• 한국정밀공학회:학술대회논문집
• /
• 한국정밀공학회 1993년도 추계학술대회 논문집
• /
• pp.475-481
• /
• 1993

The objective of this study is to develope the reliability prediction model for Float Rated Integrating Gyroscope( :FRIG) at maximum loading. The equation of motion for FRIG is firstly derived to set up the reliability prediction model. To analysis reliability or all parts of the gyro is not easy due to their complicated structure. Therefore the failure parts are chosen by Failure Mode Effective Analysis (:FMEA). F.E.M is utilized to calculate loads for the selseced rotating assembly and pivot / jewel. The technical reliability is calculated by applying reliability design theory with these results and the performance reliability is sought through distribution estimation with error test data. The bulk reliability of gyroscope is sought by applying the two results. The present prediction results are compared with the accumulation time in good agreement.

• Earthquakes and Structures
• /
• 제2권3호
• /
• pp.279-295
• /
• 2011

This paper develops a probabilistic methodology for the seismic reliability analysis of structures with random properties. The earthquake loading is assumed to be described in terms of response spectra. The proposed methodology takes advantage of the response spectra and thus does not require explicit dynamic analysis of the actual structure. Uncertainties in the structural properties (e.g. member cross-sections, modulus of elasticity, member strengths, mass and damping) as well as in the seismic load (due to uncertainty associated with the earthquake load specification) are considered. The structural reliability is estimated by determining the failure probability or the reliability index associated with a performance function that defines safe and unsafe domains. The structural failure is estimated using a performance function that evaluates whether the maximum displacement has been exceeded. Numerical illustrations of reliability analysis of elastic and elastic-plastic single-story frame structures are presented first. The extension of the proposed method to elastic multi-degree-of-freedom uncertain structures is also studied and a solved example is provided.

• International Journal of Concrete Structures and Materials
• /
• 제9권3호
• /
• pp.267-281
• /
• 2015

Six full-scale prestressed concrete (PC) I-beams with steel fibers were tested to failure in this work. Beams were cast without any traditional transverse steel reinforcement. The main objective of the study was to determine the effects of two variables-the shear-span-to-depth ratio and steel fiber dosage, on the web-shear and flexural-shear modes of beam failure. The beams were subjected to concentrated vertical loads up to their maximum shear or moment capacity using four hydraulic actuators in load and displacement control mode. During the load tests, vertical deflections and displacements at several critical points on the web in the end zone of the beams were measured. From the load tests, it was observed that the shear capacities of the beams increased significantly due to the addition of steel fibers in concrete. Complete replacement of traditional shear reinforcement with steel fibers also increased the ductility and energy dissipation capacity of the PC I-beams.

• 한국윤활학회:학술대회논문집
• /
• 한국윤활학회 2001년도 제34회 추계학술대회 개최
• /
• pp.331-340
• /
• 2001

Elastic-Plasitc Finite element analysis is peformed about the TiN coated medium. The normal contact is simulated by a rigid asperity pressing the surface of an elastic-plastic half-surface. The case of a surface film stiffer than the substrate is considered, and general solutions for the subsurface stress and deformation fields are presented for several coating thickness. Additionally, the critical normal loads for deformation in the substrate and coating fracture are calculated when the yield of TiN film follows the Maximum Principal Stress Theory and Von Mises Theory. The results can be subsumed in failure maps for TiN thin film on steel.

• Structural Engineering and Mechanics
• /
• 제61권1호
• /
• pp.117-124
• /
• 2017

Load testing is one of the important tests to determine if the structural elements can be used at the intended locations for which they have been designed. It is nothing but gradually applying the loads and measuring the deflections and other parameters. It is usually carried out to determine the behaviour of the system under service/ultimate loads. It helps to identify the maximum load that the structural element can withstand without much deflection/deformation. It will also help find out which part of the element causes failure first. The load-deflection behaviour of the road bridge girder has been studied by carrying out the load test after simulating the field conditions to the extent possible. The actual vertical displacement of the beam at mid span due to the imposed load was compared with the theoretical deflection of the beam. Further, the recovery of deflection at mid span was also observed on removal of the test load. Finally, the beam was checked for any cracks to assert if the beam was capable of carrying the intended live loads and that it could be used with confidence.

• Composites Research
• /
• 제30권2호
• /
• pp.132-137
• /
• 2017

본 연구에서는 카본/BMI 면재와 노멕스 허니콤 코어를 가지는 샌드위치 포팅 체결부의 다양한 설계변수에 대한 파손특성 연구를 수행하였다. 샌드위치 시편은 코어 높이, 면재 두께 및 밀도에 따라 총 6종류가 제작되었고, 이중 1종류의 시편에 대해 온/습도 효과를 보기 위해 환경 조건이 가해졌다. 시험 결과 밀도가 $64kg/m^3$ 코어를 제외한 모든 시편에서 코어의 전단좌굴이 초기 파손모드로 나타났으며, 이후 하중을 지지하다 윗면재 파손과 동시에 아랫면재에 볼트가 파고드는 파손형상이 나타났다. 하지만 밀도에 의해 높은 강성을 가지는 시편의 경우 초기 전단좌굴 발생 없이 윗면재와 코어의 계면파손에 의해 낮은 최대파손하중을 나타냈다. 샌드위치 시편의 환경적 영향 평가를 위해 수행된 ETW1($82^{\circ}C$, Wet)과 ETW2($177^{\circ}C$, Wet)의 경우 RTD($24^{\circ}C$, Dry) 조건과 확연히 다른 초기 파손모드를 보였으며, 동일한 습도조건 하에 온도가 상승된 ETW2는 ETW1보다 전단좌굴 하중이 약 18% 감소되는 경향을 보였다.

• 항공우주기술
• /
• 제2권2호
• /
• pp.105-114
• /
• 2003

본 논문에서는 KSR-III 1단부의 도로운송과 핸들링시에 예상되는 진동하중의 분석을 다룬다. 일반적으로 기체가 이송 중에 겪는 진동하중은 실제 기체가 비행 중에 겪는 진동 환경과는 많은 차이가 있다. 이송시 겪는 진동하중 특성에 대한 부적절한 해석은 이송 중에 로켓시스템에 직접적인 손상을 야기할 수 있을 뿐만 아니라, 비행임무 실패로 이어질 수도 있다. 그러므로, 기체 설계단계에서부터 이송시 진동하중을 함께 고려하여야 하며, 이송에 대한 적절한 방법을 강구해야 한다. 본 연구에서는, KSR-III의 도로운송이나 핸들링시의 진동하중을 예측하여 그 규격을 설정하는 과정을 기술하며, 저진동 이송치구의 동특성 분석과 사전도로테스트를 통하여 이송치구와 이송과정의 타당성을 검증하고, KSR-III 단인증 모델(1단)의 이송결과를 정리하고 분석한다. KSR-III 운송과정중의 최대허용 진동하중은 2g이며, 실제 운송결과 이보다 작은 값이 기록되었다.

• 한국해안해양공학회지
• /
• 제16권3호
• /
• pp.142-151
• /
• 2004

수리학적 안정성과 구조적 안정성을 동시에 만족시키면서 피복재의 중량을 산정할 수 있는 방법이 수립되었다. 수리학적 안정성은 Hudson의 경험식을 이용하여, 구조적 안정성은 충격하중 작용시 피복재 내부에 발생되는 최대인장응력을 산정, 피복재의 인장 저항력과 비교하는 개념으로 해석되었다. 이와 같이 산정된 수리학적 안정성과 구조적 안정성에 대한 적용한계를 재현기간별 설계 유의파고, 피복재의 중량, 그리고 인장 저항력의 함수로 제시하여 실무자들이 쉽게 사용할 수 있도록 하였다. 또한 결정론적 산정법의 불확실성을 고려하기 위하여 수리학적 안정성과 구조적 안정성에 대한 신뢰성 해석이 추가로 수행되었다. 두 파괴모드를 하나의 직렬계로 구성하여, 신뢰성설계법에서 이용되는 목표파괴확률을 가지고 단면파괴율의 함수로 피복재의 최적중량을 산정할 수 있었다.

• 대한기계학회논문집A
• /
• 제32권9호
• /
• pp.782-787
• /
• 2008

First, the effect of the geometry such as the curved shape of the struts composing the truss structure of WBK is elaborated. Then, analytic solutions for the material properties of WBK and the maximum loads of a WBK-cored sandwich panel under bending are derived. A design optimization with the face sheet thickness and the core height selected as the design variables is presented for given slenderness ratios of the WBK core. Unless the face sheet thickness is limited, the optimal design to give the maximum load per weight is always found at a confluence of three failure modes, namely, face sheet yielding, indentation plastic, and core shear modeB plastic.

• Wind and Structures
• /
• 제39권1호
• /
• pp.47-69
• /
• 2024

Pounding of structures may result in considerable damages, to the extent of total failure during severe lateral loading events (e.g., earthquakes and wind). With the new generation of tall buildings in densely occupied locations, wind-induced pounding becomes of higher risk due to such structures' large deflections. This paper aims to develop mathematical formulations to determine the maximum pounding force when two adjacent structures come into contact. The study will first investigate wind-induced pounding forces of two equal-height structures with similar dynamic properties. The wind loads will be extracted from the Large Eddy Simulation models and applied to a Finite Element Method model to determine deflections and pounding forces. A Genetic Algorithm is lastly utilized to optimize fitting parameters used to correlate the maximum pounding force to the governing structural parameters. The results of the wind-induced pounding show that structures with a higher natural frequency will produce lower maximum pounding forces than those of the same structure with a lower natural frequency. In addition, taller structures are more susceptible to stronger pounding forces at closer separation distances. It was also found that the complexity of the mathematical formula from optimization depends on achieving a more accurate mapping for the trained database.