• 제목/요약/키워드: 유압 구동기

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A Heave Compensation System for Offshore Crane (해상 크레인의 상하동요 보상 시스템의 능동제어)

  • Seong, Hyung-seok;Choi, Hyeong-sik;Jeong, Seong-hoon;Lee, Sang-ki
    • Journal of Advanced Navigation Technology
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    • v.20 no.3
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    • pp.175-181
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    • 2016
  • This paper introduces a heave compensation system for offshore crane when it gets unexpected disturbances and external force. The dynamic model consists of crane assumed to be the rigid body, hydraulic driven winch, elastic rope and payload. To keep the payload from moving up and down, PD control algorithm is applied. By using the control, the oscillating amplitude of the payload is reduced. Also by using the estimated values involved with time-delay, the relative motion of payload in heave direction is dramatically shortened. This paper shows using the control algorithm with estimated value having time-delay 0.1 second is enough to heave compensation system.

Study on Dynamic Characteristics and Performance of Tip Jet Rotor Using Small-scaled Rotor (축소로터를 이용한 Tip Jet 로터의 성능 및 동특성 연구)

  • Kwon, Jae Ryong;Baek, Sang Min;Rhee, Wook;Lee, Jae Ha
    • Journal of Aerospace System Engineering
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    • v.12 no.2
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    • pp.30-36
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    • 2018
  • In this study, a small-scaled test system for a tip jet rotor was developed to contribute to the research on unmanned compound rotorcraft. The performance and dynamic characteristics of the tip jet rotor were investigated using the test system. The diameter of the tip jet rotor was set to 2m in consideration of the size of the test site and the pneumatic supply capacity of the. The rotating speed of the rotor was controlled by the pressure of the compressed air. The thrust and forces during the rotor rotation were measured using a load measuring device. A hydraulic actuator was installed for the dynamic test and full-bridge strain gages were attached to the root of each blade to measure the flap, lag, and torsion-wise responses generated when the rotor is excited by the actuator. The performance and dynamic characteristic tests were conducted at various rotor speeds and blade pitches. In order to check the validity of the test results, the results were also compared with the CAMRAD II analysis.