• Title/Summary/Keyword: Pressure Tank

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A Study on the Fatigue Strength of Compressed Air Tank for Ships(I) (선박용 압축공기 탱크의 피로강도에 관한 연구(I))

  • Kim Jon-Ho;An Jae-Hyeong
    • Journal of Advanced Marine Engineering and Technology
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    • v.29 no.8
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    • pp.923-928
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    • 2005
  • The estimation of fatigue life at the design stage of the compressed air tank on board is very important in order to arrive at feasible and reliable solutions considering the total lifetime of the tank. In this paper the compressed air tank on board was selected as a model and the change of inside pressure of the tank during normal navigation period was measured and the cycle of fluctuation stress was presumed statistically based on this. Also the effect of stress concentration with the FEM analysis on the longitudinal weld and the mean stress effect on the fatigue strength of compressed air tank were discussed.

Numerical Simulation of Fast Filling of a Hydrogen Tank

  • Suryan, Abhilash;Kim, Heuy-Dong
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2010.11a
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    • pp.353-358
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    • 2010
  • High pressure gas is a widely used storage mode for hydrogen fuel. A typical hydrogen tank that is charged with hydrogen gas can function as a hydrogen supply source in a large number of applications. The filling process of a high-pressure hydrogen tank should be reasonably short. However, when the fill time is short, the maximum temperature in the tank increases. Therefore the process should be designed in such a way to avoid high temperatures in the tank because of safety reasons. The paper simulates the fast filling process of hydrogen tanks using Computational Fluid Dynamics method. The local temperature distribution in the tank is obtained. Results obtained are compared with available experimental data. Further work is going on to improve the accuracy of the calculations.

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Effect of Curing Temperature and Autofrettage Pressure on a Type 3 Cryogenic Propellant Tank (경화온도와 자긴 압력이 Type 3 극저온 추진제 탱크에 미치는 영향 연구)

  • Kang, Sang-Guk;Kim, Myung-Gon;Kong, Cheol-Won;Kim, Chun-Gon
    • Composites Research
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    • v.19 no.4
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    • pp.31-38
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    • 2006
  • In this study, effects of curing temperature and autofrettage pressure on a Type 3 cryogenic propellant tank, which is composed of composite hoop/helical layers and a metal liner, were investigated by thermo elastic analysis and composite/aluminum ring specimen tests. Temperature field of a Type 3 tank was obtained from solving the heat transfer problem and, in turn, was used as nodal temperature boundary conditions during the elastic analyses for curing temperature and autofrettage pressure effects. As a result, it was shown that the higher curing temperature was, the more residual compressive stress and tensile stress were induced in composites and metal liner, respectively. On the contrary, autofrettage pressure brought the reduction of these residual thermal stresses caused by cryogenic environments to the tank structure. This tradeoff for curing temperature and autofrettage pressure must be considered in the design and manufacturing stages for a Type 3 cryogenic tank.

A Study on the Thermal Characteristics of High Pressure Hydrogen Storage Tank according to Nozzle Angle and Length/Diameter Ratio (고압수소 저장용기의 노즐 각도 및 길이/직경비에 따른 열적 특성 연구)

  • JEONG HWAN YOON;JUNYEONG KWON;KYUNG SOOK JEON;JIN SIK OH;SEUNG JUN OH
    • Transactions of the Korean hydrogen and new energy society
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    • v.34 no.5
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    • pp.431-438
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    • 2023
  • Recently, study on hydrogen is being conducted due to environmental pollution and fossil fuel depletion. High-pressure gas hydrogen commonly used is applied to vehicle and tube trailers. In particular, high-pressure hydrogen storage tank for vehicles must comply with the guidelines stipulated in SAE J2601. There is a charging temperature limitation condition for the safety of the storage tank material. In this study, numerical analysis method were verified based on previous studies and the nozzle angle was changed for thermal management to analyze the increase in forced convection effect and energy uniformity due to the promotion of circulation flow. The previously applied high-pressure hydrogen storage tank has a length/diameter ratio of about 2.4 and was analyzed by comparing the length/diameter ratio with 8. As a result, the circulation flow of hydrogen flowing into the high-pressure hydrogen storage tank is promoted at a nozzle angle of 30° than the straight nozzle and accordingly, the effect of suppressing temperature rise by energy uniformity and forced convection was confirmed.

Numerical Study on the Design Safety of $9\%$ Nickel Based Inner Tank Bottom Plate in Terms of Hydrostatic Pressure (유체정압을 고려한 $9\%$ 니켈강재 내부탱크 바닥판의 설계 안정성에 관한 수치적 연구)

  • Kim Chung Kyun;Kim Han Goo
    • Journal of the Korean Institute of Gas
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    • v.8 no.2 s.23
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    • pp.35-41
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    • 2004
  • This paper presents the stress and deformation characteristics of $9\%$ nickel based inner tank bottom plate in full containment LNG storage tank. When a . maximum hydrostatic pressure applies the bottom plate of inner tank, the maximum = f stress and displacement distributions of the bottom plate have been analyzed as ' functions of inclined angle of the bottom plate, and the thickness and length of the annular plate between the shell plate and bottom one. The calculated results indicate that the taper of the bottom plate is recommended by 100${\~}$200 : 1 for $140,000m^3$ storage capacity of the inner tank. The results recommend that the thickness of the annular plate is around 20mm and the length is greater than 3m for a maximum hydrostatic pressure of $140,000m^3$ tank capacity.

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A Study on the Integrated Control and Safety Management System for 9% Ni Steel LNG Storage Tank (9% 니켈강재식 LNG 저장탱크용 통합제어안전관리시스템에 관한 연구)

  • Kim, Chung-Kyun
    • Journal of the Korean Institute of Gas
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    • v.14 no.5
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    • pp.13-18
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    • 2010
  • This paper presents the development of an integrated control and safety management system for 9% nickel steel LNG storage tank. The new system added the measuring equipment of pressure, displacement and force compared to the conventional measurement and control system. The measured data has simultaneously been processed by integrating and analyzing with new control equipments and safety management systems. The integrated control and safety management system, which may increase a safety and efficiency of a super-large full containment LNG storage tank, added additional pressure gauges and new displacement/force sensors at the outer side wall and a welding zone of a stiffener and top girder of an inner tank, and the inner side wall of a corner protection tank. The displacement and force sensors may provide failure clues of 9% nickel steel structures such as an inner tank and a corner protection, and a LNG leakage from the inner tank. The conventional leak sensor may not provide proper information on 9% nickel steel tank fracture even though LNG is leaked until the leak detector, which is placed at the insulation area between an inner tank and a corner protection tank, sends a warning signal. Thus, the new integrated control and safety management system is to collect and analyze the temperature, pressure, displacement, force, and LNG density, which are related to the tank system safety and leakage control from the inner tank. The digital data are also measured from control systems such as displacement and force of 9% nickel steel tank safety, LNG level and density, cool-down process, leakage, and pressure controls.

Pressure-volume-temperature gauging method experiment using liquid nitrogen under microgravity condition of parabolic flight

  • Seo, Mansu;Park, Hana;Yoo, DonGyu;Jung, Youngsuk;Jeong, Sangkwon
    • Progress in Superconductivity and Cryogenics
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    • v.16 no.2
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    • pp.64-69
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    • 2014
  • Measuring an exact amount of remaining cryogenic liquid propellant under microgravity condition is one of the important issues of rocket vehicle. A Pressure-Volume-Temperature (PVT) gauging method is attractive due to its minimal additional hardware and simple gauging process. In this paper, PVT gauging method using liquid nitrogen is investigated under microgravity condition with parabolic flight. A 9.2 litre metal cryogenic liquid storage tank containing approximately 30% of liquid nitrogen is pressurized by ambient temperature helium gas. During microgravity condition, the inside of the liquid tank becomes near-isothermal condition within 1 K difference indicated by 6 silicon diode sensors vertically distributed in the middle of the liquid tank. Helium injection with higher mass flow rate after 10 seconds of the waiting time results in successful measurements of helium partial pressure in the tank. Average liquid volume measurement error is within 11% of the whole liquid tank volume and standard deviation of errors is 11.9. As a result, the applicability of PVT gauging method to liquid propellant stored in space is proven with good measurement accuracy.

Design Modification of a Thermal Storage Tank of Natural-Circulation Solar Water Heater for a Pressurized System (자연순환형 태양열 온수기 축열조의 압력식 설계 개조)

  • Boo, Joon-Hong;Jung, Eui-Guk
    • Journal of the Korean Solar Energy Society
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    • v.27 no.3
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    • pp.45-54
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    • 2007
  • For a conventional natural-circulation type solar water heater, the pressure head is limited by the height between the storage tank and hot water tap. Therefore, it is difficult to provide sufficient hot water flow rate for general usage. This study deals with a design modification of the storage tank to utilize the tap-water pressure to increase hot-water supply Based on fluid dynamic and heat transfer theories, a series of modeling and simulation is conducted to achieve practical design requirements. An experimental setup is built and tested and the results are compared with theoretical simulation model. The storage tank capacity is 240 l and the outer diameter of piping was 15 mm. Number of tube turns tested are 5, 10, and 15. Starting with initial storage tank temperature of $80^{\circ}C$, the temperature variation of the supply hot water is investigated against time, while maintaining minimum flow rate of 10 1/min. Typical results show that the hot water supply of minimum $30^{\circ}C$ can be maintained for 34 min with tap-water supply pressure of 2.5 atm, The relative errors between modeling and experiments coincide well within 10% in most cases.

A Numerical Study on the Sloshing Characteristics in a Two-dimensional Rectangular Tank Using the Level Set Method (레벨셋법을 이용한 2 차원 사각 탱크 내부의 슬로싱 특성에 관한 수치적 연구)

  • Yoon, Hyun-Sik;Lee, Jung-Min;Chun, Hwan-Ho;Lee, Hyun-Goo
    • Journal of the Society of Naval Architects of Korea
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    • v.45 no.2
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    • pp.132-143
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    • 2008
  • The sloshing phenomena in a two-dimensional rectangular tank are investigated using a level set method based on finite volume method. The code validations are performed by comparing between the present results and previous numerical results, which gives a good agreement. We present the streamlines pattern, free surface shape, maximum free surface elevation and pressure fluctuation patterns in the tank under the pitch and surge motions with various frequencies. These two different motions cause the different flow structures in the tank. The time variations of surface elevation and pressure at the different locations in the tank strongly depend on the exciting frequency of tank moving.

Large Steel Tank Fails and Rockets to Height of 30 meters - Rupture Disc Installed Incorrectly

  • Hedlund, Frank H.;Selig, Robert S.;Kragh, Eva K.
    • Safety and Health at Work
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    • v.7 no.2
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    • pp.130-137
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    • 2016
  • At a brewery, the base plate-to-shell weld seam of a $90-m^3$ vertical cylindrical steel tank failed catastrophically. The 4 ton tank "took off" like a rocket leaving its contents behind, and landed on a van, crushing it. The top of the tank reached a height of 30 m. The internal overpressure responsible for the failure was an estimated 60 kPa. A rupture disc rated at < 50 kPa provided overpressure protection and thus prevented the tank from being covered by the European Pressure Equipment Directive. This safeguard failed and it was later discovered that the rupture disc had been installed upside down. The organizational root cause of this incident may be a fundamental lack of appreciation of the hazards of large volumes of low-pressure compressed air or gas. A contributing factor may be that the standard piping and instrumentation diagram (P&ID) symbol for a rupture disc may confuse and lead to incorrect installation. Compressed air systems are ubiquitous. The medium is not toxic or flammable. Such systems however, when operated at "slight overpressure" can store a great deal of energy and thus constitute a hazard that ought to be addressed by safety managers.