• Proceedings of the Korean Institute of Surface Engineering Conference
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• 2017.05a
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• pp.111-111
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• 2017

쇼트피닝 기술은 크게 피로강도 향상을 위한 쇼트피닝(shot peening), 재료의 청정 및 도장 품질 향상을 위한 쇼트블라스트(shot blast) 그리고 쇼트피닝 시 판재의 변형되는 성질을 이용한 핀포밍(peen forming) 등으로 구분할 수 있다. 그 중 본 연구에서는 해양산업 분야에서 널리 사용되는 회주철의 효과적인 내구성 향상을 위해 쇼트피닝 기술을 적용하였다. 그러나 쇼트피닝 기술 적용에 있어서 가장 중요한 것은 제품의 균일성, 정확성, 신뢰성을 확보하기 위해 쇼트피닝 강도를 제어하는 여러 가지 변수들에 대하여 최적 상태를 유지하는 것이다. 따라서 회주철에 대한 최적 쇼트피닝 분사조건 규명작업은 반드시 쇼트피닝 가공 전에 수반되어야만 한다. 그 일환으로 실험은 쇼트피닝 분사시간과 분사압력을 변수로 하여 회주철 표면에 적용하였으며, 기계적 특성 평가를 통해 최적의 쇼트피닝 조건을 규명하고자 하였다. 쇼트피닝 분사조건에 따른 회주철의 내구성을 평가하기 위해 캐비테이션 실험을 실시하였으며, 경도 측정, 횡단면 관찰 및 표면의 3D 현미경 관찰 등을 통해 기계적 특성을 분석하였다. 캐비테이션 실험은 ASTM G32 규정에 의거하여 천연해수 내 $30^{\circ}C$에서 $50{\mu}m$의 진폭으로 실시하였다. 실험 후에는 주사전자현미경으로 손상표면을 관찰하였으며, 손상 정도를 비교하기 위해 무게 감소량을 계측하여 상호 비교/분석하였다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.33 no.2
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• pp.60-66
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• 2005

Corrosion highly affects the lifetime and performance of machinery metallic components. The effects of shot peening on the fatigue life of Al 7075-T6 under corrosive environment are investigated in this paper. Experimental results show that the fatigue limit of shot peened specimen increases about 52%. That means the fatigue life of metallic components is highly extended by shot peening. The corrosion greatly reduces the fatigue strength depending on the corrosive condition from one week up to one year. In case of shot peened specimen, the corrosion does not reduce the fatigue strength and fatigue life up to six months. It means that the shot peening has superior effectiveness to reduce the influence of corrosion to the metallic materials.

• Journal of the Korean Society of Marine Environment & Safety
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• v.19 no.5
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• pp.545-551
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• 2013

In this study, shot peening technique was employed with shot peening time for durability improvement and surface modification of copper alloy to investigate the electrochemical characteristics and microstructural variations. As a result of shot peening, roughness was distributed over the surface, and homogenization phenomenon was observed with increasing shot peening time due to the enhancement of coverage. The results revealed that hardness increased for shot peened specimens and particularly 3.5 mins of shot-peening time represented a hardness improvement of 52 %, showing similar electrochemical characteristics to that of the un-peened surface.

• Proceedings of the Korean Institute of Surface Engineering Conference
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• 2008.11a
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• pp.138-138
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• 2008

H13강에 대해 이온질화에 대한 쇼트피닝의 효과를 살펴보았다. 쇼트피닝을 이온질화는 기존이온질화에 비해 높은 경도와 깊은 경화층을 얻을 수 있었다. 이는 쇼트피닝에 의해 결정립계와 전위밀도가 증가함에 따라 질화공정이 가속화된 것으로 보인다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.31 no.7
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• pp.63-68
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• 2003

Shot peening process is most often used to improve the fatigue properties of metal parts, In order to achieve an optimum, repeatable, and reliable fatigue enhancement from the shot peening process, the important shot peening parameters must be optimized, In this paper, the optimum peening intensity(Almen intensity) condition is investigated by experiment. Rotary bending fatigue test has been adopted to investigate the effects of optimum peening on the fatigue characteristics, Experimental results show that the fatigue strength and fatigue life has been tremendously increased by optimum-peening treatment. However, the fatigue strength and fatigue life has been decreased by under or over peening.

• Journal of the Korean Society for Nondestructive Testing
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• v.26 no.5
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• pp.291-296
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• 2006

The residual stress in shot-peened Al 7075 alloy was evaluated using surface acoustic wave (SAW). Shot peening was conducted to produce a variation in the residual stress with the depth below the surface under a shot velocity of 30 m/s. The SAW velocity was measured from the V(z) curve using a scanning acoustic microscopy (SAM). The Vickers hardness profile from the surface showed a significant work hardening near the surface layer with a thickness of about 0.25 mm. As the residual stress became more compressive, the SAW velocity increased, whereas as the residual stress became more tensile, the SAW velocity decreased. The variation in the SAW velocity through the shot peened surface layer was in good agreement with the distribution of the residual stress measured by X-ray diffraction technique.

• Journal of the Korean Society for Railway
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• v.12 no.6
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• pp.895-901
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• 2009

Fatigue fracture of the welded joints of bogie frames is one of unsolved problems. To improve the fatigue strength of the welded joints, various techniques have been applied. In this study, we have investigated the effect of shot peening on the fatigue characteristics of SS400 welded specimens. The fatigue lives of four kinds of welded specimens were examined; welded, PWHT, shot peened, and shot peened after PWHT. The results of the fatigue tests show that the fatigue limit of the shot-peened specimens is higher than that of the welded specimens, and the PWHT specimens have a lower fatigue limit than the welded specimens. It was found that shot peening is a very effective method to improve the fatigue strength of SS400 welded joints.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.36 no.11
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• pp.1381-1389
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• 2012

The object of this study considers corrosion fatigue improvement of 7075-T6 aluminum by using shot peening treatment on 3.5% NaCl solution at room temperature. Aluminum alloy is generally used in aerospace structural components because of the light weight and high strength characteristics. Many studies have shown that an aluminum alloy can be approximately 50% lighter than other materials. Mostly, corrosion leads to earlier fatigue crack propagation under tensile conditions and severely reduces the life of structures. Therefore, the technique to improve material resistance to corrosion fatigue is required. Shot peening technology is widely used to improve fatigue life and other mechanical properties by induced compressive residual stress. Even the roughness of treated surface causes pitting corrosion, the compressive residual stress, which is induced under the surface layer of material by shot peening, suppresses the corrosion and increases the corrosion resistance. The experimental results for shot peened specimens were compared with previous work for non treated aluminum alloy. The results show that the shot peening treatment affects the corrosion fatigue improvement of aluminum alloys and the induced compressive residual stress by shot peening treatment improves the resistance to corrosion fatigue.

• Proceedings of the KSME Conference
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• 2005.11a
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• pp.140.2-140.2
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• 2005

• Proceedings of the Korean Society of Marine Engineers Conference
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• 2012.06a
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• pp.254-254
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• 2012