• 제목/요약/키워드: 체결 해석

검색결과 329건 처리시간 0.023초

스냅링 체결 공정 해석 (Finite Element Analysis for Fastening Process of Snap Ring)

  • 류일훈;임영훈
    • 한국자동차공학회논문집
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    • 제17권2호
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    • pp.187-192
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    • 2009
  • A snap ring is a kind of metal spring with open ends which can be installed into a groove to prevent lateral movement. In this study a nonlinear finite element analysis model is developed to simulate the fastening process of a snap ring connecting the constant velocity joint and the transmission. Insert load, disengage load and breakage are three important issues. They are analyzed using the developed model. The load histories of simulations are similar to those of tests and the differences of maximum load are around 10%. Bending of the entire ring and unfolding of the end section are major contributors of the fastening load. The load variations caused by the angular position of spline tooth are about 50%. Breakage is highly sensitive to the position of a snap ring.

Anchor bracket 체결 볼트에 대한 절단 강도 해석 (Breaking Strength Analysis for Bolt Connection of Anchor Bracket)

  • 이봉주;양헌석;오형식
    • 한국철도학회:학술대회논문집
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    • 한국철도학회 2011년도 춘계학술대회 논문집
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    • pp.55-60
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    • 2011
  • For the bolster type bogie, bolster anchor body connections are proviede to transmit the longitudinal loads for traction or braking between the carbody and the truck. The bolster anchor body connection is generally composed of anchor rod bracket, anchor rod and its fastening devices. The bolster anchor body connection shall be basically capable of withstanding a longitudinal load resulting from excessive braking case or impact. Additionally the north America standard requires that the anchor rod bracket shall be frangible, I.e. the anchor rod bracket shall fail and fall away under load before the carbody structure is damaged since to protect the cabody structure in the event of unexpected accident. This paper describes the shear connection design using the optimized mechanical fasteners in the bolster anchor body connection to satisfy these Northe America requirements.

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점진적 파손해석 기법을 이용한 일방향-평직 혼합 적층 복합재 체결부의 강도 (Strength of UD-Fabric Hybrid Laminated Composite Joints Based on Progressive Failure Analysis)

  • 신소영;안현수;권진회
    • 한국복합재료학회:학술대회논문집
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    • 한국복합재료학회 2002년도 춘계학술발표대회 논문집
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    • pp.17-21
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    • 2002
  • A finite element method based on the two-dimensional progressive failure analysis is presented for characterizing the strength and failure of the unidirectional-fabric hybrid laminated composite joints under pin loading. The 8-node laminated shell element is incorporated in the updated Lagrangian formulation. Various failure criteria including the maximum stress, Tsai-Wu, Yamada-Sun, and combinations of them are used in conjunction with the complete unloading stiffness degradation method. For the verification, joint tests are conducted for the specimens with various geometries. Although there are some differences depending on the geometry, the finite element model using the Yamada-Sun or the combined Yamada-Sun and Tsai-Wu criterion predicts the failure strength best.

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체결방법에 따른 볼트결합 구조물의 동적해석 (A dynamic analysis of bolted joints under various conditions)

  • 정영도;박세만;박명균
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2002년도 춘계학술대회 논문집
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    • pp.774-777
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    • 2002
  • There are various methods to join mechanical structures together. They typically include welding, mechanical joints by bolts and other processes depending on specific needs. Analyses of joints in the mechanical structures are essential in understanding the dynamic characteristics of the structures. In this research an impulse technique is applies to investigate the dynamic behavior of joints produced by bolts. The length overlap in the joints was varied as the number of the bolts in the joins was changed. Also, the torque applied to the bolts were adjusted. Resonance frequencies were determined for the joints to evaluate the relationship between the increase in the applied torque and the increase in the number of bolts used in the joints. The results have demonstrated that the resonance frequencies of the joints increase with the increasing torque.

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다이케스팅 머신의 구조 해석

  • 윤승원
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 1995년도 추계학술대회 논문집
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    • pp.813-817
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    • 1995
  • Structural analysis of horizontal cold chamber die casting machine is performed by the FEM. The analyzed model is made up of stationary die platen,movable die platen,link housing platen, C-frame, and tie bar which mainly undertake die locking force and injection force. In modeling, compression gap elements are used for to simulate contacting condition between tie bar and movable die platen, movable die platen and base frame, and link housing and base frame. Unbalanced die locking force imposed on four tie bars are considered. As the results, the deformed shape and the stresses of the die casting machine are given.

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액체로켓엔진 극저온 산화제 배관 제작공정 개발 (Development of Cryogenic Oxygen Line Manufacturing Process for Liquid Rocket Engine)

  • 김진형;조황래;방정석;이병호;유재한;문일윤;이수용
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2011년도 제37회 추계학술대회논문집
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    • pp.62-65
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    • 2011
  • 액체로켓엔진용 극저온 산화제 고압 배관 기술 개발을 위해 시제품을 제작하였다. 기술 개발 시제품은 체결용 플랜지, 직관, 곡관, 벨로우즈, 분기구로 구성하였다. 액체로켓엔진용 극저온 산화제 고압 배관은 터보펌프에서 토출된 고압의 극저온 산화제를 연소기로 공급하는 경로이므로 극저온, 고압의 작동환경에서 구조적 안정성을 가져야 한다. 따라서 본 제작공정 개발에서는 극저온을 고려한 구조해석을 수행하여 적합한 소재를 선정하였으며, 공정개발과 특수공정을 적용하여 시제품을 제작한 후 구조강도 시험을 수행하였다. 본 개발을 통해 액체로켓엔진에 적용되는 극저온 산화재 고압배관을 위한 기술적 기반과 소재 응용기술, 향후 고성능 대형 액체로켓엔진에 적용하기 위한 공정개발을 완료하였다.

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오목형 피스톤 조립체의 볼과 소켓의 체결을 위한 점진적 성형공정의 유한요소해석 (Finite Element Analysis of an Incremental Forming Process for Joining the Ball with the Socket of a Concave Piston Assembly)

  • 이민철;엄재근;전만수
    • 한국소성가공학회:학술대회논문집
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    • 한국소성가공학회 2006년도 춘계학술대회 논문집
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    • pp.353-358
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    • 2006
  • A three-dimensional finite element approach to process analysis and design for joining the socket with the ball by a kind of the rotary forging processes is presented in this paper. The rigid-plastic finite element method is employed and its results are used to reduce the number of process design tryouts. The approach is applied to developing a concave piston assembly for a high pressure hydraulic pump. Experiments show that the developed piston assembly satisfies the quality requirement on geometrical tolerance.

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재료비선형을 고려한 일방향-평직 혼합 적층 복합재 체결부의 점진적 파손해석 (Progressive Failure Analysis of UD-Fabric Hybrid Laminated Composite Joints Considering Material Nonlinearity)

  • 최정석;신소영;안현수;권진회
    • 한국복합재료학회:학술대회논문집
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    • 한국복합재료학회 2002년도 추계학술발표대회 논문집
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    • pp.79-82
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    • 2002
  • A finite element method based on the two-dimensional progressive failure analysis considering material nonlinearity is presented for characterizing the strength and failure of the unidirectional-fabric hybrid laminated composite joints under pin loading. The 8-node laminated shell element is incorporated in the updated Lagrangian formulation. Failure criteria including the Maximum Stress and Tsai-Wu are used in conjunction with the complete unloading stiffness degradation method. For the verification, joint tests are conducted for the specimens with two different ply-number ratios of UD composite to fabric composite. Although there are some differences depending on ply-number ratios, the finite element model using the maximum stress criterion considering nonlinear material behavior predicts the failure strength best.

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비대칭 경계조건을 가지는 체결부의 3차원 접촉응력해석 (Three-dimensional contact analysis of a composite joint with unsymmetric boundary condition)

  • 장기정;박노회;안현수;권진회;최진호
    • 한국복합재료학회:학술대회논문집
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    • 한국복합재료학회 2002년도 추계학술발표대회 논문집
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    • pp.110-113
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    • 2002
  • As a preliminary study for the three dimensional failure analysis of composite joints, the three dimensional stress analysis on a pin-loaded unidirectional-fabric hybrid composite joints are performed. The contact and frictions between composite plate and metal bush are considered in the finite element method by NASTRAN. Experiments are conducted to validate the accuracy and feasibility of the finite element technique for 25 specimens with 5 different geometries. The finite element and experimental results show the bush cap induces the unsymmetric deformation, stress distribution, and failure behavior through the thickness. The experiment also shows the failure loads are higher in the joint with bush cap than without it.

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체결단계를 고려한 승용차용 에어스프링 정특성 설계해석기법 개발 (Static FE Analysis of Air Springs for Passenger Cars Considering the Mounting Steps)

  • 이형욱;H.ThomasHahn;박진용
    • 소성∙가공
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    • 제24권6호
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    • pp.387-394
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    • 2015
  • Air springs are designed to support loads using the volume elasticity in a cylindrical shaped air bag made of a composite material with a rubber matrix and two plies of reinforced fibers. Recently, applications of these springs have been expanded from railway vehicles to passenger cars. The current study presents a finite element analysis of a manufactured air spring for a passenger car. The analysis was conducted including the mounting steps of the air bag using a static loading condition. A method for controlling the internal pressure and displacements during the mounting step was developed. The characteristic load curve and the shape of the air bag were in good agreement with the experimental data with respect to the design height, the bump height and the rebound height. Results indicate that ply angles of fibers vary from 38 degrees to 56 degrees during static loading.