• Title/Summary/Keyword: 액화가스운반선

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Applications of the Multiobjective Optimization Method in Main Particular Selection (선박의 주요치수 선정에 있어서 다목적함수 최적화의 응용)

  • Dong-Kon Lee;Soo-Young Kim;Soo-Chul Shin
    • Journal of the Society of Naval Architects of Korea
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    • v.32 no.2
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    • pp.10-21
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    • 1995
  • In this paper, main particulars of a ship are optimized by the multiobjective optimization method which can offer more information to designer. To analyze the effect of a ship building cost and operating cost in the optimum design of a ship, the multiobjective optimization is performed with objective functions of building and operating costs. And Required Freight Rate(RFR) is also calculated as dependent variable. The design model was developed for the Liquefied Natural Gas(LNG) carrier with longer operating distance. The LNG carrier has some characteristics such as higher speed and building cost in comparison with other commercial ships.

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A Study for Deformation During the Erection of LNG Carrier's Motor/Compressor Room (액화천연가스운반선 모터/컴프레서 룸의 탑재 시 처짐에 대한 검토 사례 소개)

  • Oh, Chang-Min;Jang, Yoo-Soo;Oh, Dong-Yoon;Yang, Jin-Seok
    • Special Issue of the Society of Naval Architects of Korea
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    • 2007.09a
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    • pp.1-6
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    • 2007
  • To improve productivity of the LNG carriers which are growing bigger and bigger, many researches are being carried out by shipyards. In this regard, we reviewed possible problems which could occur during the erection of 216K LNG carrier's motor/compressor room with all outfittings pre-installed. As a first item, the weights of hull and outfittings were precisely estimated to make sure that the erection is carried out within yard's capability. In the next place, deflection and safety of the structure were verified by FEM analysis. As a result, the erection was finished successfully and yard's productivity was also improved. This review is a good example which shows the importance of through study and preparation for improving yard's productivity which is already reached its limit.

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Thermal Analysis Comparison of IMO with USCG Design Condition for the INGC During the Cool-down Period (급냉각기간에서 IMO설계조건과 USCG 설계조건에 대한 LMGC 화물탱크의 열해석 비교)

  • Lee, Jung-Hye
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.28 no.11
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    • pp.1390-1397
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    • 2004
  • This study is concerned with the thermal analysis during the cool-down period of 135,000㎥ class GT-96 membrane type LNG carrier under IMO and USCG design condition. During the cool-down period, the spraying rate for the NG cooling decreases as the temperature of NG falls down from -4$0^{\circ}C$ to -l3$0^{\circ}C$, and the spraying rate for the cooling of the insulation wall increases as the temperature gradient of the insulation wall is large. It was confirmed that there existed the largest temperature decrease at the first barrier and the first insulation, which are among the insulation wall, especially in the top side of the insulation wall under IMO and USCG design condition. Also, as the NG temperature distribution is fixed, the outer temperature condition under the design condition has influence on the temperature variation at the insulation. By the 3-D numerical calculation about the cargo tank and the cofferdam during the cool-down period, the temperature variation in hulls and insulations is precisely predicted under IMO and USCG design condition. From the comparison between two conditions; IMO design condition shows more severe temperature gradient than USCG design condition, therefore, it provides the conservative estimation of the BOG.

Thermal Analysis for the GT-96 Membrane Type LNGC during the Cool-down Period (GT-96 멤브레인형 LNGC의 급냉기간에서의 열해석)

  • Lee, Jung-Hye;Choi, Hyun-Kue;Choi, Soon-Ho;Oh, Cheol;Kim, Myoung-Hwan;Kim, Kyung-Kun
    • Proceedings of the KSME Conference
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    • 2004.04a
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    • pp.1346-1351
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    • 2004
  • This study is concerned with the thermal analysis during the cool-down period of 135,000 $m^3$ class GT-96 membrane type LNG carrier under IMO design condition. The cool-down is performed to cool the insulation wall and the natural gas in cargo tank for six hours to avoid the thermal shock at the start of loading of $-163^{\circ}C$ LNG. During the cool-down period, the spraying rate for the NG cooling decreases as the temperature of NG falls clown from $-40^{\circ}C$ to $-130^{\circ}C$ and the spraying rate for the insulation wall cooling increases as the temperature gradient of the insulation wall is large. It was confirmed that there existed the largest temperature decrease at the 1 st barrier and 1st insulation, which are among the insulation wall, especially in the top side of the insulation wall. By the 3-D numerical calculation about the cargo tank and the cofferdam during the cool-down period, the temperature variation in hulls and insulations is precisely predicted.

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Hydrodynamic Forces and Maneuvering Characteristics of Ships at Low Advance Speed (저속시 선체에 작용하는 조종유체력 및 조종성능에 관한 연구)

  • Kyoung-Ho Sohn
    • Journal of the Society of Naval Architects of Korea
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    • v.29 no.3
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    • pp.90-101
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    • 1992
  • Some practical methods have already been proposed for predicting the characteristics of ship manoeuvring motions at relatively high advance speed. However, these methods can hardly be applied to motions of ships in starting, stoppint, backing and slow steaming conditions, even though such extensive motions are of vital importance from a safety point of view particularly in harbour areas. The method presented here aims at predicting the characteristics of ship manoeuvring at low advance speed, which covers starting, stopping, backing and slow steaming conditions. The force mathematical models at large angles of incidence to the hull as well as under the tilde range of propeller operations are formulated. Simulations of various manoeuvres at low advance speed are carried out for two types of merchant ship, i.e. a LNGC and a VLCC. Comparisons between simulations and corresponding full-scale measurements or free-running model tests provide a first verification of the proposed mathematical models.

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Experimental examination for effect of voids on bonding performance in cryogenic temperature condition (내부 기공이 극저온에서 접착강도에 미치는 영향에 대한 실험적 고찰)

  • Shon, Min-Young;Kim, Jong-Ho;Kim, Jong-Hak
    • Composites Research
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    • v.22 no.2
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    • pp.14-17
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    • 2009
  • Adhesive joints are widely used for structural joining applications in various fields and environmental conditions. Polyurethane adhesive is using for LNG carrier with cryogenic temperature condition. In industrial application of polyurethane adhesive, void of adhesive layer is often discussed regarding its effects on bonding properties. In present study, artificial void were prepared on Polyurethane adhesive layer with various size and location. The single lap shear test was carried out by using prepared specimens under $-170^{\circ}C$. As a result, it was confirm that the void of adhesive layer didn't affect the adhesion properties independent of their size and location.

Impact Properties and Fractography of Structural Materials for LNG Tank at Cryogenic Temperatures (LNG 저장탱크용 재료의 극저온 충격특성과 파면해석)

  • Shin Hyung-Seop;Lee Hae-Moo;Shin Ju-Yeong;Park Jong-Seo
    • Journal of the Korean Institute of Gas
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    • v.2 no.1
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    • pp.99-106
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    • 1998
  • In order to investigate the impact properties of structural materials for LNG tank, instrumented Charpy impact tests were carried out at cryogenic temperatures. $9\%$ Ni steel showed a superior fracture resistance because of less degradation in toughness until 77 K. From the load-deflection curve obtained by an instrumented methods it was found that with the decrease of temperature from 173 K to 77 K, the peak load in the curve increased, but the total absorbed energy decreased. In addition, the energy absorbed during the crack growth was larger than one absorbed in the process of crack initiation. In SUS304L material, the energy absorbed in the process of the crack initiation was relatively large, but the energy absorbed in the process of crack growth was small, the behavior of absorbed energy was well agreed with the observations of the fracture surface which showed a relatively smooth fracture surface. The absorbed Charpy impact energy in the case of A5083 alloy was lower as compared with other steels, and some cracks were observed along the crack propagation direction at the fracture surface of 77 K.

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Effect of graphene oxide on mechanical characteristics of polyurethane foam (산화그래핀이 폴리우레탄 폼 기계적 강도에 미치는 영향)

  • Kim, Jong-Min;Kim, Jeong-Hyeon;Choe, Young-Rak;Park, Sung Kyun;Park, Kang Hyun;Lee, Jae-Myung
    • Journal of Advanced Marine Engineering and Technology
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    • v.40 no.6
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    • pp.493-498
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    • 2016
  • In the present study, graphene oxide based polyurethane foams were manufactured as a part of the development process of mechanically strengthened polyurethane foam insulation material. This material is used in a liquefied natural gas carrier cargo containment system. The temperature of the containment system is $-163^{\circ}C$. First, graphene oxide was synthesized using the Hummers' method, and it was supplemented into polyol-isocyanate reagent by considering a different amount of graphene oxide weight percent. Then, a bulk form of graphene-oxide-polyurethane foam was manufactured. In order to investigate the cell stability of the graphene-oxide-polyurethane foam, its microstructural morphology was observed, and the effect of graphene oxide on microstructure of the polyurethane foam was investigated. In addition, the compressive strength of graphene-oxide-polyurethane foam was measured at ambient and cryogenic temperatures. The cryogenic tests were conducted in a cryogenic chamber equipped with universal testing machine to investigate mechanical and failure characteristics of the graphene-oxide-polyurethane foam. The results revealed that the additions of graphene oxide enhanced the mechanical characteristics of polyurethane foam. However, cell stability and mechanical strength of graphene-oxide-polyurethane foam decreased as the weight percent of graphene oxide was increased.

Cryogenic Mechanical Characteristics of Laminated Plywood for LNG Carrier Insulation System (LNG운반선 방열시스템에 적용되는 적층형 플라이우드의 극저온 기계적 특성 분석)

  • Kim, Jeong-Hyeon;Park, Doo-Hwan;Choi, Sung-Woong;Lee, Jae-Myung
    • Journal of Ocean Engineering and Technology
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    • v.31 no.3
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    • pp.241-247
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    • 2017
  • Plywood, which is created by bonding an odd number of thin veneers perpendicular to the grain orientation of an adjacent layer, was developed to supplement the weak points such as contraction and expansion of conventional wood materials. With structural merits such as strength, durability, and good absorption against impact loads, plywood has been adopted as a structural material in the insulation system of a membrane type liquefied natural gas (LNG) carrier. In the present study, as an attempt to resolve recent failure problems with plywood in an LNG insulation system, conventional PF (phenolic-formaldehyde) resin plywood and its alternative MUF (melamine-urea-formaldehyde) resin bonded plywood were investigated by performing material bending tests at ambient ($20^{\circ}C$) and cryogenic ($-163^{\circ}C$) temperatures to understand the resin and grain effects on the mechanical behavior of the plywood. In addition, the failure characteristics of the plywood were investigated with regard to the grain orientation and testing temperature.

Sloshing Impact Response Analysis for Insulation System of LNG CCS Considering Elastic Support Effects of Hull Structures (선체구조의 탄성지지 효과를 고려한 LNG 운반선 방열구조의 슬로싱 충격응답 해석법에 관한 연구)

  • Nho, In Sik;Ki, Min-Seok;Kim, Sung-Chan;Lee, Jang Hyun;Kim, Yonghwan
    • Journal of Ocean Engineering and Technology
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    • v.31 no.5
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    • pp.357-363
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    • 2017
  • The sloshing pressure acting on a membrane-type LNG CCS is a typical irregular impact load, and the structural response of a tank system induced by sloshing also shows very complex behavior, including fluid structure interaction. Therefore, it is not easy to accurately estimate the sloshing impact pressures and resulting structural response. Moreover, a huge time consuming process to deal with the enormous pressure data obtained during a model tank test and the following structural analysis would be inevitable. To reduce the computation time for structural analysis, in this study, a rational structural modeling strategy was considered, and a simplified scheme to analyze the dynamic structural responses of an LNG CCS was introduced, which was based on the concept of the linear combination of the triangular response functions obtained by a transient response analysis of structures under unit triangular impact pressure. A structural analysis of a real Mark III membrane type insulation system under the sloshing impact pressure time histories obtained by model tests was performed using the various proposed structural models and simplified analysis scheme. The results were investigated in detail, including the elastic support effects of the hull structure.