• 항공우주시스템공학회지
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• 제15권2호
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• pp.16-25
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• 2021

Reliability of fatigue strength on Aircraft Composites(GFRP) Structures was assessed in this paper. Fatigue strength of GFRP was used through the existing fatigue test data with Monte Carlo method. The S_a-N_f curve of composites fatigue strength was assumed as normal distribution and reliability was analyzed using SSIT model. Fatigue stress was designed IAW ASTM F3114-15 with special safety factor of S_sf=1.2~2.0. Reliability was calculated by analytic method and FORM. Sensitivity for the effect of mean and standard deviation of fatigue strength as well as fatigue stability was evaluated. This result can be usefully applied to reliability and fatigue design for composite structures of light weight aircraft.

• 대한기계학회논문집A
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• 제29권11호
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• pp.1488-1493
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• 2005

In this study, fatigue tests to obtain S-N curves and FE analyses to obtain structural stress concentration factors were conducted for the two types of cruciform fillet welded joints, that is, load-carrying and non load-carrying types. Then we changed the obtained S-N curve of load carrying joint to that based on hot spot stress. As a result, the S-N curve of load carrying joint based on hot-spot stress was almost exactly coincided with that of non load-carrying joint based on nominal stress. So we have conducted that the fatigue strength of a welded joint with different geometry from the non stress distribution along the expected crack path.

• 한국해양공학회:학술대회논문집
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• 한국해양공학회 2004년도 학술대회지
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• pp.291-296
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• 2004

The paper describes a test program on welded K-joints fabricated from circular hollow section brace members and chords made with API 2W 50 grade steel produced by POSCO. The K-joints were tested for three loading conditions at RIST. The specimens were tested in reaction frame that allowed vertical uniform loading to the structure. From the test, the crack initiation and development were observed and the fatigue failure could be predicted. The results were also compared with the provided S-N curves by DnV.

• 대한조선학회지
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• 제8권2호
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• pp.13-24
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• 1971

When friction welded material is actually used for parts of a machine, its fatigue strength is an important problem. Especially, there is no report which deals with mechanical properties of friction welded mild steel(S20C) and stainless steel(SUS27B). In this study are compared the compared the characteristics of such specimens as mild steel, stainless steel and welded material in the S-N diagram. And metallurgical consideration is directed to HAZ. The obtained results in these studies are summarized as follows; 1) The fatigue strength of welded material is slightly less than those of mild steel and stainless steel. 2) In the S-N diagram the knuckle point of welded material has larger number of cycle than that of stainless steel. 3) The fatigue notch factor of welded material is between those of mild steel and stainless steel. 4) mHv is the largest on the weld interface. It is larger before than after fatigue test on the stainless steel side. On the mild steel side it is the way around.

• Journal of Welding and Joining
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• 제30권1호
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• pp.59-63
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• 2012

The spacer grid is one of the main structural components in a fuel assembly. It supports fuel rods, guides cooling water and maintains geometry from external impact load and cyclic stress by the vibration of nuclear fuel rod, it is necessary to have sufficient strength against dynamic external load and fatigue strength. In this study, the mechanical properties and fatigue characteristics of laser beam welded zircaloy thin sheet are examined. The material used in this study is a zirconium alloy with 0.66 mm of thickness. The fatigue strength under cyclic load was evaluated at stress ratio R=0.1. S-N curves are presented with statistical testing method recommend by JSME- S002 and compared with S-N curves at R.T. and $315^{\circ}C$. As a result of the experimental approach, the design guide of fatigue strength is proposed and the results obtained from this study are expected to be useful data for spacer gird design.

• 항공우주기술
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• 제13권1호
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• pp.10-19
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• 2014

기존의 헬리콥터 로터 시스템에서 기계적 힌지/베어링 부품을 복합재 빔 구성품으로 대체하여 중량과 부품수를 줄인 무베어링 허브 시스템을 설계하였으며, 그 중 중요 구성품인 유연보와 토크튜브에 대한 피로 안전수명 해석을 수행하였다. VABS를 이용한 2차원 단면 해석 수행을 통해 인장, 굽힘 및 뒤틀림 강성을 도출하였으며 2차원 탄성 보 모델에 대한 단면 구조해석 방법을 적용하여 각 단면에 발생하는 변형율을 계산하였다. 각 복합재 소재에 대한 S-N 곡선을 Wohler equation을 적용하여 생성하였으며, 정적구조해석을 통해 피로파손에 취약할 것으로 판단되는 영역에 대한 피로해석을 수행하였다. 헬리콥터 운영시로부터 구성품에 발생하는 하중은 CAMRAD II를 통해 계산하였으며, 하중해석 결과를 HELIX/FELIX 표준 하중 스펙트럼에 적용하여 무베어링 로터 허브 시스템의 하중 스펙트럼을 생성한 후, 이를 통해 최종적으로 피로 안전수명을 산출하였다.

• 콘크리트학회지
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• 제7권6호
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• pp.233-241
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• 1995

본 논문에서는 인장부위가 결손된 철근콘크리트 단순보를 제작하여 유기계 보수재료로서 폴리머계(에폭시, 폴리에스터), 유.무기 혼합 보수재료로서 폴리머-시멘트계(라텍스, 프리믹스), 그리고 부기계 보수재료로서 시멘트계(그라우트)등으로 주입 또는 팻칭의 방법으로 보수한 시험체에 대해 피로실험을 수행하였다. 피로실험은 3점 휨 실험법으로 실시하였으며, 실험시 각 시험체의 하중반복횟수에 대한 보수재의 부착성능, 중앙처짐과 피로파괴시의 반복횟수를 조사하였다. 이들 실험결과를 토대로 반복횟수에 대한 각 보수시험체의 균열 및 파괴양상, 중앙처짐 등을 비교 분석하였으며, 피로강도를 예측하기 위한 S-N선도를 작도하였다. 연구결과, 콘크리트 모체와 보수재와의 부착성능은 폴리머계로 보수한 시험체가 가장 우수하였고, 폴리머-시멘트계 및 시멘트계로 보수한 시험체의 경우는 보수 접합면을 따라 균열이 진전되었다. 반복횟수에 대한 보수시험체의 중앙처짐은 사용하중 상태인 응력수준 60%에서는 모든 보수시험체가 무보수시험체와 유사한 경향을 보였으나 응력수준이 증가할수록 폴리머-시멘트계로 보수한 시험체만이 무보수시험체와 가장 유사한 경향을 나타냈다. 또한 본 피로실험 결과를 회귀분석하여 구한 S-N선도에 의하면 콘크리트 모체와 유사한 재료적 특성을 지닌 폴리머-시멘트계로 보수한 시험체가 무보수 시험체의 피로특성과 가장 유사한 것으로 드러났다.

• 대한조선학회논문집
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• 제38권4호
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• pp.75-82
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• 2001

건조 후 수행하는 수압시험 또는 화물의 적재 등과 같은 정하중은 파랑변동하중에 비하여 선체구조물에 상당히 큰 응력을 유발한다. 이러한 정하중이력에 의하여, 선체구조물의 응력집중으로 인해 피로강도가 문제되는 용접이음부에서는, 재료의 탄소성 거동에 의하여 초기용접잔류응력이 상당히 이완될 것으로 예상된다. 따라서, 이러한 용접이음부의 피로강도를 평가할 때에는 이완된 잔류응력의 영향을 고려하는 것이 보다 합리적이다. 본 연구에서는 선체구조물의 여러 가지 용접형태 중 Padding plate가 용접된 형태에 대하여 정하중이력($0.5{\sigma}Y,\;0.85{\sigma}Y$)에 의한 초기 용접잔류응력의 변화를 측정하며, 잔류응력의 변화가 피로강도에 미치는 영향을 검토한다.

• 한국철도학회:학술대회논문집
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• 한국철도학회 1999년도 춘계학술대회 논문집
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• pp.390-397
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• 1999

This paper investigates about the prediction of rail bending fatigue lifes for the purpose of the effective maintenance of surface irregularities of rail welded parts. The rail bending stresses are calculated using a track dynamic analysis program. The rail surface irregularities measured in situ are given as inputs in the analyses. On the other hand, the S-N curves are derived based on the results of bending fatigue tests. Using data found so far, rail fatigue lifes are estimated adopting a modified Miner's rule. The useful guides for maintenance of rail welded part are proposed in terms of grinding period and grinding depth of rail surface irregularities.

• 한국재료학회지
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• 제6권6호
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• pp.561-567
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• 1996

The grain size effect on grain boyndary cracking in Pb-Sn eutectic during isothermal fatigue was investigated. Fatigue experiments were confined to two conditions : (1) 0.4% total strain range(approximetely 0.2% plastic strain range), 1.67$\times$10$^{-3}$/s frequency; and (2) 1.5% total strain rante(approximately 1.2% plastic strain range), 8.33$\times$10$^{-4}$/s frequency. Fatigue specimens were cross-sectioned to monitor the depth of crack growth continuosly and then, the maximum crack depths in units of the number of boundaries were plotted as functions of number of cycles for these two different strain ranges. The results revealed that the rate of crack growth(per cycle at fixed rate of crosshead motion) can be expressed as dc/dN=($\Delta$$\varepsilon$$_p$)$^n$c where n is typically 2, c is the crack length, $\Delta$$\varepsilon$$_p$ is the plastic strain range, and A is a "constant" that depends on whether the crack is deeper or shallower than its first triple point of the grain boundary, A decrdases by about a factor of three after the crack hits the first triple point, indecating that the fatigue crack is trapped at the triple point of the grain boundaries.