• 제목/요약/키워드: Residual Structure

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컨테이너 기중기의 제어 : 수정된 시간최적주행과 비선형 잔류흔들림 제어 (Container Crane Control: Modified Time-Optimal Traveling Followed by Nonlinear Residual Sway Control)

  • 홍금식
    • 제어로봇시스템학회논문지
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    • 제5권5호
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    • pp.630-639
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    • 1999
  • To achieve fast loading and unloading of containers from a container ship, quick suppression of the remaining sway motion of the container at the end of each trolley stroke is crucial. Due to the pendulum motion of the container and disturbances like sind, residual sway always exists at the end of trolley movement. In this paper, the sway-control problem of a container crane is investigated. A two-stage control is proposed. The first stage is a time optimal controlfor the purpose of fast trolley traveling. The second stage is a nonlinear control for the quick suppression of residual sway, which starts right after the first stage while lowering the container. The nonlinear control is investigated in the perspective of controlling an underatuated mechanical system, which combines partial feedback linearization to account for the known nonlinearities as much as possible, and variable structure control to account for the unmodeled dynamics and disturbances. Simulation and experimental results are provided.

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고속가공에서 미시적 정밀도의 특성 평가 (Characteristic evaluation of microscopic precision in high speed machining)

  • 김철희;김전하;강명창;김정석
    • 한국공작기계학회:학술대회논문집
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    • 한국공작기계학회 2001년도 춘계학술대회 논문집(한국공작기계학회)
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    • pp.352-357
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    • 2001
  • In this study, residual stress was investigated to evaluate damaged layer in high speed machining through simulation. In machining steel(STDll), residual stress remaining in machined surface was mainly appeared as compressive stress. The scale of this damaged layer more depends on feed per tooth and radial depth than spindle speed. Damaged layer was measured by optical microscope and hardness method. The micro-structure of damaged layer was a martensite because of cutting force and cutting temperature. Thickness of damaged layer is increased with incresing of feed per tooth and radial depth.

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유전자 알고리즘을 이용한 구조물 손상 탐색기법에 관한 연구 (A Study for Structural Damage Identification Method Using Genetic Algorithm)

  • 우호길;최병민
    • 한국소음진동공학회논문집
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    • 제17권1호
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    • pp.80-87
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    • 2007
  • In this paper, a method for identifying the location and extent of a damage in a structure using residual forces was presented. Element stiffness matrix reduction parameters in a finite element model were used to describe the damaged structure mathematically. The element stiffness matrix reduction parameters were determined by minimizing a global error derived from dynamic residual vectors, which were obtained by introducing a simulated experimental data into the eigenvalue problem. Genetic algorithm was used to get the solution set of element stiffness reduction parameters. The proposed scheme was verified using Euler-Bernoulli beam. The results were presented in the form of tables and charts.

항공기용 알루미늄 판재의 냉간가공 특성 연구 (A Study on Cold Working Properties of Aluminum Plates for Aircraft Structure)

  • 이동석;이준현
    • 한국정밀공학회지
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    • 제20권3호
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    • pp.165-171
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    • 2003
  • In a structure, many components are fastened together using bolts, nuts and rivets through drilled holes. Not only do these fastened joints enable easy assembly and dismantling, they are also able to transfer as well as to distribute loads applied onto the structures. The major drawback of such connections, however, is that the fatigue life of the components is reduced by the presence of the hole since the stress concentration around the hole is increased. In addition, the hole drilling process itself may introduce defects or roughness at the surfaces of the hole that may cause further decrease in fatigue performance of the components. For applications where fatigue loadings are important, one way to compensate the decrease in fatigue life of the components is by introduction of beneficial compressive residual stress around the hole using cold working. The material used for this research were A12024-T351 and A17050-T7451 using the primary member of aircraft. We present, In this paper, the characteristics of coldworking by evaluation of the hole expansion ratio, residual stress distribution, and fatigue properties.

형상기억합금의 양방향효과를 이용한 두개의 형상기억합금선이 부착된 작동기의 수치해석 (Numerical Simulation of Double SMA wire Actuator Using Two-Way Shape Memory Effect of SMA)

  • 김상헌;조맹효
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2004년도 추계학술대회논문집
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    • pp.287-290
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    • 2004
  • A structure using the two-way shape memory effect (TWSME) returns to its initial shape by increasing or decreasing temperature under initial residual stress. Through the thermo-mechanical constitutive equation of shape memory alloy(SMA) proposed by Lagoudas et al., we simulate the behavior of a double actuator in which two SMA wires are attached to the tip of panel under the initially given residual stress. Through the numerical results conducted in the present study, the proposed actuator device is suitable for repeated actuation. The simulation algorithm proposed in the present study can be applied extensively to the analysis of the assembled .system of SMA-actuator and host structure in the practical applications.

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선체 용접부의 균열진전 및 피로수명예측에 관한 연구(II) (A Study of Crack Propagation and Fatigue Life Prediction on Welded Joints of Ship Structure (II))

  • 김경수;심천식;권영빈;고희승;기혁근
    • 대한조선학회논문집
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    • 제45권6호
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    • pp.679-687
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    • 2008
  • The fatigue life of ship structure under cyclic loading condition is made up of crack initiation and propagation stages. For a welding member in ship structure, the fatigue crack propagation life is more important than the fatigue crack initiation life. To calculate precisely the fatigue crack propagation life at the critical welding location, the knowledge of the residual stress sensitivity on the fatigue strength is necessary. In this study, thermo elastic-plastic analysis was conducted in order to examine the effect of residual stress on the fatigue crack propagation life. Also the fatigue crack propagation lives considering residual stress were calculated using fatigue crack growth code, AFGROW, on the basis of fracture mechanics. AFGROW is widely used for fatigue crack growth predictions under constant and variable amplitude loading. The reliability of AFGROW on the fatigue of ship structure was confirmed by the comparison of the estimated results with the fatigue propagation test results.

상변태를 고려한 탄소강 용접부의 잔류응력 해석에 관한 연구 (A Study on the Analysis of Residual Stress in Weldment by Considering the Phase Transformation of Carbon Steel)

  • 조시훈;김재웅
    • 대한기계학회논문집A
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    • 제25권3호
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    • pp.390-398
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    • 2001
  • Welding process generates distortion and residual stress in the weldment due to rapid heating and cooling. Welding distortion and residual stress in the welded structure result in many troubles such as dimensional inaccuracies in assembling and safety problem during service. The accurate prediction of welding residual stress is thus very important to improve the quality of weldment and find the way to reduce itself. This paper suggests new analysis method to predict welding residual stress by considering solid phase transformation during welding process. Using the method, analysis is performed for medium and low carbon steel. The analysis result for medium carbon steel reveals that case considering phase transformation has compressive residual stress in contrast with the case neglecting phase transformation because of martensite formation. However, for the case of low carbon steel, residual stress shows little difference between the case considering phase transformation and the other case, because it has small transformation strain and recovers rapidly stress after phase transformation.

가압 급냉하에서의 사출 성형품내의 잔류 응력 형성 해석 (Residual stress formation in injection-molded samples under constrained quenching)

  • 윤경환
    • 한국정밀공학회지
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    • 제14권11호
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    • pp.58-68
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    • 1997
  • The residual stresses in injection-molded plastic parts can be divided into two, i.e., the flow-induced residual stress produced in flowing stage and the thermally-induced residual stress produced in cooling stage. Especially, the main source for the defect in the final parts, such as warpage, is known to be the thermally-induced stresses. For the freely quenched samples the structures of residual stresses and bire-fringence have been investigated by many researchers extensively. However, the boundary condition for free quenching was found to be improper to study actual injection molding process. In the present study a datailed structure of the residual stresses and birefringence produced under constrained quenching has been investigated experimentally. In constrained quenched samples a similar pattern but much less stress values than that for the freely quenched samples has been found in the case of the thickness of 1.0 mm. Howvere, in the case of the thickness of 4.0mm, totally different stress profile has been found experimentally. Suprisingly uniform birefringence throughout whole thickness has been found for all the cases of constrained quenching. Finally, to explain the mechanism to produce the final residual stresses and bire-fringence some preliminary numerical results including free volume theory have been introduced briefly.

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용접(鎔接) 강구조(鋼構造) 부재(部材)의 잔류응력(殘留應力) 특성(特性)에 관한 연구(研究) (A Study on the Characteristics of the Residual Stress Distribution of Steel Structural Members)

  • 장동일;김두환
    • 대한토목학회논문집
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    • 제7권1호
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    • pp.93-101
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    • 1987
  • 용접부(鎔接部)에서 잔류응력(殘留應力)은 용접열(鎔接熱)에 의한 국부(局部) 가열(加熱)과 불규칙적(不規則的)이고 비교적(比較的) 급속(急速)한 냉각(冷却)으로 유발(誘發)되는 열응력(熱應力)과 구조물(構造物)의 강성(剛性) 및 재료(材料) 등에 의하여 발생(發生)되며, 잔류응력(殘留應力)의 존재(存在)는 취성파괴강도(脆性破壞强度), 피로강도(疲勞强度), 좌굴강도(挫屈强度), 진동특성(振動特性), 부식저항(腐蝕抵抗) 등에 영향(影響)을 미치는 궁극적(窮極的) 요인(要因)으로 간주(看做)됨으로 본(本) 연구(硏究)는 구조물(構造物)의 강도(强度)를 저하(低下)시키고 기능(機能)에 악영향(惡影響)을 끼치는 잔류응력(殘留應力)의 기구학적(機構學的) 특성(特性)을 파악(把握)하기 위하여 SWS 58 강판(鋼板)을 X홈 용접(鎔接)하여 이것을 4단계(段階) 즉 $350^{\circ}C$, $500^{\circ}C$, $650^{\circ}C$, $800^{\circ}C$로 열처리(熱處理)하여 hole drilling method를 사용(使用)하여 잔류응력(殘留應力)을 측정(測定)한 결과(結果), 다음과 같은 결론(結論)을 얻었다. 잔류응력(殘留應力)을 제거(除去)시키는 가장 효과적(效果的)인 온도(溫度)는 $650^{\circ}C$ 정도(程度)이었고, 구멍의 직경(直經)이 구멍의 깊이와 일치할 때 구멍바로 근처(近處)의 소성변형(塑性變形)은 완전(完全)히 해방(解放)되었으며, 경도시험(硬度試驗)을 통(通)해 열처리(熱處理) 후(後) 열영향부(熱影響部)의 높은 경도(硬度)가 모두 삭감(削減)되는 것을 알 수 있었으며 또한 잔류응력(殘留應力)에 끼치는 용접입열(鎔接入熱)의 영향(影響)은 입열량(入熱量)의 표준(標準)보다 1/4 이상(以上), 이하(以下)인 경우 잔류응력(殘留應力)은 용접입열(鎔接入熱)에 큰 영향(影響)이 없음을 알았다.

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