• Transactions of the Korean Society of Mechanical Engineers A
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• v.41 no.7
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• pp.635-643
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• 2017

The purpose of this study is to investigate the influence of the cold reduction rate and an ultrasonic fatigue test (UFT) on the fatigue behaviors of STS 304L. The tensile strength, yield strength, hardness value and fatigue limit in the UFT fatigue test linearly increased as thickness decreased from 1.5 mm to 1.1 mm, as the cold reduction rate of STS 304L increased. As a result of the UFT fatigue test (R = -1) of four specimens, the fatigue limit of the S-N curve formed a knee point in the region of $10^6$, and the 2nd fatigue limit caused by giga cycle fatigue did not appeared. In the case of t = 1.1 mm, the highest fatigue limit was 345 MPa, which was 64.3% higher than the original material (t = 1.5 mm). As a result of the UFT fatigue test of STS 304L, many small surface cracks occurred, grown, coalesced while tearing.

• Journal of the Korean Society for Railway
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• v.15 no.3
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• pp.266-271
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• 2012

This study was carried out for the purpose of improving driving safety and comfort of the railways quickly becoming popular. To conducted gas pressure welding to ensure the strength safety of continuous welded rail and rotating bending test tensile test was conducted. The element to determine the tensile strength of gas pressure welds at experiments be attributed to more upsetting length than pressure, according to increases of upsetting length, from brittle fracture to ductile fracture was observed. Through the biopsy of the fracture surface, according to the presence of brittle fracture could be evaluated to strength safety. In addition, mechanical strength of gas pressure welding depending on changes in upsetting length was different. Rotary bending test results were obtained to the infinite life according to exhibited higher fatigue limit of 373MPa at upsetting length 25mm.

• Proceedings of the KSR Conference
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• 2002.05a
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• pp.399-403
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• 2002

The transmission system of high speed train serve in the severe condition compared with those of other trains, namely, they have to transmit high power to run with high speed and they have to make maximum use of the limited space. To clarify the strength of gear for Korea High-Speed Train, a bending fatigue test of gear specimen is performed and compare with actual gear's. From this result, specimen test is useful to infer S-N curve and endurance limit of actual gear that much time and expense are consumed.

• Bulletin of the Society of Naval Architects of Korea
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• v.32 no.1
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• pp.50-54
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• 1995

선박의 구조설계단계에서 최종붕괴강도를 설계기준으로 삼는 경우는 거의 없으나 최근에 각국 선급에서 최종붕괴강도를 의무적인 설계기준으로 삼기 위해 자체적인 해석법과 설계식을 제시 하고 규정화하는 작업을 진행시키고 있다. [12, 17, 31, 32]. 1994년 ISSC [1]에서도 토론된바와 같이 특히 새로운 구조방식을 가진 선박의 합리적인 구조설계를 위하여는 해상플렛폼의 구조설 계시와 마찬가지로 삼아야 할 것이다. 본고에서는 선각거더의 최종붕괴강도에 대한 해석법과 간이계산식에 관한 연구동향을 문헌조사를 통하여 분석하였다. 그 결과 순수굽힘모멘트가 작용 하는 문제의 경우 최종붕괴강도 해석법은 어느정도 확립되었다고 판단되지만 최종붕괴강도의 간이계산식은 아직도 정도 등의 면에서 개선의 여지가 남아 있다고 생각된다. 앞으로 순수 굽 힘모멘트뿐만아니라 조합하중을 받는 경우와 피로균열을 비롯한 초기구조손상을 가진 노후화된 선박에 대한 최종붕괴강도를 보다 정밀하게 해석하기 위한 해석법의 개발과 간이계산식의 도 출이 필요하다고 사료된다. 또한, 충돌, 좌초, 폭발 등에 기인된 선각거더의 붕괴강도 평가를 위한 해석법의 개발도 앞으로 남은 과제중의 하나이다.

• Journal of Dental Rehabilitation and Applied Science
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• v.24 no.3
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• pp.269-281
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• 2008

Fatigue or overload can result in mechanical problems of implant components. The mechanical strength in the implant system is dependent on several factors, such as screw and fixture diameters, material, and design of the fixture-abutment connection and abutment. In these factors, the last rules the strength and stability of the fixture-abutment assembly. There have been some previous reports on the mechanical strength of the fixture-abutment assembly with the compressive bending test or short-term cyclic loading test. However, it is restrictive to predict the long-term stability of the implant system with them. The purpose of this study was to evaluate the influence of the design of the fixture-abutment connection and abutment on the mechanical strength and failure mode by conducting the endurance limit test as well as the compressive bending strength test. Tests were performed according to a specified test(ISO/FDIS 14801) in 4 fixture-abutment assemblies of the Osstem implant system: an external butt joint with Cemented abutment (group BJT), an external butt joint with Safe abutment (group BJS), an internal conical joint with Solid abutment (group CJO), and an internal conical joint with ComOcta abutment (group CJT). The following conclusions were drawn within the limitation of this study. Compressive bending strengths were decreased in order of group BJS(1392.0N), group CJO(1261.8N), group BJT(1153.2N), and group CJT(1110.2N). There were no significant differences in compressive bending strengths between group BJT and group CJT(P>.05). Endurance limits were decreased in order of group CJO(600N), group CJT(453N), group BJS(360N), and group BJT(300N). 3. Compressive bending strengths were influenced by the connection and abutment design of the implant system, however endurance limits were affected more considerably by the connection design.

• Journal of Dental Rehabilitation and Applied Science
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• v.25 no.4
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• pp.349-360
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• 2009

Purpose: As the esthetic demands of dental implant patients are increased, the demands of zirconia as implant abutment material are also increased. It has non-metalic color, good biocompatibility, high strength and high toughness. Even thought the advatage of zirconia abutment, there are a few studies about mechanical properties of zirconia abutment. This study evaluated the mecanical strength with compressive bending strength and endurance limit of implant-zirconia abutment assembly. Materials and Methods: Static and cyclic loading of implant-Zirconia abutment assembly were simulated under worst case condition according to ISO. Test groups were implants of external butt joint with straight regular diameter and angled regular diameter zirconia abutment, implant of external butt joint with narrow straight diameter zirconia abutment and implant of internal conical joint with straight narrow diameter zirconia abutment. All test group were evaluated the mecanical strength with compressive bending strength and endurance limit. After fatique testing, fracture surface were examined by SEM. Results: The compressive bending strengths exceed 927N. Regular diameter zirconia abutment were stronger than narrow diameter zirconia abutment(P<.05). The endurance limits ranged from 503N to 868N. Conclusion: Within the limitation of this study, zirconia implant abutment exceeded the estabilished values for maximum incisal biting forces reported in the literature.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.20 no.9
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• pp.2819-2832
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• 1996

The estimation of the remaining life for the aged components in power plant as well as chemical and petroleum plants has been recently concerned. The raw materials used in this study are the 1Cr-1Mo-0.25V steel which intensified P and S compositions along with the nominal compositions of ASTM A 470 standard. Five kinds of specimens with the different degradation levels were prepared by isothermal aging heat treatment at 630.deg.C. The mechanical properties and rotated bending fatigue strength of virgin and aged 1Cr-1Mo-0.25V steel have been investigated through the hardness, tensile, fatigue test, SEM fractograph and EDS analysis at 538.deg.C and room temperature, respectively. Thus the data of aged specimens were compared with those of virgin specimen to evaluate the aging effects. The main results obtained in this study are as follows ; The decrease of the yield and tensile strength due to degradation was distinguished until 50, 000hrs simulated service time. And it was confirmed that the considerable amount of P, Mn, Cr and S was precipitated at the grain boundary of aged material through the SEM and EDS analysis. The rotated bendingd fatigue strength at 538.deg.C of virgin, 25, 000, 50, 000, 75, 000 and 100, 000 hrs aged material was decreased 44.6 %, 49.6 %, 51.5 %, 52.4% and 53.8% than that of virgin material at 10$_{7}$cycles of room temperature, respectively. The major cracks of virgin and aged materials mainly initiated at the inclusions including Si, P and Mn compositions which were located at the outer periphery of the specimen.n.

• Proceedings of the Korean Society for Agricultural Machinery Conference
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• 2017.04a
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• pp.62-62
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• 2017

모터와 스크류를 이용한 경량 식혈기를 처음으로 개발함에 따라 실제 산림의 식재 시험에서 발생될 수 있는 것은 감속기와 스크류의 연결부분의 파괴이다. 이 감속기 축의 파괴는 토양내부의 큰 자갈로 인해 스크류가 낄 경우 식재봉을 좌우로 흔들게 되면 가장 취약한 부분인 스크류와 감속기의 연결부위에 가장 강한 모멘트가 걸리게 된다. 물론 작업자의 부주위가 원인이기도 하지만 감속기(K6G30C. Korea)의 축 지름이 8mm이므로 식재봉을 좌우로 흔들면 굽힘파괴가 일어날 가능성이 높다. 감속기의 축이 파괴가 되지 않게 하는 방법은 재료의 강도가 높은 새로운 감속기를 찾은 일과 기존 감속기의 축을 굽힘응력에 안전하게 대응할 수 있게 설계를 하는 방법이 있다. 본 연구에서는 전자에 대한 조사와 동시에 후자에 대한 설계와 제작을 수행하여 기 제작된 경량식혈기와 비교 분석하였다. 스크류 축의 굽힘응력에 대한 대응 방법으로 감속기 축의 보강방법은 감속기 축에 식재봉으로 부터 굽힘응력이 직접 전달되지 않게 하기 위해 모터 하우징의 하부 위치에 감속기 축을 감싸는 Radial Bearing을 결합하였다. 그리고 스크류의 축은 상단의 지름을 크게 키운 상태로 감속기의 축에 연결하는 방법으로 설계하였다. 이때 식혈봉으로 부터 걸리는 모멘트는 스크류의 상단 지름에 걸리게 되는데 상단부는 모터 하우징의 하단과 단단하게 결합함으로써 감속기 축을 보호하게 되고 또한 감속기 축의 길이에서 Bearing과 스크류 상단부 큰 지름이 각각 반반씩 보호하는 형태로 설계하였다. 이와 같이 감속기의 축을 보강한 경우 종전의 식혈기보다 무게가 무거워지게 된다. 즉, 1차 식혈기 무게는 3.38kgf, 2차 시작기는 3.28kgf, 축 강도가 보강된 3차 시작기는 무게가 3.87kgf로 증가되었다. 따라서 종전보가 약 600g 증가되어 다소 무거운 느낌이 들었다. 여기서 리듐 폴리머 배터리와 가방의 무게 3.23kgf를 부가하면 1차, 2차, 3차 시작기의 무게는 각각 6.61kgf, 6.51kgf, 7.1kgf로 나타났다. 따라서 굽힘응력에 대한 보강의 방안으로 설계된 무게 과다가 현장 시험에서 작업자의 피로도 증가와 작업의 비효율성이 예상되어 포트묘의 현장 식재시에 이에 대한 평가를 수행하여 비교 분석할 예정이다.

• Journal of Welding and Joining
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• v.13 no.2
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• pp.96-105
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• 1995

A modified method for the analysis of short fatigue crack growth has been presented, and calculations based upon the modified method are compared with experimental results for S45C carbon steel. It is also shown that the modified method is in good agreement with experimental data. The proposed equation for the fatigue crack growth rates includes a material constant which relates the threshold level to the endurance limit, a correction for elastic-plastic behaviour and a means for dealing with the effects of crack closure. In this study one of the modifications is to substitute the Forman' s elastic expression of the stress intensity factor range into the geometrical factor The other is a consideration of the bending effect which is developed from the moment caused by the eccentric cross sectional geometry as the crack grows. Thus, this method is useful for residual life prediction of the mechanical structures as well as the welding structures.

• Journal of the Korean Society of Fisheries and Ocean Technology
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• v.24 no.2
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• pp.94-100
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• 1988

Recently with the rapid development in marine and shipbuilding industries such as marine structures, ship, and chemical plants, there occurs much interest in the study of corrosion fatigue characteristics was closed up an important role in mechanical design. In this study, the 5086 Al-Alloy was tested by used of a rotary bending fatigue tester and was investigated under the environments of various specific resistance and air. The specific resistance, as a corrosion environment, was changed 15, 20, 25 and 5000$\Omega$.cm. The corrosion fatigue crack initiation sensitivity was quantitatively inspected for 5086 Al-Alloy in the various specific resistance. The experimental constants of Paris rule were examined in the various specific resistances, and the influences of load and corrosion with affect the crack growth rate were compared with. Main results obtained are as follows: (1) Number of stress cycles to corrosion fatigue crack initiation delaies and corrosion fatigue crack initiation sensitivity decreases with the increasing for the specific resistance. (2) The experimental constant m of Paris rule decreases with the decreasing for specific resistance. Hence the effect of corrosion is more susceptible than that of stress intensity factor. (3) The corrosion fatigue crack of 5086 Aluminium Alloy appears intergranular fracture. (4) Corrosion sensitivity is decreased with the increasing stress intensity factor and is nearly uniform when stress intensity factor is over 40kg.mm super(-3/2)