• Structural Engineering and Mechanics
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• 제75권6호
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• pp.701-711
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• 2020

This papers studies nonlinear stability and post-buckling behaviors of geometrically imperfect metal foam doubly-curved shells with eccentrically stiffeners resting on elastic foundation. Metal foam is considered as porous material with uniform and non-uniform models. The doubly-curved porous shell is subjected to in-plane compressive loads as well as a transverse pressure leading to post-critical stability in nonlinear regime. The nonlinear governing equations are analytically solved with the help of Airy stress function to obtain the post-buckling load-deflection curves of the geometrically imperfect metal foam doubly-curved shell. Obtained results indicate the significance of porosity distribution, geometrical imperfection, foundation factors, stiffeners and geometrical parameters on post-buckling characteristics of porous doubly-curved shells.

• Structural Engineering and Mechanics
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• 제60권4호
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• pp.615-631
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• 2016

In this paper, an analytical method for the Post-buckling response of cylindrical shells with spiral stiffeners surrounded by an elastic medium subjected to external pressure is presented. The proposed model is based on two parameters elastic foundation Winkler and Pasternak. The material properties of the shell and stiffeners are assumed to be continuously graded in the thickness direction. According to the Von Karman nonlinear equations and the classical plate theory of shells, strain-displacement relations are obtained. The smeared stiffeners technique and Galerkin method is used to solve the nonlinear problem. To valid the formulations, comparisons are made with the available solutions for nonlinear static buckling of stiffened homogeneous and un-stiffened FGM cylindrical shells. The obtained results show the elastic foundation Winkler on the response of buckling is more effective than the elastic foundation Pasternak. Also the ceramic shells buckling strength higher than the metal shells and minimum critical buckling load is occurred, when both of the stiffeners have angle of thirty degrees.

• Structural Engineering and Mechanics
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• 제84권6호
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• pp.767-782
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• 2022

In this paper, the nonlinear vibration behavior of the spiral stiffened multilayer functionally graded (SSMFG) cylindrical shells exposed to the thermal environment and a uniformly distributed harmonic loading using a semi-analytical method is investigated. The cylindrical shell is surrounded by a nonlinear viscoelastic foundation consisting of a two-parameter Winkler-Pasternak foundation augmented by a Kelvin-Voigt viscoelastic model with a nonlinear cubic stiffness. The distribution of temperature and material constitutive of the stiffeners are continuously changed through the thickness direction. The cylindrical shell has three layers consisting of metal, FGM, and ceramic. The interior layer of the cylindrical shell is rich in metal, while the exterior layer is rich in ceramic, and the FG material is located between two layers. The nonlinear vibration problem utilizing the smeared stiffeners technique, the von Kármán equations, and the Galerkin method has been solved. The multiple scales method is utilized to examine the nonlinear vibration behavior of SSMFG cylindrical shells. The considered resonant case is 1:3:9 internal resonance and subharmonic resonance of order 1/3. The influences of different material and geometrical parameters on the vibration behavior of SSMFG cylindrical shells are examined. The results show that the angles of stiffeners, temperature, and elastic foundation parameters have a strong effect on the vibration behaviors of the SSMFG cylindrical shells.

• 헤리티지:역사와 과학
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• 제46권3호
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• pp.212-228
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• 2013

파손된 석조문화재를 재사용하기 위한 방법으로 금속보강재를 사용하게 되는데 현재까지 보강재에 대한 보존처리 지침 없이 처리자의 경험에 의해서 이루어지다 보니 여러 가지 문제점이 도출되고 있다. 따라서 2차적인 원부재의 훼손을 최소화하기 위한 금속봉의 구조적 보강방법과 거동 특성 등을 제안된 실험체를 통해 검증 받아 금속보강재 매입방법에 관한 설계기준을 마련하고자 하였다. 절단면에 에폭시수지 접합만 할 경우 원 모재 물성의 70% 정도밖에 회복되지 않아 30%에 대한 금속보강재의 구조적 보강이 필요하다. 금속봉은 석재 취성파괴 후 구조적 거동을 받는데 금속보강재비가 0.251% 이하로 설계되면 구조적 거동은 발생하지 않으며, 0.5% 이상이면 구조적 보강은 이루어지나 모재의 2차 훼손을 유발시킨다. 따라서 $1,500kgf/cm^2$ 강도를 갖는 석재의 적정 금속보강재비는 접착단면적의 0.283~0.377% 정도로 설계되어야 가역성 있는 파손과 보강재의 연성거동이 이루어진다. 또한 휨 하중에 대응되는 금속봉의 최대 응력을 기대하기 위해서는 보강재 간격을 멀리하는 것보다 가깝게 유지하는 것이 효율적이며, 특히 상부에 보강재를 매입하는 것은 구조적으로 아무런 도움이 되지 못하고 오히려 원부재의 손상만 유발한다. 따라서 보강재는 하부에 집중배치하고 일부 중앙부에 매입하여야 안정적인 인장재 역할을 하면서 하중응력을 받는다. 금속봉의 분산효과는 보강봉의 면적에 영향을 받을 뿐 지름과는 무관하였다. 하지만 큰 규모를 대상으로 할 때는 접착 단면을 고려하여 보강재 개수를 늘려주는 것이 하중응력에 안정적이다. 이때 적용되는 정착길이는 보강재의 직경에 따라 다음과 같은 식($l_d=a_tf_y/u{\Sigma}_0$)에 의거하여 설계한다. 또한 구조재로서 거동을 하기 위해서는 반드시 마디가 있는 전산형 보강봉을 사용하여야 한다.

• Steel and Composite Structures
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• 제37권1호
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• pp.51-73
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• 2020

The present paper investigates the simultaneous resonance behavior of spiral stiffened multilayer functionally graded (SSMFG) cylindrical shells with internal and external functionally graded stiffeners under the two-term large amplitude excitations. The structure is embedded within a generalized nonlinear viscoelastic foundation which is composed of a two-parameter Winkler-Pasternak foundation augmented by a Kelvin-Voigt viscoelastic model with a nonlinear cubic stiffness. The cylindrical shell has three layers consist of ceramic, FGM, and metal. The exterior layer of the cylindrical shell is rich ceramic while the interior layer is rich metal and the functionally graded material layer is located between these layers. With regard to classical shells theory, von-Kármán equation, and Hook law, the relations of stress-strain are derived for shell and stiffeners. The spiral stiffeners of the cylindrical shell are modeled according to the smeared stiffener technique. According to the Galerkin method, the discretized motion equation is obtained. The simultaneous resonance is obtained using the multiple scales method. Finally, the influences of different material and geometrical parameters on the system resonances are investigated comprehensively.

• Structural Engineering and Mechanics
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• 제74권2호
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• pp.255-266
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• 2020

The main requirements of modern welded metal structures are the load-carrying capacity (safety), fitness for production, and economy. The primary objective of attaching longitudinal stiffeners is to improve the buckling strength of relatively thin compression panels. This paper gives several comparisons for stiffened plates with different loadings (static, dynamic), different shape of stiffeners (flat, L-shape, trapezoidal), different steel grades, and different welding technologies (SMAW, GMAW, SAW), different costs to show the necessity of a combination of design, fabrication and economic aspects. Safety and fitness for production are guaranteed by fulfilling the design and fabrication constraints. The economy is achieved by minimizing the cost function. It is shown that the optimum sizes depend on the welding technology, the material yield stress, the profile of the stiffeners, the load cycles and the place of the production.

• Steel and Composite Structures
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• 제28권6호
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• pp.735-748
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• 2018

In this study, the semi-analytical finite strip method is adopted to examine the free vibration of cylindrical shells made up of functionally graded material. The properties of functionally graded shells are assumed to be temperature-dependent and vary continuously in the thickness direction according to a simple power law distribution in terms of the volume fraction of ceramic and metal. The material properties of the shells and stiffeners are assumed to be continuously graded in the thickness direction. Theoretical formulations based on the smeared stiffeners technique and the classical shell theory with first-order shear deformation theory which accounts for through thickness shear flexibility are employed. The finite strip method is applied to five different shell theories, namely, Donnell, Reissner, Sanders, Novozhilov, and Teng. The approximate procedure is compared favorably with three-dimensional finite elements. Finally, a detailed numerical study is carried out to bring out the effects of power-law index of the functional graded material, stiffeners, and geometry of the shells on the difference between various shell theories. Finally, the importance of choosing the shell theory in simulating the functionally graded cylindrical shells is addressed.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1996년도 한국자동제어학술회의논문집(국내학술편); 포항공과대학교, 포항; 24-26 Oct. 1996
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• pp.516-519
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• 1996

Sub-assembly in ship manufacturing is a sequence of filet joint welding of stiffeners on metal panels and the process is different depending on companies. In this paper, we introduce a new intelligent robotic system of the sub-assembly process in Samsung Heavy Industry, where one shift of 22m * 9m workspace includes one to ten panels and each panel includes up to 10 stiffeners. The inherent problems such as several hundreds of different panels, unstructured task environment and the large scale do not allow a fixed automation, but needs highly intelligent versatile automation. The robotic system is composed of four 14DOF macro-mini robots and a task recognition system. Application of this system has verified the task specification such as low temperature environment(-10.deg. C) and productivity is satisfied successfully.

• 보존과학회지
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• 제28권2호
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• pp.141-151
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• 2012

석조문화재의 훼손된 부재를 재사용하기 위한 보존관리는 1900년대부터 시작되었다고 볼 수 있는데 일제강점기 시대에 무기물인 시멘트를 원료로 사용하면서 부터이다. 1990년대에 접어들면서 건축 재료인 유기질의 에폭시수지가 도입되었고 현재에 이르기까지 석조문화재 전반에 활용되고 있다. 특히 절단된 부재의 구조적 보강에도 충전제를 혼합하여 사용하는 등의 적극적인 보존처리 작업이 진행되었다. 그러나 구조적 보강을 위해 넣은 금속봉의 길이는 보존과학자의 인지적 경험을 바탕으로 설계하였기 때문에 다양한 매입길이와 함께 원부재의 2차적 훼손을 유발할 수 있다. 따라서 본 실험을 통해 원부재의 훼손율을 최소화하면서 최대의 구조적 보강을 하기 위해 유효정착길이를 표준화한 결과 ø8mm 는 60.88mm, ø12mm는 91.32mm, ø16mm는 121.76mm가 적정하였다. 이 외의 구경은 ${\ell}_d=a_tf_y/u{\Sigma}_0$을 이용하여 정착길이를 구한다. 이 때 사용된 금속보강재는 전산형 환봉을 사용하여야 휨, 전단, 압축 등의 재하하중에 대항할 수 있었다.

• Steel and Composite Structures
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• 제35권4호
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• pp.567-578
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• 2020

Based on third-order shear deformation shell theory, the present paper investigates post-buckling properties of eccentrically stiffened metal foam curved shells/panels having initial geometric imperfectness. Metal foam is considered as porous material with uniform and non-uniform models. The single-curve porous shell is subjected to in-plane compressive loads leading to post-critical stability in nonlinear regime. Via an analytical trend and employing Airy stress function, the nonlinear governing equations have been solved for calculating the post-buckling loads of stiffened geometrically imperfect metal foam curved shell. New findings display the emphasis of porosity distributions, geometrical imperfectness, foundation factors, stiffeners and geometrical parameters on post-buckling properties of porous curved shells/panels.