• 제목/요약/키워드: limit strain

검색결과 507건 처리시간 0.034초

고온 크리프 구조물의 장시간 한계응력강도 예측 (Prediction of Long-Term Stress Intensity Limit of High-Temperature Creep Structures)

  • 김우곤;류우석;김현희
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2003년도 춘계학술대회
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    • pp.648-653
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    • 2003
  • In order to predict stress intensity limit of high-temperature creep structures, creep work-time equation, defined as $W_ct^P=B$, was used, and the results of the equation were compared with isochronous stress-strain curve (ISSC) ones of ASME BPV NH Code. For this purpose, the creep strain tests with. time variations for commercial type 316 stainless steel were conducted with different stresses; 160 MPa, 150 MPa, 145 MPa, 140 MPa and 135 MPa at $593^{\circ}C$. The results of log $W_c$ and log t plots showed a good linear relation up to $10^5$ hr. The constants p, B and stress intensity limit values showed comparatively good agreement to those of ASME NH ISSC. It is believed that the relation can be simply obtained with only several short-term 1% strain data without ISSC which can be obtained by long-term creep data.

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판재의 이론적 변형한계 스트레인의 면외압 의존성 (Effect of Out-of- Plane Stress on the theoretical Forming Limit Strain of Sheet Metals)

  • 정태훈
    • 한국공작기계학회:학술대회논문집
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    • 한국공작기계학회 2004년도 추계학술대회 논문집
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    • pp.162-169
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    • 2004
  • In press forming of sheet metals, the material sheet is usually subjected to very large plastic strain under in-plane stressing. Moreover, the sheet also very often is subjected to out-of-plane compressive force between tools such as the upper and lower dies, the blank holder and the die, and so forth. In this paper, it is clearly demonstrated theoretically that out-of-plane stress may notably raise the forming limit strain and thus it can be effectively utilized to avoid earlier fracture of the sheet in press forming.

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레이디얼 압출에서 플랜지의 성형한계 (The Forming Limit of Flange in the Radial Extrusion)

  • 고병두;장동환;최호준;임중연;황병복
    • 소성∙가공
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    • 제12권3호
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    • pp.228-235
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    • 2003
  • In this paper, the workability of flange in the radial extrusion is analyzed in terms of the deformation pattern, the punch load and the forming limit by using simulation and experiment. A single action pressing is applied to both simulation and experiment. The analysis in this study is focused on the transient extrusion into the gap in radial direction with various gap heights and die corner radius. Based on the surface strains where surface cracking occurs, the forming patterns and strain-fracture relationships in producing radially extruded flange are obtained.

액성한계에 따른 재성형 점토의 압밀특성에 관한 연구 (A Study on Consolidation Characteristics of Remolded Clay due to the Liquid Limit)

  • 임형민
    • 한국지반환경공학회 논문집
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    • 제15권5호
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    • pp.67-74
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    • 2014
  • 본 연구에서는 점토의 액성한계에 따른 압밀특성을 연구하기 위하여 일정한 압력으로 예압밀 된 재성형 점토를 이용하여 표준압밀시험과 일정변형률 압밀시험을 수행하였다. 압밀시료들은 카올리나이트에 중량대비 6 %, 9 %, 12 %, 15 %의 벤토나이트를 혼합하여 제작하였으며, 시료들의 액성한계시험을 수행한 결과 각각 77 %, 84 %, 88 %, 91 %의 값을 얻을 수 있었다. 또한 액성한계의 약 2배의 증류수를 첨가 후 충분히 교반하여 0.2 MPa의 일정한 압력조건하에 예압밀시켜 제작하였다. 최근 일반적으로 사용되고 있는 표준압밀시험과 ASTM, D4186-82에 따라 변형률 속도를 0.001 %/min, 0.004 %/min, 0.01 %/min을 적용하여 일정변형률 압밀시험을 수행하고 선행압밀하중을 0.2 MPa의 예압밀압력에 대해서 비교 분석하였다. 그 결과 액성한계가 낮을수록 빠른 변형률 속도에서 선행압밀하중이 예압밀압력과 유사하게 나타났으며, 액성한계가 높을수록 느린 변형률 속도에서 선행압밀하중이 예압밀압력과 유사하게 나타났다.

Influence of brass laminate volume fraction on electromechanical properties of externally laminated coated conductor tapes

  • Bautista, Zhierwinjay M.;Shin, Hyung-Seop;Lee, Jae-Hun;Lee, Hunju;Moon, Seung-Hyun
    • 한국초전도ㆍ저온공학회논문지
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    • 제18권3호
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    • pp.6-9
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    • 2016
  • The enhancement of mechanical properties of coated conductor (CC) tapes in practical application are usually achieved by reinforcing through lamination or electroplating metal layers on either sides of the CC tape. Mechanical or electromechanical properties of the CC tapes have been largely affected by the lamination structure under various loading modes such as tension, bending or even cyclic. In this study, the influence of brass laminate volume fraction on electromechanical properties of RCE-DR processed Gadolinium-barium-copper-oxide (GdBCO) CC tapes was investigated. The samples used were composed of single-side and both-side laminate of brass layer to the Cu-stabilized CC tape and their $I_c$ behaviors were compared to those of the Cu-stabilized CC tape without external lamination. The stress/strain dependences of $I_c$ in laminated CC tapes under uniaxial tension were analyzed and the irreversible stress/strain limits were determined. As a result, the increase of brass laminate volume fraction initially increased the irreversible strain limit and became gradual. The corresponding irreversible stress limit, however, showed no difference even though the brass laminate volume fraction increased to 3.4. But the irreversible load limit linearly increased with the brass laminate volume fraction.

인장과 휨변형하에서 목재의 응력이완 및 이론모형 (Stress Relaxation of Wood and Theoretical Models under Tensile and Bending Strain)

  • 장상식;강춘원
    • Journal of the Korean Wood Science and Technology
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    • 제26권4호
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    • pp.13-19
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    • 1998
  • Stress relaxation tests have been performed under five different tensile strain levels and five different bending strain levels. Three different theoretical models have been developed based on four-element Burger's model, viscoelastic theory and viscous-viscoelastic theory. Experimental data were used to obtain parameters of the models and to verify accuracy of the models. Among the three theoretical models developed in this study, three-integral model (Model 3) based on viscous-viscoelastic theory showed the most exact estimations of stress relaxation under both tensile and bending strains and their correlation coefficients were greater than 0.99 for all the strain levels. Model 1 showed little initial stress relaxation. Model 2 showed excessive initial relaxation and, then, no relaxation after about 20 minute of strain application. Stress retention under strain decreased as strain increased, which means increased stress relaxation as strain increases. When the strain level was less than proportional limit, the effect of strain level on stress relaxation was not clearly shown. However, this effect was increased as strain level increased when strain level was greater than proportional limit.

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AZ31 합금 판재의 변형모드에 따른 성형한계에 관한 연구 (Forming Limits Diagram of AZ31 Alloy Sheet with the Deformation Mode)

  • 정진호;이영선;권용남;이정환
    • 소성∙가공
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    • 제17권7호
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    • pp.473-480
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    • 2008
  • Sheet metal forming of Mg alloy is usually performed at elevated temperature because of the low formability at room temperature. Therefore, strain rates affected with the forming temperature and speed must be considered as important factor about formability. Effects of process parameters such as various temperatures and forming speeds were investigated in circular cup deep drawing. From the experimental results, it is known that LDR (Limit Drawing Ratio) increase as the strain rate increase. On the contrary, the FLD (Forming Limit Diagram) shows lower value as faster strain rate. Therefore, anisotropy values are investigated according to the temperature and strain rates at each forming temperature. R-values also represent higher value as faster strain rate. It is known that the formability can be different with the deformation mode on warm forming of AZ31 alloy sheet.

다층금속 경사재의 변형양태의 수치적연구 (Numerical simulation for Deformation Shape of Declined Multilayer Metals Material)

  • 정태훈
    • 한국공작기계학회:학술대회논문집
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    • 한국공작기계학회 2004년도 춘계학술대회 논문집
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    • pp.124-128
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    • 2004
  • By the use of a similar numerical method as that in the previous paper, the forming limit strain by coaling method of clad sheet metals is investigated, in which the FEM is applied and J2G(J$_2$-Gotoh's corner theory) is utilized as the plasticity constitutive equation. Declined Multilayer Metals Materials are stretched in a plane-strain state, with various work-hardening exponent n-values and thicknesses of each layer. Processes of shear-band formation in such composite sheets are clearly illustrated. It is concluded that, in the bonded state, the higher limiting strain of one layer is reduced due to the lower limiting strain of the other layer and vice versa, and does not necessarily obey the rule of linear combination of the limiting strain of each layer weighted according thickness.

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M-K 모델 기반의 박판금속 성형성 평가에서 물성의 영향에 대한 해석적 연구 (Analytical Study of the Effect of Material Properties on the Formability of Sheet Metals based on the M-K Model)

  • ;김석봉;허훈
    • 소성∙가공
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    • 제19권7호
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    • pp.393-398
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    • 2010
  • This paper investigates the effect of material properties on the formability of sheet metals based on the Marciniak-Kuczynski model (M-K model). The hardening behavior of the material is modeled as the Hollomon model with the strain rate effect. The yield surfaces are constructed with Hosford79 yield function. The material properties considered in this study include the R-value, the strain hardening exponent, the strain rate hardening exponent, and the crystal structure of the material. The effect of the crystal structure on formability is roughly expressed as the change of the yield surface by varying the value of the exponent in Hosford79 yield function. Results show that the R-value affects neither the magnitude nor the shape of right hand side of forming limit diagrams (FLDs). Higher strain hardening exponent and higher strain rate hardening exponent improve the formability of sheet metals because they stabilize the forming processes.

DNS 자료에 의한 저레이놀즈수 2차 모멘트 난류모형의 개발 (Development of Low-Reynolds-Number Ssecond Moment Turbulence Closure by DNS Data)

  • 신종근;최영돈
    • 대한기계학회논문집B
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    • 제20권8호
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    • pp.2572-2592
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    • 1996
  • A low-Reynolds-number second moment turbulence closure was developed with the aid of DNS data. Model coefficients of nonlinear return to isotropy term were derived by use of Cayley-Hamilton theorem and two component turbulence limit condition as the functions of invariances of anisotropy and turbulent Reynolds number. Launder and Tselepidakis' cubic mean pressure strain model was modified to fit the predicted pressure-strain components to the DNS data. Two component turbulence limit condition was the precondition to be satisfied in developing the second moment turbulence closure for the realizable Reynolds stress prediction. But the satisfactions of Reynolds stress level and pressure-strain level of each component were compromised because the satisfaction of both levels was impossible.