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      KCI등재 SCIE SCOPUS

      Effect of under-platform dampers on the forced vibration of high-speed rotating blades

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      https://www.riss.kr/link?id=A108580140

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      다국어 초록 (Multilingual Abstract)

      Under-platform dampers (UPDs) are commonly used to adapt turbine blade vibration characteristics by friction. However, acquiring their effect on the forced vibration of high-speed rotating blades is difficult. In this paper, the blade vibration experi...

      Under-platform dampers (UPDs) are commonly used to adapt turbine blade vibration characteristics by friction. However, acquiring their effect on the forced vibration of high-speed rotating blades is difficult. In this paper, the blade vibration experiments with atomised liquid-jet excitation in high-speed rotation were designed to compare the effects of different UPDs on blade vibration. Also, the damping ratios of different UPDS were obtained by numerical calculation methods. The experimental and computational results showed that when the mass of the dampers was within the appropriate range, the maximum vibration responses decreased significantly, and optimum mass of UPDs reduced the vibration by 28 % compared with the vibration responses without dampers. Moreover, the frequencies of the maximum blade response increased with the mass of the UPDs by up to 4.3 %. Meanwhile, the blade vibration response had multiple amplitude peaks due to the dry friction damping with installed UPDs.

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      참고문헌 (Reference) 논문관계도

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      2 A. B. Stanbridge, "Vibration measurements in a rotating blisk test rig using an LDV" 1-8, 2002

      3 K. Y. Sanliturk, "Underplatform dampers for turbine blades: theoretical modeling, analysis, and comparison with experimental data" 123 (123): 919-929, 2001

      4 S. Kwon, "Transient vibration characteristics of a rotating multi-packet blade system excited by multiple nozzle forces" 83 : 76-90, 2014

      5 L. Gaul, "The role of friction in mechanical joints" 54 (54): 93-106, 2001

      6 M. Ciavarella, "The influence of rounded edges on indentation by a flat punch" 212 (212): 319-327, 1998

      7 F. Götting, "Systematic mistuning of bladed disk assemblies with friction contacts" 257-267, 2004

      8 L. Panning, "Spatial dynamics of tuned and mistuned bladed disks with cylindrical and wedgeshaped friction dampers" 9 (9): 219-228, 2003

      9 J. Yuan, "Propagation of friction parameter uncertainties in the nonlinear dynamic response of turbine blades with underplatform dampers" 156 : 107673-, 2021

      10 C. Gastaldi, "On the relevance of a microslip contact model for under-platform dampers" 115 : 145-156, 2016

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      42 C. Yudi, "A method for the resonant response evaluation of blades system with underplatform dampers" 4 : 164-169, 2014

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