• 한국가스학회지
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• 제22권4호
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• pp.1-6
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• 2018

IMO에서 규정하는 LNG 벙커링 선박용 연료 탱크 중 C형 가압탱크는 내외 2중 용기로 구성된 초저온 탱크에 $10^{-2}$ Torr 진공과 펄라이트 단열재가 충전되는 것이다. 그러나 이 단열방식은 LNG 기화량이 하루당 2.0 % 내외로 증발율이 커서 보다 단열효과가 좋은 탱크가 요구되어 진다. 본 연구에서는 내외탱크 사이에 고진공을 적용하고 외부탱크의 내벽체에 중간 단열로 펄라이트 진공단열을 적용하는 단열 방식을 새로이 고안하여 열해석을 수행하였다. 이의 장점으로는 진공 공간의 감소로 고진공 형성 시간을 크게 감소되고, 진공도 $10^{-4}$ Torr 이하에서 하루당 증발율이 0.16 %에 불과한 매우 효율이 높은 탱크 단열방식이 되었다. 만약 현재의 IMO C형 탱크의 진공펄라이트 단열에서 진공이 파괴되는 경우, C형 탱크는 하루당 4.9 %의 증발이 발생하고 새 고안 탱크는 5.23 %로 거의 동일하게 된다.

• 한국초전도ㆍ저온공학회논문지
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• 제16권4호
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• pp.71-77
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• 2014

For a long-term space mission, filling process of cryogenic liquid propellant is operated on a space vehicle in space. A vent process during transfer and filling of cryogenic propellant is needed to maintain the fuel tank pressure at a safe level due to its volatile characteristic. It is possible that both liquid and vapor phases of the cryogenic propellant are released simultaneously to outer space when the vent process occurs under low gravity environment. As a result, the existing filling process with venting not only accompanies wasting liquid propellant, but also consumes extra fuel to compensate for the unexpected momentum originated from the vent process. No-Vent Fill (NVF) method, a filling procedure without a venting process of cryogenic liquid propellant, is an attractive technology to perform a long-term space mission. In this paper, the preliminary experimental results of the NVF process are described. The experimental set-up consists of a 9-liter cryogenic liquid receiver tank and a supply tank. Liquid nitrogen ($LN_2$) is used to simulate the behavior of cryogenic propellant. The whole situation in the receiver tank during NVF is monitored. The major experimental parameter in the experiment is the mass flow rate of the liquid nitrogen. The experimental results demonstrate that as the mass flow rate is increased, NVF process is conducted successfully. The quality and the inlet temperature of the injected $LN_2$ are affected by the mass flow rate. These parameters determine success of NVF.

• 한국추진공학회지
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• 제11권2호
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• pp.54-61
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• 2007

액체로켓추진시스템에서 추진제 가압시스템은 추진제가 저장되어 있는 탱크의 얼리지 공간에 가압제인 가스를 제어된 압력으로 공급하는 것이다. 이러한 추진제 가압시스템의 가장 중요한 설계변수는 가압제를 저장하고 있는 탱크에서 토출되는 가압제의 온도이며, 기체상태인 가압제의 밀도는 토출되는 가압제의 온도에 따라 민감하게 변한다. 일반적으로 고추력을 요구하는 극저온 추진제가 적용되는 추진기관에서는 가압제를 고밀도 고압으로 저장하여 가압제 탱크의 무게를 줄이기 위하여 가압제 저장탱크를 극저온 추진제 탱크 내부에 설치하는 극저온 저장 가압시스템을 사용한다. 본 연구에서는 가압제가 가압제 저장탱크에서 토출 될 때 강하되는 온도 변화를 실험 및 해석을 통하여 고찰하였다. 본 연구에 적용된 유체는 외부유체로 공기와 액체산소 그리고 가압제로 $GN_2$와 GHe를 각각 사용하였다.

• 한국전산구조공학회논문집
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• 제30권2호
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• pp.95-102
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• 2017

이 논문에서는 LNG 탱크를 지진으로부터 격리시키는 면진장치의 일종인 마찰진자시스템(FPS)의 성능변화에 따른 구조물 응답 및 지진취약도를 분석하였다. 마찰진자시스템(FPS)에 사용되는 마찰재 시편을 PVDF와 $TiO_2$의 배합비율에 따라 제작하였다. 제작한 마찰재 시편의 물성을 면진받침에 적용하여 구조물의 가속도 응답 및 외조 콘크리트의 하부 모멘트에 대하여 분석하고 각각의 한계상태에 대해 지진취약도를 분석하였다. 구조물의 지진취약도 분석을 통한 최적의 배합비를 가지는 마찰재 선정을 위해 각 한계상태에 따른 지진취약도 곡선의 가중치 설정 후 조합이 필요한 것을 확인하였다. 이를 통하여 다양한 구조물에 적용되는 마찰진자시스템의 요구 성능을 만족하는 최적의 마찰재 선정이 가능할 것으로 기대된다.

• 한국태양에너지학회:학술대회논문집
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• 한국태양에너지학회 2009년도 추계학술발표대회 논문집
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• pp.80-85
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• 2009

Mathematical modeling and performance simulation results were shown for the solar thermal storage system which used heat pipe. The thermal storage system was composed of thermal storage tank and charging/discharging heat exchanger with one by the heat pipes. Heat pipe heat exchanger was attached to system, and could carry out charging and discharging to thermal storage tank at the same time. Height of the thermal storage tank was 600 mm, and that of the charging/discharging heat exchanger was 400 mm. Length of the heat pipe was the same as the total height of thermal storage system, and outer and inner diameter were 25.4 mm(O.D.) and 21.4 mm(I.D.) respectively. Diameter of the circular was 43 mm(O.D.), and fin geometries were considered as the design parameters. High temperature phase change material(PCM), $KNO_3$ and low temperature PCM, $LINO_3$ were charged to storage tank to adjust working temperature. Total size of thermal storage system able to get heat capacity more than 500 kW was calculated and the results were shown in this study. Number of heat pipe was required more than maximum 500, and total length of thermal storage system was calculated to the more than maximum 3 m at various condition.

• 한국수소및신에너지학회논문집
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• 제31권2호
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• pp.194-201
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• 2020

Recently, Type 2 high-pressure hydrogen storage tank is studied due to fast defect detection, easy manufacturing, and cost efficiency. Moreover, the dry winding a high-strength metal wire will make increased economic efficiency compare with the wet winding method and the carbon/glass fiber winding method. In this study, a theoretical study on the dry winding of a Type 2 high pressure hydrogen tank using a metal wire was done, and the equations of the total stress on the aligned and the staggered winding for the hoop winding were derived, and the following results were obtained by using these equations. As the diameter of the metal wire, the number of winding layers, and the outer diameter of the liner increase, the maximum stress decreases, but the difference between the maximum stress occurring in the aligned winding and the staggered winding increases. As the pressure increases, the thickness of the winding layer increases, but as the strength of the metal wire increases, the thickness of the winding layer decreases. In addition, regardless of the strength of the metal wire, the thickness of the winding layer of the staggered winding was about 13.4% thinner than that of the aligned winding.

• Journal of Advanced Marine Engineering and Technology
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• 제39권9호
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• pp.876-880
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• 2015

IMO의 규제인 신조 선박에 대한 NOx 80% 감축의 2016년 발효를 앞두고, 청정에너지인 LNG연료 선박 및 벙커링 선박의 보급이 유럽 선진국들을 중심으로 추진되고 있다. LNG 저장탱크는 LNG 벙커링의 필수 설비로 현재의 액체질소 등을 저장하는 극저온 액체 저장탱크와 동일한 구조이며, IMO의 "C"형 가압탱크인 내외 용기로 구성된 2중 탱크에 진공펄라이트 단열재가 충전되는 형식이다. 그러나 이 단열방식은 진공작업이 어렵고 일 LNG 기화량이 2.0 % 내외가 되어 보다 고효율의 탱크가 요구되어 진다. 본 연구에서는 진공과 단열재를 분리하여 내외탱크에 고진공을 적용하고 외부 탱크에 우레탄폼을 가설시킨 탱크 단열 방식을 새로이 고안하여 열해석을 수행하였다. 해석결과 본 개발 탱크는 진공도가 $10^{-3}Torr$ 이하일 때 일 기화량이 0.03 % 이하로 매우 적게 유지될 수 있고, $10^{-4}Torr$ 이하가 되면 일 기화량이 0.11 %가 되었다. 진공이 파괴되는 경우에도 현재 진공펄라이트 단열은 일 4.9 %의 증발이 발생하나, 새 고안 탱크는 일 증발율이 4.12 %가 되는 매우 효율이 높고 안전한 LNG 탱크 단열방식이 되었다.

• 대한조선학회논문집
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• 제40권5호
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• pp.36-42
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• 2003

A CFD simulation technique has been developed to handle the unsteady body motion with large amplitude by use of overlapping multi-block grid system. The three-dimensional, viscous and incompressible flow around body is investigated by solving the Navier-Stokes equations, and the motion of body is represented by moving effect of the grid system. Composite grid system is employed in order to deal with both the body motion with large amplitude and the condition of numerical wave maker in convenience at the same time. The governing equations, Navier-Stokes (N-S) and continuity equations, are discretized by a finite volume method, in the framework of an O-H type boundary-fitted grid system (inner grid system including test model) and a rectangular grid system (outer grid system including simulation equipments for generation of wave environments). If this study, several flow configurations, such as an oscillating cylinder with large KC number, are studied in order to predict and evaluate the hydrodynamic forces. Furthermore, the motion simulation of a Series 60 model advancing in a uniform flow under the condition of enforced roll motion of angle 20$^{\circ}$ is performed in the developed numerical wave tank.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2005년도 춘계학술발표대회 논문집
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• pp.17-20
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• 2005

In-situ structural health monitoring of filament wound pressure tanks were conducted during water-pressurizing test using embedded fiber Bragg grating (FBG) sensors. We need to monitor inner strains during working in order to verify the health condition of pressure tanks more accurately because finite element analyses on filament wound pressure tanks usually show large differences between inner and outer strains. Fiber optic sensors, especially FBG sensors can be easily embedded into the composite structures contrary to conventional electric strain gages (ESGs). In addition, many FBG sensors can be multiplexed in single optical fiber using wavelength division multiplexing (WDM) techniques. We fabricated a standard testing and evaluation bottle (STEB) with embedded FBG sensors and performed a water-pressurizing test. In order to increase the survivability of embedded FBG sensors, we suggested a revised fabrication process for embedding FBG sensors into a filament wound pressure tank, which includes a new protecting technique of sensor heads, the grating parts. From the experimental results, it was demonstrated that FBG sensors can be successfully adapted to filament wound pressure tanks for their structural health monitoring by embedding.

• 한국분무공학회지
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• 제1권4호
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• pp.46-53
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• 1996

The present study is aiming at improving the performance of main nozzle of an air jet loom with a modified reed and auxiliary nozzles. The double coaxial pipe jets consisting of a central air jet and an annular air jet have been experimentally investigated. The duter jet has a potential core and a constant velocity. The inner jet through an inner long pipe is induced by the subatmospheric pressure near the inner nozzle edge, and the jet velocity of an inner pipe is always lower than that of a outer pipe. The static pressures of the main nozzle over a wide range of the nozzle tank pressure were measured, and the nozzle velocity and Mach numbers were analytically calculated. Experiment81 results indicate that the critical condition of Mach number of unity to occur at the two positions in a main nozzle; one of them is the needle tip and the other is the acceleration tube exit An increase in the tank pressure causes the critical throat condition to occur at the two positions above. The velocity of acceleration-tube exit is maximum at the critical length L* and flow patter in acceleration-tube over critical lengh remains unstable.