• 제목/요약/키워드: U-bending

검색결과 229건 처리시간 0.027초

로타리 경운날의 마모에 관한 연구 (A Study on the Wear of Rotary Blades)

  • 최상인;김진현;이양근
    • Journal of Biosystems Engineering
    • /
    • 제18권1호
    • /
    • pp.15-20
    • /
    • 1993
  • Wearness has been a major failure criterion in Korean-made rotary blade. However, few studies have been conducted to improve it. In this study, the fundamental data obtained from the measurement of wearness and failure of rotary blade were analyzed to provide a guideline for the design of rotary blades. For the straight part(about 20-23 em from bolt hole) from the bolt hole to bending point of rotary blade, modifications were proposed for improvements, however, for the portion from bending point to tip was made no design recommendations because the failure behavior of that portion was difficult to analyze with the experimental data. The results are summarized as follows. 1. The current V-shape section has to be moved about 5 em toward the bending point of rotary blade. 2. The section modulus at the portion about 5-7 em distant from bolt hole has to be increased about 15-20 %. 3. The V-shape section has to be changed into U-shape to reduce the on account of recieving initial stress in blades. 4. The radius of curvature of the neck(the portion about 5-7 cm apart from bolt hole) has to be made larger to decrease the stress concentration.

  • PDF

섬유강화 복합재료의 인장 및 굽힘에 의한 파괴 (Fracture Behavior of Fiber Reinforced Composites under tensile and Bending Loadings)

  • 남기우;문창권
    • 수산해양기술연구
    • /
    • 제30권1호
    • /
    • pp.45-52
    • /
    • 1994
  • The study was conducted to evaluate reliability of the longitudinal tensile properties of unidirectional carbon fiber reinforced composites. Two kinds of carbon fiber reinforced composites laminates were tested in order to examine the factors of variability and have the information concerning reliability improvement. Temperature dependence of the strength and its variability were investigated by means of testing at two kinds of temperatures. Statistical distributions of the respective mechanical properties were obtained from the tensile tests. As a result, strength of composites was directly proportional to the ultimate strain and was not proportional to the elastic modulus. The fracture behavior in bending of notched plate was studied for a composite material. The uniform bending tests of notched plates have been carried out for a wide range of notch radii. The experiment shows that the nominal stress at failure decreased with decreasing notch radius and it approaches a constant value when the notch radius is less than about 0.3mm. The critical maximum stress is governed by notch root radius alone in the case of a constant thickness of specimen.

  • PDF

Thermo-mechanical coupling behavior analysis for a U-10Mo/Al monolithic fuel assembly

  • Mao, Xiaoxiao;Jian, Xiaobin;Wang, Haoyu;Zhang, Jingyu;Zhang, Jibin;Yan, Feng;Wei, Hongyang;Ding, Shurong;Li, Yuanming
    • Nuclear Engineering and Technology
    • /
    • 제53권9호
    • /
    • pp.2937-2952
    • /
    • 2021
  • A typical three-dimensional finite element model for a fuel assembly is established, which is composed of 16 monolithic U-10Mo fuel plates and Al alloy frame. The distribution and evolution results of temperature, displacement and stresses/strains in all the parts are numerically obtained and analyzed with a self-developed code of FUELTM. The simulation results indicate that (1) the out-of-plane displacements of Al alloy side plates are mainly attributed to the bending deformations; (2) enhanced out-of-plane displacements appear in fuel plates adjacent to the outside Al plates, which results from the occurred bending deformations due to the applied constraints of outside Al plates; (3) an intense interaction of fuel foil with the cladding occurs near the foil edge, which appears more heavily in the fuel plates adjacent to the outside Al plates. The maximum first principal stresses in the fuel foil are similar for all the fuel plates and appear near the fuel foil edge; while, the through-thickness creep strains of fuel foil in the fuel plate near the central region of fuel assembly are larger, and the induced creep damage might weaken the fuel skeleton strength and raise the fuel failure risk.

평행사변형 유한요소의 강성 매트릭스와 하중 매트릭스 (Stiffness and Load Matrix for Finite Parallelogrammic Plate Bending Element)

  • 조병완
    • 한국전산구조공학회:학술대회논문집
    • /
    • 한국전산구조공학회 1989년도 봄 학술발표회 논문집
    • /
    • pp.28-32
    • /
    • 1989
  • 최근에 건설된 여러 토목구조물에서 평행사변형 모양으로 이루어진 구조 요소들이 점차 생겨나고있다. 특히 미국의 일부 I-75 고속도로에서 쓰여진 평행사변형 모양의 슬라브구조나 지형학적 또는 구조역학적인 이유로 인한 고량의 평행사변형 모양 슬라브는 하중의 편심재하로 인한 구조역학의 정확한 해석의 필요성을 야기시켰다. 이에 본 연구는 유한요소법에 의한 평행사변형 요소의 강성매트릭스와 하중매트릭스를 유도하여 평행사변 유한요소를 해석할수있는 구조해석용 서브루틴 프로그램(Subroutine Program)을 만들고 특히 경사 죠인트를 가진 도로구조 해석용 쇼프트웨어(Software)를 만드는데 목적이있다.

  • PDF

중지압 운반 갱도내 변형계측 및 하중역산에 관한 연구 (A Study on the In-Situ Measurement of the Deformation and the Back Calculation of the Load in the Mine Roadway Over-Stressed Rocks)

  • Cho, Young-Soo;Kim, Hong-Woo;Shin, Hee-Soon;Chung, So-Keul;Lee, Hi-Keun
    • 터널과지하공간
    • /
    • 제3권1호
    • /
    • pp.40-49
    • /
    • 1993
  • In this study, the indirect estimation method of the support load which is based upon the integrated measuring technique suggested by Kovari was applied to the calculation of support load in the mine roadway. Four test supports were installed in the area where they had to be replaed. Two of those were GI-130 rigid supports and the others were U-26 yieldable supports. The vibrating wire strain gages which were attached inpairs on the steel arch support were used to provide an accurate measurement. Bending moments and normal forces obtained from strain gage pairs were used to calculate the support load. This method was also verified by laboratory bending tests. The results obtained from the back-calculction method showed relatively good agreement with the measured convergence for each crossection.

  • PDF

유한두께를 가지는 보강된 균열평판에 대한 면외굽힘을 고려한 응력강도계수 계산 (Calculation of stress intensity factor considering out-of-plane bending for a patched crack with finite thickness)

  • 김종호;이순복
    • 대한기계학회:학술대회논문집
    • /
    • 대한기계학회 2000년도 춘계학술대회논문집A
    • /
    • pp.165-169
    • /
    • 2000
  • A simple method was suggested to calculate the stress intensity factor for a one-sided patched crack with finite thickness. To consider out-of-plane bending effect resulting from the load-path eccentricity, the spring constant as a function of the through-thickness coordinate z was calculated from the stress distribution in the un-cracked plate, ${\sigma}_{yy}(y=0,\;z)$, and the displacement for the representative single strip Joint, $u_y(y=0,\;z)$. The stress Intensity factors were obtained using Rose's asymptotic solution approach and compared with the finite element results. In short crack region, two results had a little difference. However, two results were almost same in long crack region. On the other hand, the stress intensity factor using plane stress assumption was more similar to finite element result than plane strain condition.

  • PDF

선수선형(船首船型)의 파랑하중(波浪荷重) 특성(特性) (The Effect of Forebody Section Shape on Wave Loads)

  • 황종흘;이승준;유재문
    • 대한조선학회지
    • /
    • 제19권1호
    • /
    • pp.15-22
    • /
    • 1982
  • The effects of the forebody geometry of ships on the response function of wave loads are investigated by numerical calculations based on a strip method. For the vertical wave loads both shearing forces and bending moments, the V-shaped bow gives greater responses than the U-shaped one in regular oblique waves. These results have been clarified by the vector diagram of all static and dynamic components contributing to the resultant wave bending moment. In the present evaluation the phase relation among the components plays an important role. And the effect of the forebody geometry on lateral wave loads seems to be negligible from the result of the present investigation.

  • PDF

A compressible finite element model for hyperelastic members under different modes of deformation

  • Manna, M.C.;Sheikh, A.H.;Bhattacharyya, R.
    • Structural Engineering and Mechanics
    • /
    • 제24권2호
    • /
    • pp.227-245
    • /
    • 2006
  • The performance of a three dimensional non-linear finite element model for hyperelastic material considering the effect of compressibility is studied by analyzing rubber blocks under different modes of deformation. It includes simple tension, pure shear, simple shear, pure bending and a mixed mode combining compression, shear and bending. The compressibility of the hyperelastic material is represented in the strain energy function. The nonlinear formulation is based on updated Lagrangian (UL) technique. The displacement model is implemented with a twenty node brick element having u, ${\nu}$ and w as the degrees of freedom at each node. The results obtained by the present numerical model are compared with the analytical solutions available for the basic modes of deformation where the agreement between the results is found to be satisfactory. In this context some new results are generated for future references since the number of available results on the present problem is not sufficient enough.

U리브 현장용접이음부 응력거동에 관한 연구 (Analysis of Stress Behavior on Field Welded Joints of U-rib in Steel Bridge)

  • 강창입;최성민;국승규;이동욱
    • 한국강구조학회 논문집
    • /
    • 제16권3호통권70호
    • /
    • pp.387-396
    • /
    • 2004
  • 본 연구에서는 강교량의 강상판에서 많이 사용되는 U리브 현장이음부에 대해 시공오차로 인한 단차의 영향을 조사하기 위해 실물 대모형에 대해 응력해석을 실시하였다. 또한 실물대모형 시험체를 제작하여 3점 휨 피로실험을 실시하였으며, 주사형전자현미경(SEM) 및 비치마크를 이용하여 피로균열 발생점 및 피로균열전파방향을 조사하였다. 실물대모형 모델에 대한 응력해석 결과, U리브의 하면 우각부에 응력이 크게 나타났으며, 단차가 커질수록 응력이 현저히 증가하는 것을 확인할 수 있었다. 실물대모형 시험체에 대한 정하중 및 피로실험에서도 U리브 하면의 우각부에 응력이 크게 나타났으며, 단차가 크면 피로수명은 단축되고 단차가 적으면 피로수명은 길어졌다. 또한 파단면 조사결과, 피로균열은 모재측 루트부에서 발생하여 용접비드 표면측으로 전파되었다.

Moment redistribution of RC continuous beams: Re-examination of code provisions

  • Da Luo;Zhongwen Zhang;Bing Li
    • Structural Engineering and Mechanics
    • /
    • 제85권5호
    • /
    • pp.679-691
    • /
    • 2023
  • Many codes allow designers to use the bending moment diagram computed by elastic analysis and modify it by a certain amount of moment redistribution (MR) to account for plastic behaviour of continuous beams. However, several researchers indicated that the MR at the ultimate limit state (𝛽u) for some beams deviate significantly from the specified values of various codes. This paper examines the applicability of the provisions on 𝛽u in ACI 318-19 and Eurocode 2 through numerical investigations and comprehensively explores the influencing factors. The results show that some parameters not considered in those codes influence 𝛽u to a certain extent, where the ratio of tensile reinforcement ratio at intermediate support to tensile reinforcement ratio at midspan (𝜌s1/𝜌s2) and load type are crucial parameters to consider. The specific combination of these two parameters may make the codes overestimate or significantly underestimate the 𝛽u. On the other hand, the yield state of both critical sections is found to have an important influence on the influence degree of each parameter on 𝛽u. The yield conditions are investigated, and an empirical judgment equation is proposed. In addition, the influence laws of the critical parameters on 𝛽u have been further proved by theoretical derivation. Finally, due to 𝜀t is found to have a better linear correlation with 𝛽u than xu/d, equations as a function of 𝜀t for predicting the 𝛽u of continuous beams under the two loads are proposed, respectively.