 ; Conference date: 24-04-2023 Through 28-04-2023",
year = "2023",
month = apr,
day = "23",
language = "English",
series = "Proceedings of ...European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC",
booktitle = "Conferece Proceedings - European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC",

}

Download

TY - GEN

T1 - Transient resonance passage of a mistuned bladed disk with and without underplatform dampers

AU - Brinkmann, K.

AU - Hoffmann, T.

AU - Panning-Von Scheidt, L.

AU - Stüer, H.

N1 - Publisher Copyright: Copyright © by the Authors.

PY - 2023/4/23

Y1 - 2023/4/23

N2 - In this work, the vibration response of an academic free-standing turbine blisk is analysed regarding transient resonance passages. Measurement data is recorded using strain gauges and tip timing to evaluate the blades first bending mode both linearly and with two types of underplatform dampers. These results are validated against steady-state responses and show good agreement towards each other. To examine the effects of a transient resonance passage, response functions of each blade are evaluated both with and without the underplatform dampers. It is shown that friction damping is able to inhibit any appearance of a transient ring-down. Additionally a multi-mass oscillator model with frictional contacts is analysed, that qualitatively exhibits the same dynamics as the measurements. Due to geometric mistuning all blades exhibit different vibration responses. This can lead to a transient amplitude amplification, which is observed on several blades. Analogously, this phenomenon can be mitigated by friction damping.

AB - In this work, the vibration response of an academic free-standing turbine blisk is analysed regarding transient resonance passages. Measurement data is recorded using strain gauges and tip timing to evaluate the blades first bending mode both linearly and with two types of underplatform dampers. These results are validated against steady-state responses and show good agreement towards each other. To examine the effects of a transient resonance passage, response functions of each blade are evaluated both with and without the underplatform dampers. It is shown that friction damping is able to inhibit any appearance of a transient ring-down. Additionally a multi-mass oscillator model with frictional contacts is analysed, that qualitatively exhibits the same dynamics as the measurements. Due to geometric mistuning all blades exhibit different vibration responses. This can lead to a transient amplitude amplification, which is observed on several blades. Analogously, this phenomenon can be mitigated by friction damping.

KW - GEOMETRIC MISTUNING

KW - TRANSIENT RESONANCE PASSAGE

KW - TURBINE BLADE VIBRATION MEASUREMENT

KW - UNDERPLATFORM DAMPER

UR - http://www.scopus.com/inward/record.url?scp=85177651532&partnerID=8YFLogxK

M3 - Conference contribution

AN - SCOPUS:85177651532

T3 - Proceedings of ...European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC

BT - Conferece Proceedings - European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, ETC

T2 - 15th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics 2023, ETC 2023

Y2 - 24 April 2023 through 28 April 2023

ER -