• 제목/요약/키워드: lap length

검색결과 155건 처리시간 0.025초

프레스 접합성형 GMT-Sheet의 기계적 성질 (Mechanical Properties of GMT-Sheet on Press joined Molding)

  • 김혁;최유성;이동기;한길영;김이곤
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2000년도 제15차 학술회의논문집
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    • pp.553-553
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    • 2000
  • The application as the parts of an automobile, using the property of GMT-Sheet, is increasing. In order to exchange the parts of an automobile for GMT-Sheet, at first, the establishment and joining problem of exact joining strength must be determined. We have studied it using composites which is not same each other fiber oriented condition so as to determine joining strength and joining condition of GMT-Sheet. h this study, the result of experiment of forming condition concerned joining problem of GMT-Sheet is this ; joining efficiency of of GMT-Sheet, increases as lap joint length L increases. Increase of compression ratio causes decrease of joining efficiency after of GMT-Sheet joining. In the viewpoint of recycling, randomly oriented composite of GMT-Sheet is desirable more than unidirectional oriented composite. We has better design the structure so as not to occur to stress centralizatien on the joining part.

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GMT-Sheet의 접합에 있어서 기계적 성질에 미치는 성형조건의 영향 (Effect of Molding Condition on Mechanical properties during Joining of GMT-Sheet)

  • 김혁;최유성;서진;한길영;이동기
    • 한국해양공학회지
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    • 제15권2호
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    • pp.111-119
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    • 2001
  • The application as the parts of an automobile, using the property of GMT-Sheet, is increasing. In order to exchange the parts of an automobile for GMT-Sheet, at first, the establishment and problem of exact joining strength must be determined. We have studied it using composites which is not same each other fiber oriented condition so as to determine joining strength and joining condition of GMT-Sheet. In this study, the result of experiment of forming condition concerned joining problem of GMT-Sheet is this; joining efficiency of GMT-Sheet, increases as lap joint length L increases. Increase of compression ratio causes decrease of joining efficiency after of GMT-Sheet joining. In the viewpoint of recycling, randomly oriented composite of GMT-Sheet is desirable more than unidirectional oriented composite. We has better design the structure so as not to occur to stress centralization on the joining part.

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GTA-GMA 하이브리드공정에 따른 자동차용 아연도금강판의 용접부 기공감소 (II) - 하이브리드공정 적용 결과 (Porosity Reduction during Gas Tungsten Arc-Gas Metal Arc Hybrid Welding of Zinc Coated Steel Sheets (II) - Hybrid Welding Results)

  • 안영남;김철희
    • Journal of Welding and Joining
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    • 제34권4호
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    • pp.48-54
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    • 2016
  • The use of Zn coated steel has increased in the automotive industry due to its excellent corrosion resistance. Conventionally the BIW(body-in-white) structure and the hang-on parts have been made of Zn coated steel and more recently Zn coated steel began to be applied in the chassis parts. During gas metal arc (GMA) welding of the chassis part, lap fillet joint used to be adopted but spatter generation and porosities are most important concerns. In the industrial applications, an intentional joint gap was made to avoid the weld defects but it is not easy to control the size of joint gap. In this research, gas tungsten arc (GTA) is combined with GMA welding where GTA precedes GMA. As pulsed arc was adopted as GMA, GTA was oscillated along the longitudinal direction by pulsing GMA, but the arc oscillation did not disturb the molten droplet transfer of GMA welding. By increasing the distance between GTA and GMA, the length of weld pool increased and porosity could be reduced. Moreover porosity in the welds was fully removed when the distance between two arcs was 15 mm.

RC 부재 휨 실험에 의한 GFRP 보강근의 이음길이 제안 (Splice Length of GFRP Rebars Based on Flexural Tests of Unconfined RC Members)

  • 최동욱;천성철;하상수
    • 콘크리트학회논문집
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    • 제21권1호
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    • pp.65-74
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    • 2009
  • 이형철근의 부식이 우려되는 경우, GFRP 보강근의 사용이 사용될 수 있다. 이 연구에서는 GFRP 보강근으로 보강된 총 36개 보 및 일방향 슬래브의 휨 실험을 수행하였다. 4종의 GFRP 보강근을 실험에 사용하였고, 보강근 직경은 13 mm이었다. 대부분의 실험체의 보강근은 중앙부에서 겹침이음되었다. 모든 보 및 슬래브는 4점재하 되었으므로, 이음부는 균일한 모멘트를 받도록 계획하였다. 실험변수는 이음길이, 피복두께 및 보강근 간격이었다. 보수적으로 부착강도를 평가하기 위하여 이음부에는 스터럽을 사용하지 않았다. 실험결과 보강근과 콘크리트 간 발생한 부착응력을 비선형 단면해석을 통하여 결정하였다. 2변수 선형 회귀분석을 사용하여 평균부착강도의 예측식을 유도하였다. 5% 분위수 개념을 사용하여 이음길이 설계식을 제안하였다. 이 연구의 결과로 이론적인 이음길이 설계식이 제안되었으며 결과를 ACI 440 정착설계식과 비교하였다.

고경질 도막을 이용한 PET 필름 접합공법의 필름 표면처리 방법에 따른 접합특성 연구 (A Study on the Joint Property by the Surface Treatment Method on the Jointing Method of PET Film using the High Hardness Liquid)

  • 이종석;김영삼;신홍철;김영근;강충모
    • 한국구조물진단유지관리공학회 논문집
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    • 제18권3호
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    • pp.153-159
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    • 2014
  • 본 연구에서는 고경질 도막재로 PET 필름을 접합하는 시공방법에 있어서 PET 필름의 표면처리 조건 및 겹침이음 길이에 따른 접합특성 및 내구특성을 검토하였는데, 그 결과 무처리 보다 코로나 방전 처리에 의해 접촉각, 접합 인장강도, 벗김저항성이 개선되었다. 특히 시험체 E (코로나 방전+프라이머+강접접착제+폴리에스터 부직포)에서 가장 높은 것으로 나타났으며, 특히 겹침 이음길이 15mm 이상일 때 16주간 장기간 열화처리에도 안정적인 접합성능을 확보하는 것으로 나타나 방수재료로서 수밀성을 확보할 것으로 판단된다.

루프이음을 가진 모듈식 슬래브 연결부의 휨성능에 관한 실험적 연구 (An Experimental Study on the Flexural Performance of Modular Slab Connections with Loop Joints)

  • 김동완;신정열
    • 한국산학기술학회논문지
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    • 제17권1호
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    • pp.459-467
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    • 2016
  • 최근, 도로를 따라 지하 5~7m의 저심도에 설치되는 저심도 도시철도시스템의 경제성을 확보하기 위해, 신개념의 모듈식 개착 시공법을 개발 중에 있다. 본 연구에서는 상부 슬래브간의 연결부에 대한 구조성능 검증을 위해 루프이음을 가진 프리캐스트 철근콘크리트 부재들의 4점 재하 실험을 수행하였다. 전체 11개의 실험체가 제작되었으며 단면형상, 이음부 형상, 이음길이, 횡방향 보강철근을 변수로 이음이 없는 전단면 및 반단면 실험체와 비교하였다. 실험결과, 루프이음 실험체는 항복하중과 최대하중시 변위량 차이가 컸으며 이는 항복이후 접합부에서 발생한 균열이 확장됨에 따라 강성저하로 변위량이 급격히 증가한 것으로 판단된다. 또한 200mm의 루프이음을 가진 반단면 실험체의 경우, 이음이 없는 기준 실험체에 상당하는 휨성능을 확보하며 200mm 초과시 휨성능 향상의 정체기를 보였다.

BIM Model 기반 철근 수량산출 시 고려사항 (Considerations When Quantity Take-Off of Rebar Based on the BIM Model)

  • 정서희;김주용;김광희
    • 한국건축시공학회:학술대회논문집
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    • 한국건축시공학회 2023년도 봄 학술논문 발표대회
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    • pp.73-74
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    • 2023
  • The purpose of this study is to derive the cause of the quantity difference and present the considerations when take-off rebar quantity based on BIM model by comparing the quantity of rebar based on BIM model with 2D drawing. This research was limited to take-off the quantity of rebars in the building frame work, and after take-off the quantity of rebars by 3D modeling the 2D drawing of the target building with Revit, the quantity difference was compared with 2D-based software. Therefore, when take-off the quantity of rebars based on the BIM model, instead of take-off the existing 2D-based quantity premium proportion, according to general structural consider development length, lap splice length, covering thickness, reinforcing bars and spacing. In the future, this study is expected to contribute to improving the accuracy of BIM-based frame construction quantity take-off.

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Effect of modifying the thickness of the plate at the level of the overlap length in the presence of bonding defects on the strength of an adhesive joint

  • Attout Boualem;Sidi Mohamed Medjdoub;Madani Kouider;Kaddouri Nadia;Elajrami Mohamed;Belhouari Mohamed;Amin Houari;Salah Amroune;R.D.S.G. Campilho
    • Advances in aircraft and spacecraft science
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    • 제11권1호
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    • pp.83-103
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    • 2024
  • Adhesive bonding is currently widely used in many industrial fields, particularly in the aeronautics sector. Despite its advantages over mechanical joints such as riveting and welding, adhesive bonding is mostly used for secondary structures due to its low peel strength; especially if it is simultaneously exposed to temperature and humidity; and often presence of bonding defects. In fact, during joint preparation, several types of defects can be introduced into the adhesive layer such as air bubbles, cavities, or cracks, which induce stress concentrations potentially leading to premature failure. Indeed, the presence of defects in the adhesive joint has a significant effect on adhesive stresses, which emphasizes the need for a good surface treatment. The research in this field is aimed at minimizing the stresses in the adhesive joint at its free edges by geometric modifications of the ovelapping part and/or by changing the nature of the substrates. In this study, the finite element method is used to describe the mechanical behavior of bonded joints. Thus, a three-dimensional model is made to analyze the effect of defects in the adhesive joint at areas of high stress concentrations. The analysis consists of estimating the different stresses in an adhesive joint between two 2024-T3 aluminum plates. Two types of single lap joints(SLJ) were analyzed: a standard SLJ and another modified by removing 0.2 mm of material from the thickness of one plate along the overlap length, taking into account several factors such as the applied load, shape, size and position of the defect. The obtained results clearly show that the presence of a bonding defect significantly affects stresses in the adhesive joint, which become important if the joint is subjected to a higher applied load. On the other hand, the geometric modification made to the plate considerably reduces the various stresses in the adhesive joint even in the presence of a bonding defect.

복합재료 동력전달축의 접착조인트 설계 (Design of Adhesive Joints for Composite Propeller Shafts)

  • 김진국;이대길
    • 한국복합재료학회:학술대회논문집
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    • 한국복합재료학회 2000년도 춘계학술발표대회 논문집
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    • pp.149-153
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    • 2000
  • Substituting composite structures for conventional metallic structures has many advantages because of higher specific stiffness and specific strength of composite materials. In this work, one-piece propeller shafts composed of carbonfepoxy and glass/epoxy composites were designed and manufactured for a rear wheel drive automobile satisfying three design specifications, such as static torque transmission capability, torsional buckling and the fundamental natural bending frequency. Single lap adhesively bonded joint was employed to join the composite shaft and the aluminum yoke. For the optimal adhesive joining of the composite propeller shaft to the aluminum yoke, the torque transmission capability of the adhesively bonded composite shaft was calculated with respect to bonding length and yoke thickness by finite element method and compared with the experimental result. Then an optimal design method was proposed based on the failure model which incorporated the nonlinear mechanical behavior of aluminum yoke and epoxy adhesive. From the experiments and FEM analyses, it was found that the static torque transmission capability of composite propeller shaft was maximum at the critical yoke thickness, and it saturated beyond the critical length. Also, it was found that the one-piece composite propeller shaft had 40% weight saving effect compared with a two-piece steel propeller shaft.

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9600 BPS Modem의 복조기와 Equalizer에 관한 연구 (On the Design of Demodulator and Equalizer of 9600 BPS Modem)

  • 장춘서;은종관
    • 대한전자공학회논문지
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    • 제20권4호
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    • pp.10-15
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    • 1983
  • 본 논문에서는 전송 속도가 9600 bps인 data modem의 복조기와 equalizer의 효과적인 구성에 대하여 연구하였으며, finite word length 효과가 equalizer 동작에 미치는 영향을 제시하였다. 복조기에는 tap수가 37개인 decimation filter를 사용해서 symbol당 곱셈 횟수를 크게 줄였는데 이때 equalizer 동작에 있어 충분한 결과를 얻을 수 있음을 알 수 있었다. 주파수 offset이 존재할 때 1차 반송파 위상 추적 loop와 2차 반공파 위상 추적 loop의 성능을 비교하였고, word length를 각각 8 bit, 12 bit 및 16bit로 변화시켰을 경우 equalizer 평형상태 MSE(mean square error)의 변화 및 tap 적응을 위한 최적 step see와 lap수를 제시하였다.

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