• 한국해양공학회지
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• 제23권3호
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• pp.46-52
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• 2009

Nowadays, many components in automobile, aircraft, offshore structure and industry require lightness and high strength. However, since developments of advanced materials have limitations, it mainly is applying to method of surface hardening. This study offered research about camshaft that is one among engine important component. The material used in this study is 0.53% carbon steel as structure material of camshaft, splineshaft, coupling, pulley, driveshaft et cetera. Camshaft is processed using mainly carbon steel, and receives wear and fatigue by special quality high speed of parts. Therefore, camshaft need surface hardening to improve camshaft's fatigue life and increase durability of engine. This study compare to residual stress and martensite microstructure created by high frequency induction treatment, and these results lead to the conclusion of fatigue crack growth characteristics.

• 한국생산제조학회지
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• 제6권4호
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• pp.80-88
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• 1997

An experimental investigation of the fatigue through crack growth behavior under simple stepped variable loading condition has been performed using Al7075-T651. Experiments were carried out by using cantilever bending type specimens, with chevron notches on a small electro-magnetic test machine. Tensile overloads have a retarding effect on the fatigue crack growth rates, therefore tensile overloads were used for the beneficial effect on the fatigue life. While in most cases compressive overloads have only a vanishing effect on crack growth rates, some experiments with single edge crack tension specimens reveal a marked growth retardation. The stress ratios used in this investigations varies from R=0.32 to 0.81, from R=0.04 to 0.76, from R=-0.15 to 0.73, and from R=-0.33 to 0.68 and the peak load for each case was not varied. The crack growth and crack closure were measured by Kikukawa's compliance method with a strain gauge mounted on the backside of each specimens. The results obtained are as follows. When the stepped variable load was applied, the smaller the stress ration was, the larger the delayed retardation of the crack growth rate was. The fatigue crack growh rate data obtained for through cracks were plotted well against the effective stress intensity factor range from 4.0 to 20.0MP{a^{SQRT}m}. It was found that the effective stress intensity factor range ratio was related well to the opening stress intensity factor, the maximum stress intensity factor, and crack length.

• 대한기계학회논문집A
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• 제21권2호
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• pp.305-316
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• 1997

A more efficient method for obtaining the fatigue life enhancement of a structure member with fastener holes is described. It is based on the combined process of cold-expansion and ring-indentation. Residual stresses were induced onto premachined holes using ring-indentation process near the fastener hole combined with cold-expansion. And residual stresses at the vicinity of a hole were evaluated using a fracture mechanics approach. The compressive residual stresses were larger using the combined process than is in the case of simple cold-expansion. Fatigue testing of aluminum specimens showed that the fatigue crack growth retardation emanating from a circular hole was greater for the combined process than for a simple cold-expansion alone.

• 대한기계학회논문집A
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• 제34권7호
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• pp.911-917
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• 2010

본 연구에서는 열적-기계적 주기하중을 받고 있는 엔진 배기매니폴드에 대해서 열응력 해석방법과 열피로수명 예측과정을 제시하였다. 즉, 파손현상이 복잡한 배기시스템의 효율적인 유한요소 모델링 방법과 온도 의존성 재료의 시험결과를 이용한 해석 데이터 구성, 그리고 열사이클 하중에 대한 열응력 및 파손 예측방법을 디젤엔진의 배기매니폴드에 대해서 나타내었다. 일반적으로 배기매니폴드의 파손 취약부에서는 고온영역에서 큰 압축소성변형이 발생하고 냉각시에는 인장의 잔류응력이 나타난다. 따라서 이같은 응력과 변형률의 이력곡선으로부터 소성변형의 진폭 또는 소성에너지의 크기를 얻을 수 있으며 이를 통해서 피로수명을 예측할 수 있다.

• 한국도로학회논문집
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• 제7권2호
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• pp.13-22
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• 2005

건설폐기물로부터 선별된 재생골재의 사용은 천연자원이 부족한 현실에 있어 많은 기회를 제공한다. 전 세계적으로 한정된 천연자원은 고갈되어가고 있으며 골재의 장거리 수송은 낮은 가격의 재생골재를 사용하는 것보다 더 비경제적 일 수 있다. 연간 한국에서 대략 7백만톤의 폐콘크리트가 발생하지만 이중 대략 2-3백만 정도만 재활용되고 있는 실정이다. 본 연구는 폐콘크리트로부터 얻어진 재생골재를 이용하는 방법에 대해서 제시하고자 한다. 재생콘크리트는 압축강도, 휨강도, 피로시험을 위해 w/c 40, 50, 60%에 대하여 제작했으며, 혼화재로는 플라이애쉬 (15%)를 사용하였다. 천연골재에 대한 재생골재의 대체율은 0, 25, 50%로 하였다. 이 연구의 목적은 재생골재 콘크리트의 피로수면과 천연골재 콘크리트의 피로수명을 비교하는데 있다. 본 연구를 통해 재생골재 콘크리트의 피로수명은 천연골재에 대한 재생골재의 대체율과 w/c에 상관성이 있음을 알 수 있었다.

• 한국해양공학회지
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• 제23권2호
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• pp.74-80
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• 2009

Surface hardening treatments, such as using the high-frequency induction hardening method, are widely used to increase the fatigue life and prevent the failure of materials by locally increasing the surface hardness. This method, in particular, brings an improvement in static strength by compressive residual surface stress due to the hardening. In this study, the mechanical properties of high-frequency induction hardened SCM440 steel were investigated. These results were also compared with those for base metal and a Q/T (tempering after quenching) treatment specimen. The test results showed that partially high-frequency induction hardened SCM440 steel specimens were more improved in static strength, surface hardness, fatigue limit, and anti-wear than the base metal and Q/T treatment specimens. In particular, the fatigue limit of the high-frequency induction hardened SCM440 steel increased by more than about 52% compared to that of base metal and by about 25% compared to that of the Q/T specimen.

• Steel and Composite Structures
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• 제43권1호
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• pp.19-30
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• 2022

The static strength and fatigue crack resistance of the aircraft skin structures depend on the materials used and joint type. Most of the commercial aircraft's skin panel structures are made from aluminium alloy and carbon fibre reinforced epoxy. In this study, the fatigue resistance of four joint configurations (metal/metal, metal/composite, composite/composite and composite/metal) with riveted, adhesive bonded, and hybrid joining techniques are investigated with experiments and finite element analysis. The fatigue tests were tension-tension because of the typical nature of the loads on aircraft skin panels susceptible of experimenting fatigue. Experiment results suggest that the fatigue life of hybrid joints is superior to adhesive bonded joints, and these in turn much better than conventional riveted joints. Thanks to the fact that, for hybrid joints, the adhesive bond provides better load distribution and ensures load-carrying capacity in the event of premature adhesive failure while rivets induce compressive residual stresses in the joint. Results from FE tool ABAQUS analysis for adhesive bonded and hybrid joints agrees with the experiments. From the analysis, the energy release rate for adhesive bonded joints is higher than that of hybrid joints in both opening (mode I) and shear direction (mode II). Most joints show higher energy release rate in mode II. This indicates that the joints experience fatigue crack in the shear direction, which is responsible for crack opening.

• Composites Research
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• 제19권1호
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• pp.22-28
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• 2006

금속재 라이너를 갖는 복합재 압력용기는 라이너의 반복 수명 향상을 위해 제조 공정 중 라이너가 압축잔류응력을 갖도록 하는 자긴처리 공정을 적용할 수 있다. 본 연구에서는 자긴처리에 의한 라이너의 압축잔류응력과 이후의 응력 거동을 정확히 예측할 수 있는 유한요소해석 기법을 제시하고, 이러한 해석 결과를 바탕으로 복합재 압력용기의 반복 수명을 예측할 수 있는 방법을 제안한다. 재료 및 기하학적 비선형성을 고려한 3차원 비선형 유한요소해석을 통해 라이너의 응력 거동을 정확히 예측하고, 압력용기의 반복수명을 결정짓는 파라미터로 금속재 라이너의 폰미세스 응력을 도입한다. 라이너 재료에 대한 피로시험과 복합재 압력용기 시제품에 대한 반복시험을 통해 제안된 방법의 타당성과 유효성을 입증한다.

• Journal of Advanced Marine Engineering and Technology
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• 제34권5호
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• pp.661-669
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• 2010

The effects of laser peening on metallic materials have been investigated with water-penetrable frequency-doubled Nd:YAG laser. Laser pulses of 200 mJ energy and 8 ns duration focused on samples underwater with 0.8 mm spot diameter. X-ray study showed that compressive residual stress was imparted on SKD61 from the surface to nearly 2 mm depth. Stress corrosion cracking (SCC) was prohibited for sensitized SUS304 even in a severely corrosive environment fatigue lives of SUS316L and SM490A welded samples were prolonged significantly in the high-cycle regime. Since 1999, laser peening has been applied to prevent SCC in operating nuclear power plants in Japan.

• 한국정밀공학회지
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• 제20권5호
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• pp.148-155
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• 2003

Most manufacturing processes such as welding, cutting and molding generate residual stresses on the surface of manufactured parts. Between compressive and tensile residual stresses, the tensile residual stress is harmful to the surface integrity, which results in reduced fatigue life and causes other structural failures when the service stresses are superimposed on the residual stresses. In the research, the residual stresses in the hardened tool steel (SKD11) were measured using hole-drilling method. The specimens were prepared through hard turning. Most of residual stresses in the machined surface were compressive.