• Title/Summary/Keyword: High fatigue strength

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Evaluation on Fatigue Crack Propagation Behavior of The Shot-peened and un-peened Spring Steel (쇼트피이닝재와 언피닝재의 피로균열진전거동 평가)

  • Park, Keyong-Dong;Ryu, Chan-Uk
    • Proceedings of the KSME Conference
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    • 2003.04a
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    • pp.247-254
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    • 2003
  • The lightness of components required in automobile and machinery industry is requiring high strength of components. In particular manufacturing process and new materials development for solving the fatigue fracture problem attendant upon high strength of suspension of automobile are actively advanced. In this paper, the effect of compressive residual stress of spring steel(JISG SUP-9) by shot-peening on fatigue crack growth characteristics in high temperatures($100^{\circ}$, $150^{\circ}$, $180^{\circ}$) was investigated with considering fracture mechanics. So, we can obtain followings. (1)Compressive residual stress decreases in high temperature, that is, with increasing temperature. (2)The effect of compressive residual stress on fatigue crack growth behavior in high temperature increases below ${\Delta}K=17{\sim}19MPa$ (3)It was investigated by SEM that the constraint of compress residual stress for plastic zone of fatigue crack tip was decreased in high temperature as compared with room temperature.

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A Study on the Effect of Compressive Residual Stress on Fatigue Crack Propagation Behavior of the Shot-peened Spring Steel (쇼트피이닝 가공 스프링강의 압축잔류응력이 피로균열 진전거동에 미치는 영향)

  • 박경동
    • Transactions of the Korean Society of Automotive Engineers
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    • v.11 no.4
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    • pp.117-124
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    • 2003
  • The lightness of components required in automobile and machinery industry is requiring high strength of components. In particular, manufacturing process and new materials development for solving the fatigue fracture problem attendant upon high strength of suspension of automobile are actively advanced. In this paper, the effect of compressive residual stress of spring steel(JISG SUP-9) by shot-peening on fatigue crack growth characteristics in high temperatures($100^{\circ}C$, $150^{\circ}C$, $180^{\circ}C$) was investigated with considering fracture mechanics. So, we can obtain followings. (1)Compressive residual stress decreases in high temperature, that is, with increasing temperature. (2)The effect of compressive residual stress on fatigue crack growth behavior in high temperature increases below $\Delta$K=17~19MPa (3)It was investigated by SEM that the constraint of compressive residual stress for plastic zone of fatigue crack tip was decreased in high temperature as compared with room temperature.

Fatigue Characteristic of HIPS(HR-1360) Materials (HIPS(HR-1360) 재료의 피로 특성 평가)

  • Park, Jae-Sil;Seok, Chang-Sung;Lee, Jong-Gyu;Lee, Jae-Hyuk
    • Proceedings of the KSME Conference
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    • 2000.11a
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    • pp.129-134
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    • 2000
  • Recently, HIPS(High Impact Polystyrene) materials are spot-lighted as office equipment, home electronics, electronics appliances housing, packing containers, etc. But its using are occur to problem caused by fatigue fracture. However, its strength is larged affected by environmental conditions. So, in this paper it tried to analyze the effect of temperature by tensile test and fatigue test. It was observed that yield strength and ultimate strength, fatigue life of same stress decreased relatively with increase temperature. Further, this paper predict S-N curve using the result of tensile test and micro vickers hardness test. For this purpose, the management in the engineering department is able to design the fatigue life of HIPS(HR-1360) materials.

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Fatigue Strength Depending on Position of Cracks for Weldments

  • Lee Hae-Woo;Park Won-Jo
    • Journal of Mechanical Science and Technology
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    • v.20 no.5
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    • pp.675-680
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    • 2006
  • This is a study of fatigue strength of weld deposits with transverse cracks in plate up to 50 mm thick. It is concerned with the fatigue properties of welds already with transverse cracks. A previous study of transverse crack occurrence, location and microstructure in accordance with welding conditions was published in the Welding Journal (Lee et al., 1998). A fatigue crack develops as a result of stress concentration and extends with each load cycle until fatigue occurs, or until the cyclic loads are transferred to redundant members. The fatigue performance of a member is more dependent on the localized state of stress than the static strength of the base metal or the weld metal. Fatigue specimens were machined to have transverse cracks located on the surface and inside the specimen. Evaluation of fatigue strength depending on location of transverse cracks was then performed. When transverse cracks were propagated in a quarter-or half-circle shape, the specimen broke at low cycle in the presence of a surface crack. However, when the crack was inside the specimen, it propagated in a circular or elliptical shape and the specimen showed high fatigue strength, enough to reach the fatigue limit within tolerance of design stresses.

A Preliminary Study on Fatigue Strength of High Toughness Thermoplastic Composite Material AS4/PEEK (고인성 열가소성 복합재료 AS4/PEEK의 피로강도에 관한 기초적 검토)

  • Song, Ji-Ho;Gang, Jae-Yun
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.24 no.4 s.175
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    • pp.1055-1064
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    • 2000
  • First, various specimen geometries, namely, coupon type, waisted type and dog-bone type, were examined to determine appropriate fatigue specimen of thermoplastic composite material AS4/PEEK and the n, fatigue strength of smooth and notched specimens of AS4/PEEK [-45/0/+45/90]2s was investigated. Fatigue tests were performed under load controlled condition at a stress ratio of 0. 1 at a frequency of 5Hz. Stiffness degradation of specimens with fatigue cycling was monitored using an automated unloading compliance technique. The waisted type specimen is found appropriate for smooth fatigue specimen geometry of AS4/PEEK. As for the effect of stress concentration, it is found that fatigue strength is higher for a 2mm-diameter hole notched specimen than a 5mm-diameter one. Fatigue notch factor decreases with the increase of fatigue life. These results are far different from the trend of fatigue strength of metallic materials. The stiffness variation of smooth specimen was only 4% at maximum until final fracture. On the other hand, the stiffness of hole notched specimen was reduced by 45% at maximum. Notched fatigue strength was compared between thermoplastic composite AS4/PEEK and thermosetting composite Graphite/Epoxy. In long-life fatigue (>104), the AS4/PEEK composite shows superior fatigue strength, but in short-life fatigue, the fatigue strength of the Graphite/Epoxy composite is nearly equal or somewhat higher than that of the AS4/PEEK composite.

A Study on the Distribution of Internal Inclusions and the Fatigue Strength of Induction Surface Hardened Steel (고주파 표면경화재의 내부개재물의 분포와 피로강도에 관한 연구)

  • Song, Sam-Hong;Choi, Byoung-Ho
    • Proceedings of the KSME Conference
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    • 2000.11a
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    • pp.333-338
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    • 2000
  • Induction surface hardening is widely used to enhance local strength and hardness. However, most research is only to have a focus on fatigue life and fatigue behavior is not so much studied. So, in this study, Cr-Mo steel alloy(SCM440) was used to show the effect of residual stress and micro hole on the fatigue strength for base metal and induction surface hardened specimen. In addition, the fatigue characteristic between surface hardened and fully hardened steel is somewhat different. It is caused by hardness distribution, residual stress and inclusions etc.. Crack origins are generally micro inclusions for the high strength steel. So, the distribution of inclusions is analyzed statistically.

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Strength Evaluation of the Cylinder Liner of Low-Speed Marine Engine (대형 엔진 실린더 라이너의 강도평가)

  • Kim, Byung-Joo;Son, Jung-Ho;Park, Jin-Soo;Choi, Ho-Jung
    • Proceedings of the KSME Conference
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    • 2001.06a
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    • pp.663-668
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    • 2001
  • Strength evaluation was carried out for the cylinder liner of a low-speed marine engine. Calculation of temperature distribution, nonlinear structural analysis, material test, and fatigue strength evaluation are briefly introduced in this paper. Strengths of five liner models are compared, and the effect of materials experiencing different heat treatment is evaluated. Structural analysis including boundary and material non-linearities was performed for axisymmetric liner models. High cycle (fatigue limit) and low cycle (fatigue life) fatigue analyses are carried out. As results, localized high stress was occurred next to the mount line. Maximum stresses are varied significantly with respect to different liner models and different materials.

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High Fatigue Life and Tensile Strength Characteristics of Low Activation Ferritic Steel(JLE-1) by TIG Welding (TIG용접한 저방사화 페라이트강(JLF-1)의 고온강도 및 피로수명특성)

  • Yoon, H.K.;Lee, S.P.;Kim, S.W.;Park, W.J.;Kohyama, A.
    • Proceedings of the KSME Conference
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    • 2001.06a
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    • pp.181-186
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    • 2001
  • JLF-1 steel (Fe-9Cr-2W-V-Ta), low activation ferritic steel, is one of the promising candidate materials fer fusion reactor applications. High temperature fatigue life and tensile strength of JLF-1 steel and its TIG welded joints were investigated at the room temperature and $400^{\circ}C$. The strength of base metal (JLF-1) is in between those of weld metal and the HAZ. When the test temperature was increased from room temperature to $400^{\circ}C$, both strength and ductility decreased for base metal, weld metal and the HAZ. The longitudinal specimens of base metal showed similar strength and ductility compared with those of the transverse specimens at room temperature and $400^{\circ}C$. Little anisotropy was observed in the JLF-1 steel base metal in terms of rolling direction. Fatigue limit of weld metal which was obtained from cross-weld specimen is 495MPa. Thus, the weld metal showed the higher fatigue limit than those of base metal at both room temperature and $400^{\circ}C$. Little anisotropy of fatigue properties was observed for JLF-1 base metal in terms of rolling direction. When the test temperature was increased from room temperature to $400^{\circ}C$, the fatigue limit of both base metal and weld metal decreased substantially.

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A Study on the Fatigue Strength of Highly Skewed Propeller (하이 스큐드 프로펠러의 피로강도에 관한 연구)

  • Kang Nak-Hwoun;Kim Jong-Ho
    • Journal of Advanced Marine Engineering and Technology
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    • v.28 no.7
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    • pp.1131-1137
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    • 2004
  • Recently there has been a remarkable increase in the number of high speed and large ships and the high power involved for propulsion of above ships has brought high pitch ratio and highly skewed propeller. The recent tendency toward highly skewed propeller has increased the load on propeller blades, and the fatigue strength of propeller blades has become the critical point in design of propellers for ships. In this paper the effect of stress ratio and skew angle on the fatigue strength of highly skewed propeller, the statistical inference on the total revolutions of highly skewed propeller for 20 years under normal sea going state. and so on have been discussed. On the basis of above discussions, the highly skewed propeller blade thicknesses by the rules of classification society and the standards of manufacturer in country were compared and reviewed.

High performance silicone for quality assurance of inter-layer joint in apartment house (공동주택 층간조인트 품질확보를 위한 고성능 실리콘 개발)

  • Seo, Tae-Seok
    • Proceedings of the Korean Institute of Building Construction Conference
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    • 2022.11a
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    • pp.201-202
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    • 2022
  • In this study, the high performance silicone was developed to assure the inter-layer joint in apartment house. The tensile strength, the elongation, the bond strength and the fatigue tests were conducted. As a result, it was confirmed that the performance of high -performance silicone was superior to the existing elastic paint. Therefore, it is expected that it will help to secure the quality of inter-layer joints in apartment houses.

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