• 제목/요약/키워드: Tank-test

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구속모형시험을 이용한 KCS 선형의 조종성능 추정 (Prediction of Maneuverability of KCS Using Captive Model Test)

  • 신현경;최시훈
    • 대한조선학회논문집
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    • 제48권5호
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    • pp.465-472
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    • 2011
  • Recently, ultra large scale of ship is being ordered continuously and because of that, the accurate prediction of ship maneuverability in design stage becomes important matter. The model test like PMM test or CFD analysis are representative methods for predicting the maneuverability of ship. In this study, the captive model tests were carried out for predicting maneuverability of MOERI container ship(KCS) which is opened to the public using X-Y Carriage of Ocean Engineering Wide Tank of University of Ulsan. Considering the dimensions of tank, 2m class model ship was used for captive model test. CMT(Circular Motion Test) was performed for obtaining purer hydrodynamic coefficients related to yawing velocity. For getting hydrodynamic coefficients which cannot be obtained using CMT, PMM test(Planar Motion Mechanism test) were also performed. The maneuverability prediction results by simulation are compared with those of other research institutes.

빙수조 모형빙 활용 최적화 방안 연구 (A study on the optimum operation of model ice in Maritime & Ocean Engineering Research Institute(MOERI))

  • 김현수;이춘주;정우철
    • 한국기계기술학회지
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    • 제13권4호
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    • pp.109-115
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    • 2011
  • The ice tank is important facility to check the performance of the ship and offshore in ice condition before the construction. MOERI(Maritime & Ocean Engineering Research Institute) constructed ice model basin on the end of 2010. The ice technology to know the phenomena of ice near the ship and to estimate power of the ship in model scale is the main characteristic of the ice model basin. To achieve this goal in one ice sheet, making of test plan and feasibility check of test possibility have to review in the beginning stage of the every test. This paper describes the number of maximum resistance and self propulsion test in a sheet of level ice and proposes the methodology to optimize pack ice, rubble ice, brash ice and ice ridge test in MOERI ice tank. The feasibility of free running test to know maneuvering performance in ice field and some specific idea to measuring ice thickness and ice ridge shape was proposed.

부력엔진 독립시험 모듈 해양공학수조 시험 (Buoyancy Engine Independent Test Module Test in the Ocean Engineering Basin)

  • 이종무;김형우;정태환
    • 한국산업융합학회 논문집
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    • 제26권6_2호
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    • pp.1155-1162
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    • 2023
  • The Korea Research Institute of Ships and Ocean Engineering (KRISO), which is developing the core technology for the buoyancy engine of underwater gliders, has developed a test module that can vertically ascend and descend with a buoyancy engine to verify the performance of the developed buoyancy engine. The independent test module was tested in a 15 metre deep pit in the Ocean Engineering Basin to verify its ability to ascend and descend. In order to test at a shallower depth than the real sea, it was necessary to know the negative buoyancy value during descent and the time at which the buoyancy engine would be activated. To do this, we solved the equation of motion in the vertical direction to obtain these values and applied them to the tank test. To validate the usefulness of solving the equation, we also compared the depth of descent over time measured in the test with the results calculated from the solution.

Sloshing suppression by floating baffle

  • Kang, Hooi-Siang;Md Arif, Ummul Ghafir;Kim, Kyung-Sung;Kim, Moo-Hyun;Liu, Yu-Jie;Lee, Kee-Quen;Wu, Yun-Ta
    • Ocean Systems Engineering
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    • 제9권4호
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    • pp.409-422
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    • 2019
  • Sloshing is a phenomenon which may lead to dynamic stability and damages on the local structure of the tank. Hence, several anti-sloshing devices are introduced in order to reduce the impact pressure and free surface elevation of liquid. A fixed baffle is the most prevailing anti-sloshing mechanism compared to the other methods. However, the additional of the baffle as the internal structure of the LNG tank can lead to frequent damages in long-term usage as this structure absorbs the sloshing loads and thus increases the maintenance cost and downtime. In this paper, a novel type of floating baffle is proposed to suppress the sloshing effect in LNG tank without the need for reconstructing the tank. The sloshing phenomenon in a membrane type LNG tank model was excited under sway motion with 30% and 50% filling condition in the model test. A regular motion by a linear actuator was applied to the tank model at different amplitudes and constant period at 1.1 seconds. Three pressure sensors were installed on the tank wall to measure the impact pressure, and a high-speed camera was utilized to record the sloshing motion. The floater baffle was modeled on the basis of uniform-discretization of domain and tested based on parametric variations. Data of pressure sensors were collected for cases without- and with-floating baffle. The results indicated successful reduction of surface run-up and impulsive pressure by using a floating baffle. The findings are expected to bring significant impacts towards safer sea transportation of LNG.

코너프로텍션과 내조를 고려한 대용량 LNG 저장탱크 앵커스트랩의 구조설계를 위한 유한요소해석 (Structural Analysis for Design of Anchor Straps for a Large-Scale LNG Storage Tank with Corner Protection and Inner Tank)

  • 김성주;하성규;김성종;이영환
    • 대한기계학회논문집A
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    • 제35권12호
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    • pp.1543-1548
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    • 2011
  • 본 연구에서는 대용량 액화천연가스(LNG 즉 Liquefied Natural Gas) 저장탱크의 앵커스트랩(anchor strap)의 설계를 위한 구조해석이 수행되었다. 본 논문에 고려된 LNG 저장탱크는 반경이 40m 의 완전방호식 저장탱크로 크게 외조와 내조로 구성되고, 둘 사이의 공간은 단열재인 블랑켓과 펄라이트로 채워져있다. 앵커스트랩은 내조, 외조 및 코너프로텍션과 연결되어 있어 지진하중에 의한 내조의 파손을 방지하는 역할을 한다. 본 연구에서는 앵커스트랩만 고려한 단일모델과 실제 형상을 고려하여 앵커스트랩, 내조, 외조 및 코너프로텍션을 동시에 고려한 확장모델에 대해서 각각 유한요소해석을 수행하여 비교, 분석하였다. 하중조건으로는 LNG 의 유출상태 및 지진하중을 고려한 다섯 가지 경우를 고려하였고, 각 하중조건에 대한 두 모델의 Tresca 응력분포를 구하여 설계기준과 비교해 보았다.

잔향수조의 구조-음향 연성효과에 관한 수치 및 실험적 고찰 (Numerical and Experimental Investigation on Structure-acoustic Coupling Effect in a Reverberant Water Tank)

  • 박용;김국현;조대승;이종주
    • 대한조선학회논문집
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    • 제56권1호
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    • pp.94-101
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    • 2019
  • Underwater acoustic power should be measured in a free field, but it is not easy to implement. In practice, the measurement could be performed in a reverberant field such as a water-filled steel tank and concrete tank. In this case, the structure and the acoustic field are strongly or weakly coupled according to material properties of the steel and water. So, characteristics of the water tank must be investigated in order to get the accurate underwater acoustic power. In detail, modal frequencies, mode shapes of the structure and frequency response functions of the acoustic field could represent the characteristics of the reverberant water tank. In this paper, the structure-acoustic coupling has been investigated on a reverberant water tank numerically and experimentally. The finite element analysis has been carried out to estimate the structural and acoustical modal parameters under the dry and water-filled conditions, respectively. In order to investigate the structure-acoustic coupling effect, the numerical analysis has been performed according to the structure stiffness change of the water tank. The acoustic frequency response functions were compared with the numerical analysis and acoustic exciting test. From the results, the structural modal frequencies of the water-filled condition have been decreased compared to those of the dry condition in the low frequency range. The acoustic frequency response functions under the coupled boundary conditions showed different patterns from those under the ideal boundary conditions such as the pressure release and rigid boundary condition, respectively.

회전익항공기용 연료탱크 충돌충격시험 수치모사 연구 (Numerical Simulation of Crash Impact Test for Fuel Tank of Rotorcraft)

  • 김현기;김성찬;이종원;황인희;김경수
    • 한국전산구조공학회논문집
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    • 제24권5호
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    • pp.521-530
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    • 2011
  • 항공기 기체와의 체결부위가 많은 연료탱크는 체계연관성이 큰 대표적인 핵심 구성품 중의 하나로 다루어져 왔다. 회전익항공기에 광범위하게 적용되고 있는 내충격성 연료탱크는 항공기 추락 시 탑승자의 생존성 향상에 크게 기여하고 있다. 미육군에서는 항공기 추락 후 화재에 의한 인명손실을 원천적으로 방지하기 위해 군용 회전익기 역사의 초기 단계부터 연료탱크 고유의 내충격성에 관련된 군사규격을 제정하여 적용해 왔다. V-22 등의 잘 알려진 사례에 따르면 미군사규격(MIL-DTL-27422D)에서 요구하고 있는 연료탱크 충돌충격시험을 원활하게 통과하지 못하는 경우, 해당 연료탱크가 장착되는 항공기 자체의 개발일정에 심각한 지장을 초래한다. 연료탱크 충돌충격시험은 시편자체의 제작비용 및 준비기간이 상당히 소요되므로, 설계 초기단계부터 충돌충격시험에 대한 일련의 수치적 모사(numerical simulation)를 통해 실물에 의한 시행착오의 가능성을 최소화해야 한다. 본 연구에서는 충돌모사 프로그램인 Autodyn을 이용하여 연료탱크 충돌충격시험에 대한 수치적 모사를 수행하였으며, 그 결과로 구해진 등가응력 및 내부압력 평가를 통해 회전익항공기용 연료탱크의 내충격 성능을 고려한 설계방향을 제시하였다.

지진하중을 받는 정사각형 강재 액체저장탱크의 벽면 압력 응답 해석 (Earthquake-Induced Wall Pressure Response Analysis of a Square Steel Liquid Storage Tank)

  • 윤장혁;강태원;양현익;전종수
    • 한국지진공학회논문집
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    • 제22권5호
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    • pp.261-269
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    • 2018
  • This study examines earthquake-induced sloshing effects on liquid storage tanks using computation fluid dynamics. To achieve this goal, this study selects an existing square steel tank tested by Seismic Simulation Test Center at Pusan National University as a case study. The model validation was firstly performed through the comparison of shaking table test data and simulated results for the water tank subjected to a harmonic excitation. For a realistic estimation of the wall pressure response of the water tank, three recorded earthquakes with similar peak ground acceleration are applied:1940 El Centro earthquake, 2016 Gyeongju earthquake, and 2017 Pohang earthquake. Wall pressures monitored during the dynamic analyses are examined and compared for different earthquake motions and monitoring points, using power spectrum density. Finally, the maximum dynamic pressure for three earthquakes is compared with the design pressure calculated from a seismic design code. Results indicated that the maximum pressure from the El Centro earthquake exceeds the design pressure although its peak ground acceleration is less than 0.4 g, which is the design acceleration. On the other hand, the maximum pressure due to two Korean earthquakes does not reach the design pressure. Thus, engineers should not consider only the peak ground acceleration when determining the design pressure of water tanks.

동체 중앙에 연료탱크를 장착한 전투기의 섬광탄 운용 방안 연구 (A Study of Flare Operation Method for The Fighter with An External Center Fuel Tank)

  • 강치행;장영일;권기범;윤용인
    • 한국항공우주학회지
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    • 제40권7호
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    • pp.616-622
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    • 2012
  • 본 논문에서는 센터 파일론에 150갤런 외부 연료 탱크를 장착한 전투기의 전술기동 중 섬광탄 운용의 문제점을 검토하고 운용 가능한 방안을 제시하였다. 섬광탄 발사시 투하 궤적 및 외부 연료 탱크 수평 핀의 손상 범위를 풍동실험과 수치해석을 통해 분석하였다. 핀의 손상을 방지하기 위한 방안으로 1) 섬광탄 발사 각도를 조정하는 방안과 2) 핀의 형상을 변경하는 방안을 비교 검토 및 실용성을 분석한 결과 핀을 재설계하는 방안이 채택되었다. 풍동실험을 통하여 재설계한 수평 핀을 장착한 외부 연료 탱크의 투하 안전성을 평가하였다.