• Title/Summary/Keyword: 공압용기

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Future Vision through NL Tensioner Technology Development and Domestic Equipment Fabrication (NL Tensioner 기술개발 및 기자재 국산화를 통한 향후 비젼)

  • Lee, Ki-Yeol;Choi, Hae-Soo;Lee, Eun-Jin;Yoon, Tae-Sam
    • Journal of Ocean Engineering and Technology
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    • v.25 no.2
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    • pp.127-133
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    • 2011
  • The following Technology Report was written with respect to recent offshore technology development. This report was prepared with the purpose of suggesting recent offshore technology and upcoming visions by describing the principles of an offshore drilling operation, the NL Tensioner Cylinder Package R & D, and the general technology related to three offshore patent areas, as major contents.

A Study on Characteristics of a Pneumatic Device for Deploying Fins (공압식 날개전개장치 특성 연구)

  • Kang, Choon-Kil;Won, Myong-Shik
    • Journal of the Korea Institute of Military Science and Technology
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    • v.13 no.3
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    • pp.365-371
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    • 2010
  • The fins of a missile which is folded within a canister are deployed according to a command during the missile flight. The aerodynamic load generated by operating environments such as missile flight speed, platform movement speed and wind acts as an anti-deploying force and prevents the fins from deploying. As the diversification of platforms and the higher speed of missiles need a larger deploying force but the space for operating the fin deploying device is getting narrower, the new design concepts are required for developing such a device. In this study, a pneumatic device for deploying missile fins is designed and its characteristics are verified through experiments and analyses.

The Review of Saturn V 1st Stage (S-IC) Propulsion System (Saturn V 발사체 1단(S-IC) 추진기관 시스템 연구)

  • Hong, Yonggi;Kim, Cheulwoong
    • Journal of the Korean Society of Propulsion Engineers
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    • v.19 no.2
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    • pp.73-80
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    • 2015
  • It had been almost a half century since Apollo Mission was ended. However, in these days, a lot of researches are being conducted for restoration and making improvements in technologies used in Saturn V rocket's development. This study reviews the first stage of Saturn V rocket(S-IC), from development history to technologies in various subsystems such as engine purge system, POGO suppression system, hydraulic and pneumatic control system, propellant dispersion system, telemetry system and retrorocket system. Understandings of S-IC stage's operation systems would be helpful in understanding of launch vehicle system and reduction of time and cost in future development process.

Evaluation of Detectable Defect Size for Inner Defect of Pressure Vessel Using Laser Speckle Shearing Interferometry (레이저 스페클 전단간섭법을 이용한 압력용기 내부결함의 측정 가능한 결함 크기의 평가)

  • Kim, Kyeong-Suk;Seon, Sang-Woo;Choi, Tae-Ho;Kang, Chan-Geun;Na, Man-Gyun;Jung, Hyun-Chul
    • Journal of the Korean Society for Nondestructive Testing
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    • v.34 no.2
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    • pp.135-140
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    • 2014
  • Pressure vessels are used in various industrial fields. If a defect occurs on the inner or outer surface of a pressure vessel, it may cause a massive accident. A defect on the outer surface can be detected by visual inspection. However, a defect on the inner surface is generally impossible to detect with visual inspection. Nondestructive testing can be used to detect this type of defect. Laser speckle shearing interferometry is one nondestructive testing method that can optically detect a defect; its advantages include noncontact, full field, and real time inspection. This study evaluated the detectable size for an internal defect of a pressure vessel. The material of the pressure vessel was ASTM A53 Gr.B. The internal defect was detected when the pressure vessel was loaded by internal pressure controlled by a pneumatic system. The internal pressure was controlled from 0.2 MPa to 0.6 MPa in increments of 0.2 MPa. The results confirmed that an internal defect with a 25 % defect depth could be detected even at 0.2 MPa pressure variation.

A Study on the Measurement Method of Leakage Flow-rate for Pneumatic Cylinder (공압실린더의 누설유량 계측방법에 관한 연구)

  • Jang J.S.;Ji S.W.;Jeong J.H.;Kang B.S.
    • Transactions of The Korea Fluid Power Systems Society
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    • v.3 no.1
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    • pp.15-19
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    • 2006
  • In this study, a measurement method of leakage flow-rate for pneumatic driving apparatus is proposed. The existing measurement methods of leakage flow-rate of air need disassemble the test component. Therefore, there is no effective method to measure the leakage flow-rate while operating pneumatic driving apparatus. In this study, the leakage flow-rate is measure from the pressure change in an isothermal chamber that can realize isothermal conditions by stuffing steel wool into it. Therefore, wide range of flow-rate could be measured only from the pressure response and the leakage flow-rate can be measured during operating pneumatic driving apparatus. The effectiveness of the proposed method is proved by experimental results.

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A Study on Modeling of the Pneumatic Part in a Gas Blow-Down System Including Pressure Regulator and Pipe-Line Characteristics (압력조절밸브와 배관 특성을 포함한 유도무기용 기체 블로우다운 시스템의 공압부 모델링에 관한 연구)

  • Park, Youngwoo
    • Journal of Drive and Control
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    • v.14 no.3
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    • pp.32-39
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    • 2017
  • In this study, a mathematical model of the pneumatic part in a gas blow-down system is proposed. The mathematical model consists of four major parts: pressure vessel, reservoir, pressure regulator and pipe-line. To ensure accuracy in long-time simulations, heat transfer between gas and pressure vessel is considered. The model is validated by comparing simulation results with experimental data. Experiments are conducted on the ground, where free convection can be assumed. Simulation results indicate the proposed model can accurately describe behavior of a gas blow-down system. Therefore, it may be used for design and analysis of similar systems with a slight modification.

Design and Engineering of the Coal Feeding System for IGCC Powerplant (IGCC 발전시스템 석탄주입계통의 설계 및 엔지니어링)

  • Lee, Chan;Kang, Seung-Jong;Lee, Han-Goo
    • Proceedings of the Korea Society for Energy Engineering kosee Conference
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    • 1994.11a
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    • pp.59-67
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    • 1994
  • 석탄가스화 복합발전설비에 사용되는 석탄주입계통 설계/엔지니어링을 위한 체계적 방법을 제시하였다. 석탄주입계통의 주요 구성요소로는 호퍼, 필터, 스크류공급기, 공압수송기 및 사출용기등을 고려하였고, 그에 대한 설계 사양 및 제한조건들을 제시하였다. 더 나아가 석탄주입계통의 공정제어를 위해 필요한 계측장비, 제어논리 및 제어시스템에 대한 설계기준을 서술하였다. 본 연구에서 제시된 방법들은 석탄주입계통의 기본설계 또는 선정을 위한 엔지니어링에 유용하게 사용될수 있을 것으로 판단된다.

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Design of Portable Welded-Nitrogen Vessel (11 kg, 10 L and 50 bar) for Shipbuilding (선박용 휴대형 질소용기(11 kg, 10 L 및 50 bar)의 두께 및 외형 설계)

  • Seong, Hansaem;Kim, Jaeyeol;Eom, Taejin;Kawk, Hyo Seo;Lee, Kwang O;Kim, Chul
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.41 no.4
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    • pp.263-270
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    • 2017
  • The shipbuilding industry uses large stationary tanks to store low-pressure air, which is used to open and close large shut-off valves. However, when supplying air from the tank to a distant valve, there are problems related to the need for supplementary pipes and the pressure drop during transportation. In this study, a portable welded vessel for storing high-pressure nitrogen (11 kg, 10 L, and 50 bar) was designed to prevent air leakage and improve the convenience of workers. This pressure vessel was elliptical to reduce the number of welded parts, which are structurally weak. The thickness and ratio of the major and minor axes of the pressure vessel were calculated to verify its structure stability at the working pressure (50 bar), and that the proposed weight and capacity were satisfactory. The residual stress caused by the welding process was calculated by performing a transient thermal-structural coupled field analysis using the ANSYS parametric design language (APDL), and the fatigue life of the vessel was verified based on the Goodman criterion.