• Steel and Composite Structures
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• 제50권1호
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• pp.63-75
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• 2024

In this paper, the modified couple stress theory (MCST) and first order shear deformation theory (FSDT) are employed to investigate the free vibration and bending analyses of a three-layered micro-shell sandwiched by piezoelectric layers subjected to an applied voltage and reinforced graphene nanoplatelets (GPLs) under external and internal pressure. The micro-shell is resting on an elastic foundation modeled as Pasternak model. The mixture's rule and Halpin-Tsai model are utilized to compute the effective mechanical properties. By applying Hamilton's principle, the motion equations and associated boundary conditions are derived. Static/ dynamic results are obtained using Navier's method. The results are validated with the previously published works. The numerical results are presented to study and discuss the influences of various parameters on the natural frequencies and deflection of the micro-shell, such as applied voltage, thickness of the piezoelectric layer to radius, length to radius ratio, volume fraction and various distribution pattern of the GPLs, thickness-to-length scale parameter, and foundation coefficients for the both external and internal pressure. The main novelty of this work is simultaneous effect of graphene nanoplatelets as reinforcement and piezoelectric layers on the bending and vibration characteristics of the sandwich micro shell.

• 한국전산구조공학회논문집
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• 제23권6호
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• pp.715-726
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• 2010

In this paper, a comparative study of metallic and non-metallic stiffened plates under a lateral pressure load is performed using conventional statistically determinate and SQP(Sequential Quadratic Programming) optimisation approaches. Initially, a metallic flat-bar stiffened plate is exemplified from the superstructure of a marine vessel and, subsequently, its structural topology is varied as hat-section stiffened FRP(Fibre Reinforced Plastics) single skin plates and monocoque FRP sandwich plates having a PVC foam core. These proposed structural alternatives are analysed using elastic closed-form solutions and SQP optimisation method under stress and deflection limits obtained from practice to calculate and optimise geometry dimensions and weights. Results obtained from the comparative study provide useful information for marine designers especially at the preliminary design stage where various building materials and structural configurations are dealt with.

• 한국산학기술학회논문지
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• 제19권1호
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• pp.85-91
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• 2018

최근 초고층 건축물에서 화재로 인해 많은 인명피해가 발생하고 있다. 특히, 화재 발생시 생성되는 유독성 가스 및 연기로 인해 많은 사망자가 발생하고 있다. 이러한 인명피해를 줄이기 위한 방안으로 제연시스템이 도입되어 있다. 제연시스템은 초고층 건축물에서 연기의 확산을 방지하고 재실자의 안전한 피난을 도와주는 장치이다. 또한, 엘리베이터를 이용한 피난은 초고층 건축물에서 필수적인 피난 방법으로 여겨진다. 하지만, 엘리베이터 구동시 생성되는 강력한 압력장 및 유동변화로 인해 제연시스템의 성능확보에 영향을 미친다. 따라서, 본 연구에서는 성능설계위주의 샌드위치 가압방식이 적용된 초고층 건축물에서 엘리베이터 구동에 따른 제연성능 확보에 미치는 영향을 실험 및 수치해석 연구로 수행하였다. 실제 초고층 건축물에서 발생되는 창문, 방화문 그리고 엘리베이터의 누설면적은 화재안전기준 및 면적비를 이용하여 산출하였다. 실제 엘리베이터 속도 7 m/s~17 m/s에 해당하는 20 m/s~100 m/s로 동역학적 상사를 통해 엘리베이터 속도를 변경하였다. 그 결과 엘리베이터 속도가 빠르면 빠를수록 부속실과 화재실 간 차압이 크게 발생하였으며 관계식은 ${\Delta}P=40{\cdot}{\exp}$(-Ves /-104.7)-23.735로 산출되었다. 본 연구 결과는 초고층 건축물에서 엘리베이터 구동을 고려한 제연시스템 설계 자료로 활용이 가능하다.

• 비파괴검사학회지
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• 제37권2호
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• pp.99-105
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• 2017

Many composite materials are used in the aerospace industry because of their excellent mechanical properties. However, the nature of aviation exposes these materials to high temperature and high moisture conditions depending on climate, location, and altitude. Therefore, the molecular arrangement chemical properties, and mechanical properties of composite materials can be changed under these conditions. As a result, surface disruptions and cracks can be created. Consequently, moisture-impregnating defects can be induced due to the crack and delamination of composite materials as they are repeatedly exposed to moisture absorption moisture release, fatigue environment, temperature changes, and fluid pressure changes. This study evaluates the possibility of detecting the moisture-impregnating defects of CFRP and GFRP honeycomb structure sandwich composite materials, which are the composite materials in the aircraft structure, by using an active infrared thermography technology among non-destructive testing methods. In all experiments, it was possible to distinguish the area and a number of CFRP composite materials more clearly than those of GFRP composite material. The highest detection rate was observed in the heating duration of 50 mHz and the low detection rate was at the heating duration of over 500 mHz. The reflection method showed a higher detection rate than the transmission method.

• 한국전기전자재료학회:학술대회논문집
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• 한국전기전자재료학회 2010년도 하계학술대회 논문집
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• pp.321-321
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• 2010

In this paper, we propose a novel type shaft-less ring type ultrasonic motor. A traveling wave rotary type ultrasonic motor is selected as a base model. The newly designed stator has two piezoelectric ceramic rings which are bonded in sandwich shape as traveling wave generator. So, we can expect to produce higher torque. The proposed model has the rotor structure that coupled with the stator provokes the pressure, this model do not install the separate plate any spring device. We used the finite element method to verify the operation principle and to compute the vibration mode of proposed model.

• 소성∙가공
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• 제16권4호
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• pp.239-243
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• 2007

Superplastic forming/diffusion bonding(SPF/DB) has been widely used in the automotive and aerospace industry since it has great advantages to produce very light and strong components. Finite element method(FEM) is used to model the SPF/DB process of 3-sheet sandwich panel to predict the pressure-time curve and to analyze the process parameters. In order to eliminate defects of the part, a new pressurization scheme is proposed. Contrary to the conventional one-step pressurization, which causes the folding at the DB joint, two-step pressurization can eliminate the folding. Effect of pressurization cycle was investigated by using FE analysis and proper pressurization cycle is proposed.

• Advances in aircraft and spacecraft science
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• 제5권4호
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• pp.477-498
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• 2018

The main goal of this article is to validate a methodological process in Actran MSC Software, that is based on the Finite Element Method, to evaluate the comfort in the cabin of a regional aircraft and to study the noise and vibrations reduction through the fuselage by the use of innovative materials. In the preliminary work phase, the CAD model of a fuselage section was created representing the typical features and dimensions of an airplane for regional flights. Subsequently, this model has been imported in Actran and the Sound Pressure Level (SPL) inside the cabin has been analyzed; moreover, the noise reduction through the fuselage has been evaluated. An important investigation and data collection has been carried out for the study of the aircraft cabin to make it as close as possible to a real problem, both in geometry and in materials. The mesh of the structure has been built from the CAD model and has been simplified in order to reduce the number of degrees of freedom. Finally, different fuselage configurations in terms of materials are compared: in particular, aluminum, composite and sandwich material with composite skins and poroelastic core are considered.

• 한국항공우주학회지
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• 제47권5호
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• pp.319-325
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• 2019

본 논문의 목적은 항공기에 장착되는 복합재 라미네이트 및 샌드위치구조를 가지는 레이돔에 대한 조류충돌해석을 수행하고 해석결과와 시험결과를 비교 및 분석하기 위함이다. 먼저 SPH(Smoothed Particle Hydrodynamics)법을 통해 물의 특성을 가지는 조류를 모델링하였으며, 조류충돌시험을 통해 조류가 충돌할 때의 속도를 입력하여 조류충돌해석을 수행하였다. 해석결과를 통해 레이돔의 파손 여부를 조사하고 최대 변형량을 시험결과와 비교하였으며 충돌과정에서의 압력변화추이가 기 연구되었던 결과와 일치함을 확인하였고, 이를 통해 수치해석모델의 신뢰성을 확보하였다. 또한 조류모델을 이루는 입자의 밀도가 레이돔의 파손 형상에 영향을 미친다는 사실을 확인하였다.

• 비파괴검사학회지
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• 제29권4호
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• pp.331-337
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• 2009

우주 발사체는 매우 높은 신뢰도의 경량구조가 필요하다. 비 파괴검사 방법 등을 이용한 구조 건전성 관리가 중요하다. 본 논문에서는 우주발사체의 제작 및 검사에 실제 사용되었던 비 파괴검사 사례 중 일부를 정리하였다. 검사 방법으로는 초음파, X-ray, tapping, 음향방출 등이 사용되었고, 하드웨어로는 페이로드 페어링, 고압탱크, 체결부 및 접합부 등을 대상으로 하였다. 페이로드 페어링에서는 샌드위치 미접착 검사의 정량적 기준을 제시하였고, 고압탱크는 내압 인증시험시 내압증가에 따른 음향방출 데이터를 정리하였다. 샌드위치 체결부에서는 음향방출 신호의 주파수 변화에 따른 파손모드를 분석하였고, 이종재료 접합 구조에서는 미접착부 초음파검사를 위한 표준시편을 제시하였다. 이러한 분석 및 기록은 발사체 시스템을 구성하여 어떠한 상황이 발생하여도 신속하게 판단할 수 있는 근거가 될 수 있으며 발사체 시스템의 신뢰도를 높여주는 역할을 한다.

• 대한본초학회지
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• 제20권2호
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• pp.7-16
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• 2005

Objectives : Scrophulariae Radix (SRE) is commonly used in combination with other herbs as a nutrient and health strengthening agent, and to remove 'heat' and replenish vital essence. The water-based extract of this herb can lower blood pressure in both anesthetized and concious animals, and exhibits an anti-inflammatory activity. But, there is lack of studies regarding the effects of SRE on the immunological activities in molecular levels. The present study was conducted to evaluate the effect of SRE on the regulatory mechanism of cytokines and nitric oxide (NO) in Raw 264.7 cells. Method : After the treatment of Scrophulariae Radix methanol extract, cell viability was measured by MTT assay, NO production was monitored by measuring the nitrite content in culture medium. COX-2 and iNOS were determined by Immunoblot analysis, and levels of cytokine were analyzed by sandwich immunoassays. Results : Results provided evidence that SRE inhibited the production of nitrite and nitrate (NO), inducible nitric oxide synthase (iNOS), $interleukin-1{\beta}\;(IL-1{\beta})$ and interleukin-6 (IL-6), and the activation of phospholylation of inhibitor ${\kappa}B{\alpha}\;(p-I{\kappa}B{\alpha})$ in Raw 264.7 cells activated with lipopolysaccharide (LPS). Conclusion : These findings suggest that Scrophulariae Radix can produce anti-inflammatory effect, which may playa role in adjunctive therapy in Gram-negative bacterial infections.