• Title/Summary/Keyword: 댐퍼변위

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Measurement of Liquid Oscillation in Tuned Liquid Dampers using a Laser Doppler Vibrometer (레이저진동계를 사용한 동조액체댐퍼의 액체 진동 측정)

  • Shin, Yoon-Soo;Min, Kyung-Won;Kim, Junhee
    • Journal of the Computational Structural Engineering Institute of Korea
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    • v.29 no.6
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    • pp.513-519
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    • 2016
  • In this study, dynamic vertical displacement of liquid in the tuned liquid column damper(TLCD) is measured by a laser Doppler vibrometer(LDV) to overcome limitations of existing sensors and to leverage noncontact sensing. Addressing advantages of noncontact measurements, operational principles of the LDV to measure velocity and displacement of a target object in motion is explained. The feasibility of application of the LDV to measurement of liquid motion in the TLCD is experimentally explored. A series of shake table tests with the TLCD are performed to determine requirements of application of the LDV. Based on the experimental results, it is proved that the LDV works under the condition of adding dye to the liquid by increasing the intensity of reflected laser and thus validity is verified by comparison with a conventional wave height meter.

A Study on the Helicopter Composite Blade Impact Loads (헬리콥터 복합재 블레이드 충돌하중 연구)

  • Lee, Hyun-Cheol;Jeon, Boo-Il;Moon, Jang-Soo;Yee, Seok-June
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.37 no.2
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    • pp.181-186
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    • 2009
  • The objective of this study is ensuring safety of cabin when the blade impacts into a obstacle by verifying safety of the rotor mast and the transmission using impact loads calculated from the simulation. The rotor mast shall not fail and the transmission shall not be displaced into occupiable space when the main rotor composite blade impact into a 8 inch rigid cylinder in diameter on the outer 10% of the blade at operational rotor speed. To calculate the reaction loads at the spherical bearing and lead-lag damper, blade impact analysis was performed with FE model consist of composite blade, tree(or rigid cylinder) using elastic-plastic with damage material and several contact surfaces which were created to describe a progress of actual failure. Also, the reaction loads were investigated in change of blade rotation speed and pitch angle.