• Title/Summary/Keyword: rotor hub system

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Evaluation of Near/Far Field and Directivity of Ultrasonic Transducer for Turbine Rotor Disc (터빈 로타 디스크의 초음파탐상을 위한 초음파탐촉자의 지향성 및 탐상범위)

  • Won, S.H.;Chang, H.K.;Cho, K.S.;Lee, J.O.;Lee, J.K.
    • Journal of the Korean Society for Nondestructive Testing
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    • v.18 no.3
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    • pp.163-171
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    • 1998
  • Near/far field length and directivity of transducers were investigated for the improvement and evaluation of the detectability of flaws in a disc. The reference block is fabricated for the disc of stage 6 in Yonggwang unit 1. The near/far field and directivity of an ultrasonic transducer with the center frequency of 5MHz were calculated for the inspection of the disc. These values showed good agreements with the experimental results. In the system composed of a wedge and a disc, those are evaluated theoretically and experimentally for the specimen with the artificial flaws of the size 2mm and 4mm and an ultrasonic transducer with the center frequency 5MHz and diameter 0.5inch. The detectability of keyway-flaw and detectable region for inspection were evaluated by using both tangential $45^{\circ}$ and $90^{\circ}$ transducers located at the distance of 53mm and 75mm from the disc hub, respectively.

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A study on the torsional frequency measurement of wind turbine blades (대형 풍력 블레이드의 비틀림 주파수 측정에 관한 고찰)

  • Ji-Hoon Kim;Jin Bum Moon;Min-Gyu Kang;Woo-Kyoung Lee;Si-Hyun Kim;Jisang Park
    • Journal of Wind Energy
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    • v.13 no.3
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    • pp.13-21
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    • 2022
  • When a wind turbine is designed, the dynamic stability of the system as well as the dynamic characteristics of the main components such as blades, hub, main shaft and tower must be evaluated. In particular, the natural frequencies of a blade, as a main load-generating component, need to be measured and assessed by component level testing. In conventional practice, the natural frequencies of a blade are determined as the measured frequencies near the reference frequencies provided by FE analysis results. But the reference frequencies are also uncertain since designers have difficulty distinguishing the torsional mode shape among the analysis results due to the complexity of its mode shape. So, in conventional practice, the determination of a measured torsional frequency inevitably contains uncertainty. Therefore, a novel method to definitely determine the torsional frequencies from the experimental data itself is necessary. In this paper, a new methodology to measure the torsional frequency of a blade was studied from the perspective of a modal test procedure, data processing method and mode determination logic. Finally, the validity of the method that can measure torsional frequency without reference FE analysis results was verified by applying it to an actual large wind turbine blade