• Title/Summary/Keyword: 체결 조건

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A Preliminary Drop Test of a Type IP-2 Transport Package with a Bolted Lid Type (볼트체결방식의 IP-2형 운반용기의 낙하예비시험)

  • Kim Dong-Hak;Seo Ki-seog;Park Hong Yun;Lee Kyung Ho;Yoon Jeong-Hyoun;Lee Heung-Young
    • Proceedings of the Korean Radioactive Waste Society Conference
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    • 2005.11a
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    • pp.339-347
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    • 2005
  • A type IP-2 transport package should prevent a loss or dispersal of the radioactive contents and a more than $20\%$ increase in the maximum radiation level at any external surface of the package when it were subjected to the drop test under the normal conditions of transport. If a shielding thickness of IP-2 transport package is thick, a bolted lid type may prevent a loss or dispersal of the radioactive contents than the door type of ISO containers which are generally used as a type IP-2 transport package. In this paper, to evaluate the effect of drop directions on the bolt tension and the coherence of a bolt, the drop tests of preliminary small model are tested and evaluated for seven directions before the drop test of a type IP-2 transport package with a bolted lid type under the normal conditions of transport. Seven drop directions which are a bottom-vertical drop, a lid-vortical drop. a horizontal drop and four corner drops have been carried out. Using a force sensor, the bolt tension during the drop impact is measured. The coherence of bolt is evaluated by the difference between the fastening torque of bolt before a drop test and the unfastening torque of bolt after a drop impact.

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Fatigue Analysis for Levitation Rail of Urban Maglev System (도시형 자기부상열차 부상레일의 피로해석)

  • Kim, Kyung-Taek;Kim, Jae-Yong;Kim, Yong-Hwan;Park, Jin-Soo;Pyen, Sang-Yun
    • Proceedings of the KSR Conference
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    • 2008.06a
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    • pp.39-45
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    • 2008
  • A levitation rail is placed on the top of track structure to operate Maglev vehicles and a part of track that link up with a sleeper is applied repeated load in Maglev vehicles operation. This paper aimed to verify validity of design for levitation rail, through the fatigue analysis about load which is applied to levitation rail in Maglev vehicles operation and impact load occurring in an emergency landing. Load conditions applied design load(23kN/m) in normal operation and skid drop load(24kN/m) in vehicle drop. And boundary conditions are consider bolt fixing and welding. Through static analysis, weak point and maximum stress of levitation rail could be obtained. S-N(stress-life) method was used in oder to predict fatigue life, and Goodman relationship was applied to consider a effect of mean stress. Also damage was calculated by using Miner's. As a result of fatigue analysis, levitation rail had a fatigue life which was more than requirement ($10^6$cycle) in all analysis conditions. Assumption that $10^8{\sim}10^9$cycles is infinite life, all analysis conditions had infinite life except a case under drop load and bolt fixing($1.21{\times}10^6$).

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Ontology Model based on Harmonized Commodity Description and Coding System Codes (품목분류코드 기반의 온톨로지 모델)

  • Kim, Dong Kyoo;Son, Jiseong;Baik, Doo-Kwon
    • Proceedings of the Korea Information Processing Society Conference
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    • 2010.11a
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    • pp.132-135
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    • 2010
  • FTA(Free Trade Agreement)는 체결국들의 자유로운 물자 이동을 기반으로 무역의 활성화와 외국자본의 직접투자를 통해 경제성장을 가져오는 중요한 협정이다. 그러나 FTA 협정의 체결조건에 따라 품목별 세율 등의 정보가 달라진다. 국제통일상품분류체계(Harmonized Commodity Description and Coding System)코드도 마찬가지로 국제 공동코드 영역인 6 자리까지 동일 하나, 7 ~ 10 자리까지는 각 국가에 의해 운영관리 되어, 국가별로 품목분류 방식이 달라진다. 또한, 품목분류코드가 갱신 될 때마다 연관 정보를 사용자에게 제공하고 있다. 그러나 우리나라와 FTA 체결국간 세부품목분류 방식이 달라 품목분류방식의 의미에 따라 담당자가 한 건씩 비교하고 맵핑하여, 많은 시간과 인력이 소모된다. 따라서, 의미를 갖는 품목분류코드를 맵핑하면서 발생하는 문제들이 있다. 이를 해결하기 위해, 이 논문에서는 품목분류코드 기반의 온톨로지 모델을 제안한다.

Legal Bases and Cases for the Form Requirement under PICC (국제상사계약에 관한 일반원칙(PICC)하에서 계약의 형식요건에 관한 법적 기준과 판결례)

  • Shim, Chongseok
    • International Commerce and Information Review
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    • v.18 no.4
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    • pp.143-164
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    • 2016
  • PICC are dealing with form requirements of international commercial contract under writings in confirmation, conclusion of contract dependent on agreement on specific matters or in a particular form, contract with terms deliberately left open, merger clauses, modification in a particular form. If a writing which is sent within a reasonable time after the conclusion of the contract and which purports to be a confirmation of the contract contains additional or different terms, such terms become part of the contract, unless they materially alter the contract or the recipient, without undue delay, objects to the discrepancy. Where in the course of negotiations one of the parties insists that the contract is not concluded until there is agreement on specific matters or in a particular form, no contract is concluded before agreement is reached on those matters or in that form. If the parties intend to conclude a contract, the fact that they intentionally leave a term to be agreed upon in further negotiations or to be determined by a third person does not prevent a contract from coming into existence. A contract in writing which contains a clause indicating that the writing completely embodies the terms on which the parties have agreed cannot be contradicted or supplemented by evidence of prior statements or agreements. However, such statements or agreements may be used to interpret the writing. A contract in writing which contains a clause requiring any modification or termination by agreement to be in a particular form may not be otherwise modified or terminated.

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Fatigue Characterization of Glass/Polypropylene Composite Bone Plates Locked with an Artificial Tibia under Moisture Environment (인조골에 체결된 유리섬유/폴리프로필렌 복합재료 고정판의 수분 환경 피로 특성)

  • Han, Min-Gu;Chang, Seung-Hwan
    • Composites Research
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    • v.26 no.5
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    • pp.328-333
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    • 2013
  • In this study, bone plate made of glass/polypropylene composite material which was applied to an artificial bone was tested to check the service ability under fatigue loading. To check serviceability of composite bone plates fatigue test was carried out considering changes in the moisture absorption rate, locking position of screws and loading condition. Test results showed that all the tested specimens had the fatigue life more than one million cycles which was much higher fatigue life than the expected value of 650,000 cycles. Screw position was not critical impact on the deformation of the fracture site. In this paper, the mechanical performance of the glass/polypropylene composite was verified by fatigue test under various water absorption conditions, and this result may give useful information on the design of composite bone plate.

Stability Design of a Coolant Heater based on Fastening Conditions (냉각수 가열장치의 체결 조건에 따른 안정화 설계)

  • Han, Dae-Seong;Yoon, Hyun-Jin
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.21 no.1
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    • pp.111-118
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    • 2022
  • The vehicle industry requires superior technology that can increase the efficiency of the battery of an electric vehicle. A coolant heater that can optimize the temperature of the battery is one of the most effective techniques for cold environments. However, the vibrations generated by this device can cause major complications, such as leakage and system errors. Therefore, the vibrations of the device must be suppressed to improve the stability. In this study, the fastening conditions of a coolant heater were analyzed using a computer simulation to investigate the natural frequencies and mode shapes which reflect the primary reasons for the largest vibrations under the given operating conditions. The results showed that six-bolted joints could considerably improve the stability of the fastening device

Strength of Glass/Epoxy Fabric Joints under the Pin-Loading (핀하중을 받는 유리/에폭시 평직 적층판의 체결부 강도)

  • 박노희;권진희;김종훈;변준형;양승운
    • Composites Research
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    • v.15 no.2
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    • pp.1-10
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    • 2002
  • The strength of glass/epoxy fabric joints under pin-loading is estimated based on the characteristics length method and experiment. To investigate the effect of finite element idealization for the contact between pin and laminate, three modeling cases are analyzed; assuming the cosine load distribution around the contact area, constraining the radial displacement at the hole boundary, and using the contact element. To study the effect of failure criteria, Tsai-Wu and Yamada-Sun methods are applied on the characteristic curve. The results of the nonlinear analysis using the contact element showed good agrements with experimental data in both laminates made of uni-directional prepreg tapes and fabrics. In terms of failure criteria, Tsai-Wu method showed better agreement with experimental results than the one by Yamada-Sun laminate.

Tightening Characteristics of domestic M8 stainless screws (국산 M8 스테인리스 나사의 체결특성)

  • 인상렬;박미영
    • Journal of the Korean Vacuum Society
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    • v.10 no.2
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    • pp.155-163
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    • 2001
  • A number of screws are inevitably used for tightening flanges in constructing a vacuum system. A theoretical relation between the axial force and the torque exerted on a screw is easily obtained assuming that the friction force generated on the contacting plane is known, however, in practice the friction is influenced strongly by unknown detailed surface condition. It is difficult to tighten optimally and uniformly the flange seals if the screws commercially available have undefined surface conditions and scattered dimensions, and the axial force produced by the screws can not be expected properly. In this paper a scatter of the axial force over screws and the deviation from an expected one, depending on various fastening conditions, are investigated using a variety of M8, the most popular size for vacuum flanges, domestic stainless screws of hexagonal head and standard thread.

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KSLV-1 1st stage Rear Fuselage Upper Compartment Detail Design (KSLV-1 1단 후방동체 상부 조합체 상세설계)

  • Yoo, Jae-Seok;Jeong, Ho-Kyeong;Jang, Soon-Young
    • Aerospace Engineering and Technology
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    • v.8 no.1
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    • pp.117-131
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    • 2009
  • In this study, a detail design was conducted for KSLV-1 1st stage Rear Fuselage Upper Compartment assembly. A basic structural sizing was done by the aircraft fuselage sizing in-house program. The frame structural design and the interface check were conducted by the FE and the CAD program. The structural margin of safety was conformed by FE analysis for the normal section model and duct cut-out section models which are the weakest parts of the rear fuselage. The shear stress analysis was performed for a fastener design of the skin-stringer which is most affected by the shear stress induced by the shear load.

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Stress Analysis of the Blade Joint for a Small Wind Turbine (소형풍력터빈 블레이드 체결부의 응력해석)

  • Kim, Deok-Su;Jung, Won-Young;Jung, Jin-Tai
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.36 no.1
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    • pp.117-124
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    • 2012
  • In this paper, an analysis of the joint that transmits power from the blades to the generator is performed using the FEM (finite element method). The mode shapes and natural frequencies were extracted using experimental modal analysis in order to establish the FEM model. Then, the model was verified by comparing the mode shapes and natural frequencies to those obtained from the ANSYS modal analysis. Dynamic stress analysis was performed at the rated and limited wind speeds considering the wind load and gravity.