• Title/Summary/Keyword: 피로파괴

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A Study on the Elastic Plastic Fracture Analysis for Carbon Steel with a Fatigue Crack (탄소강의 피로균열에 대한 탄소성파괴 해석에 관한 연구)

  • Lee, Jong-Hyung;Jeong, Hyung-Sik;Yoo, Duck-Sang;Kim, Young-Moon
    • Journal of the Korean Society of Industry Convergence
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    • v.9 no.2
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    • pp.117-122
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    • 2006
  • This paper is to provide some of the analysis procedures of the FAD(Failure Assessment Diagram), which is applied th the safety test of the atomic pressure vessels and other structures. Harrison proposed R-6 Diagram, and Bloom developed the method of DPFAD(Deformation Plasticty Failure Assessment Diagram). Analysis of J-integration of the plastic materials give the failure test curve for the materials with serious work hardening effect. J value was obtained form both FEM(Finite Element Mothod) and the experiment using compact type specimen for J=JIC, and the results were compared. In this study, the results of analysis using DPFAD and the factors affecting DPFAD in Static fatigue and fracture were reviewed. It was shown that the concept of DPFAD can be applied to test the safety of the structures.

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Peculiar Fatigue Fracture Behavior of Ultrasonic Nanocrystal Surface Modified SCM435 (초음파 나노 결정 표면개질된 SCM435의 특이한 피로 파괴 특성)

  • Kim, Jae-Hoon;Yun, Seo-Hyun;Nam, Ki-Woo
    • Journal of the Korean Society of Industry Convergence
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    • v.25 no.2_2
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    • pp.239-245
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    • 2022
  • Using the fatigue limit (∆σunsm) and residual stress (σr) of the UNSM smooth specimen, the harmless maximum crack depth (ahlm) according to the crack aspect ratio (As) was evaluated. In addition, the relationship between the minimum crack depth (aNDI1, aNDI2) detectable by non-destructive inspection(NDI), the crack depth (a25, a50) that reduces the fatigue limit by 25% and 50%, and ahlm were evaluated. The harmless crack condition was determined by the deepest crack point (point A). Since ahlm is larger than a25 and a50, a25 and a50 can secure the safety and reliability of steel via UNSM. Because aNDI1 and aNDI2 are larger than a25 and a50, cracks in a25 and a50 cannot be detected by non-destructive testing. Therefore it is necessary to apply more precise NDI.

Methodology for Developing HMA Mix Design Taking into Account Performance-Related Mechanistic Properties (포장성능관련 역학적 특성이 고려된 아스팔트 혼합물의 배합설계법 개발 방안)

  • Kim Boo-Il;Lee Moon-Sup;Kim Kwang-Woo
    • International Journal of Highway Engineering
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    • v.8 no.1 s.27
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    • pp.15-23
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    • 2006
  • Criteria of the current asphalt mix design, Marshall method, includes the stability and flow which are not related with field performance of HMA mixture, together with the air void, Void filled with asphalt (VFA) and/or Void of mineral Aggregate(VMA). In addition, the limits of stability and flow are satisfied in most cases, the Optimum asphalt content (OAC) is determined based on volumetric properties, such as the air void and/or VFA and/of VMA. Therefore, many researchers have sought mechanistic properties which can replace the stability and flow, making the designed mixture having potential for better field performance. This study initiated to develope a mix design by introducing two performance-related mechanistic properties, the deformation strengh and fracture energy, in place of the stability and flow of the Marshall method. The deformation strength $(S_D)$ from the Kim Test has a high correlation with rutting property and the fracture energy(FE) from the indirect tensile test represents the fatigue cracking property of asphalt mixture. Four types of asphalt mixture were prepared for examining possibility of using the suggested mix design method in comparison with current methods. The results showed that mechanical properties were reflected in determination of OAC with this suggested mix design, unlike the existing Marshall method.

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Damage Characteristics of Rocks by Uniaxial Compression and Cyclic Loading-Unloading Test (일축압축시험과 반복재하시험을 이용한 암석의 손상특성 분석)

  • Jeong, Gyn-Young;Jang, Hyun-Sic;Jang, Bo-An
    • The Journal of Engineering Geology
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    • v.31 no.2
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    • pp.149-163
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    • 2021
  • Damage characteristics of granite, marble and sandstone whose properties were different were investigated by uniaxial compression test and cyclic loading-unloading test. Strength, elastic constants and damage threshold stresses were measured by uniaxial compression test and were compared with those measured by cyclic loading-unloading test. Average rock strengths measured by cyclic loading-unloading test were either lower than or similar with those measured by uniaxial compression test. Rocks with high strength and low porosity were more sensitive to fatigue than that with low strength and high porosity. Although permanent strains caused by cyclic loading-unloading were different according to rock types, they could be good indicators representing damage characteristics of rock. Damage threshold stress of granite and marble might be measured from stress-permanent strain curves. Acoustic emissions were measured during both tests and felicity ratios which represented damage characteristics of rocks were calculated. Felicity ratio of sandstone which was weak in strength and highly porous could not be calculated because of very few measurements of acoustic emissions. On the other hand, damage threshold could be predicted from felicity ratios of granite and marble which were brittle and low in porosity. The deformation behaviors and damage characteristics of rock mass could be investigated if additional tests for various rock types were performed.

Management of Non-pain Symptoms in Terminally Ill Cancer Patients: Based on National Comprehensive Cancer Network Guidelines (말기암환자에서 통증 외 증상의 관리: 최신 NCCN(National Comprehensive Cancer Netweork) 권고안을 중심으로)

  • Lee, Hye Ran
    • Journal of Hospice and Palliative Care
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    • v.16 no.4
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    • pp.205-215
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    • 2013
  • Most terminally ill cancer patients experience various physical and psychological symptoms during their illness. In addition to pain, they commonly suffer from fatigue, anorexia-cachexia syndrome, nausea, vomiting and dyspnea. In this paper, I reviewed some of the common non-pain symptoms in terminally ill cancer patients, based on the National Comprehensive Cancer Network (NCCN) guidelines to better understand and treat cancer patients. Cancer-related fatigue (CRF) is a common symptom in terminally ill cancer patients. There are reversible causes of fatigue, which include anemia, sleep disturbance, malnutrition, pain, depression and anxiety, medical comorbidities, hyperthyroidism and hypogonadism. Energy conservation and education are recommended as central management for CRF. Corticosteroid and psychostimulants can be used as well. The anorexia and cachexia syndrome has reversible causes and should be managed. It includes stomatitis, constipation and uncontrolled severe symptoms such as pain or dyspnea, delirium, nausea/vomiting, depression and gastroparesis. To manage the syndrome, it is important to provide emotional support and inform the patient and family of the natural history of the disease. Megesteol acetate, dronabinol and corticosteroid can be helpful. Nausea and vomiting will occur by potentially reversible causes including drug consumption, uremia, infection, anxiety, constipation, gastric irritation and proximal gastrointestinal obstruction. Metoclopramide, haloperidol, olanzapine and ondansetron can be used to manage nausea and vomiting. Dyspnea is common even in terminally ill cancer patients without lung disease. Opioids are effective for symptomatic management of dyspnea. To improve the quality of life for terminally ill cancer patients, we should try to ameliorate these symptoms by paying more attention to patients and understanding of management principles.

A Study on the Cause and Improvement of Crack in the Installing Structure of the Bulkhead of Aircraft (항공기 Bulkhead 체결구조의 균열 원인 및 개선에 관한 연구)

  • Choi, Hyoung Jun;Park, Sung Jae
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.21 no.6
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    • pp.448-454
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    • 2020
  • This study aims to determine the cause of structural defects occurring during aircraft operations and to verify the structural integrity of the improved features. The fracture plane was analyzed to verify the characteristics of the cracks and the fatigue failure leading to the final fracture was determined by the progress of the cracks by the repeated load. During aircraft operations, the comparative analysis of the load measurement data at the cracks with the aircraft design load determined that the measured load was not at the level of 30% of the design to be capable of being damaged. A gap analysis resulted in a significant stress of approximately 32 ksi at the crack site. Pre-Load testing also confirmed that the M.S. was reduced by more than 50% from +0.71 to +0.43, resulting in a sharp increase in aircraft load and the possibility of cracking when combined. Thus, structural reinforcement and the removal of the gap for aircraft cracking sites improved the defect. Based on the structural strength analysis of the improvement features, the bulkhead has a margin of about +0.88 and the fitting feature is about +0.48 versus allowable stress. In addition, the life analysis results revealed an improvement of approximately 84000 hours.

Reliability study on rolling deformation of ITO thin film on flexible substrate (유연 기판상 ITO 박막의 롤링변형에 따른 신뢰성 연구)

  • Seol, Jae-Geun;Lee, Dong-Jun;Kim, Tae-Wook;Kim, Byoung-Joon
    • Journal of the Microelectronics and Packaging Society
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    • v.25 no.1
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    • pp.29-33
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    • 2018
  • Flexible electronics must be stable under various deformations such as bending, folding, and rolling. The reliability of ITO (Indium Tin Oxide) film used widely as a transparent electrode for flexible electronics has been studied using rolling fatigue test and bending test. During repeated rolling deformations, the electrical resistance was in-situ measured with different number of rotation. During rolling fatigue test, the electrical resistance of ITO film was significantly increased with increasing the number of rotation. As the stress state of ITO film is different according to the relative position of ITO and substrate, the rolling fatigue test was investigated under both outer and inner bending conditions. Inner rolling fatigue test showed superior electrical stability because the crack nucleation and propagation were retarded under compressive stress state.

Experimental Evaluation for Static Performance of I-Beam Concrete Slab System (I 형강 합성바닥판의 정적성능 평가)

  • 정영수;박창규;김용곤;이원표
    • Journal of the Korea Concrete Institute
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    • v.13 no.5
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    • pp.430-437
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    • 2001
  • Recently, there have been increased much concerns about repair and rehabilitation works for aged concrete structures. It is in particular known that due to repeated overburden vehicles, there are significantly increasing number of aged concrete bridge slabs, which are strongly needed to construct and rehabilitate by innovative construction method. The objective of this research is to develop the new construction method of concrete slab in bridge superstructure, which can contribute to minimize a traffic congestion during repair and rehabilitation works of aged concrete slab, and can sufficiently assure the quality through the minimization of in-situ works at the site. I-beams with punch holes, which are substituted instead of main reinforcing steels in concrete slabs, can be manufactured in accordance with the specification in the factory, and be preassembled into the panel. After erecting the preassembled panels in the site, concrete will be poured into the slab panel. This research is to investigate mechanical properties of I-beam with punch holes itself, and then to investigate structural properties of assembled I-beam panels through static test, of which result can be utilized for the development of the new constructional method for concrete slab in bridge superstructure.

The Vibration Effect by Induced Pulsation Pressure to the Fatigue Crack of the Dampener Fitting Welding Zone (항공기용 유압 펌프의 맥동 압력에 의한 감쇄기 용접부위 균열 개선 연구)

  • Shin, Jae Hyuk;Kim, Tae Hwan;Kang, Gu Heon;Ha, Do Jun
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.18 no.7
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    • pp.677-687
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    • 2017
  • Aircraft can often be exposed to a variety of environments and vibrations such as engine, hydraulic pump, aerodynamic force. These may cause cracking and destruction of the mechanical structure and sub-components by high-cycle fatigue. The axial piston type pump which is usually applied to the aircraft hydraulic pump can be necessarily accompanied by the fluid pulsation by continuous rotation of the axial piston. The fatigue crack was identified at the dampener fitting welding zone to prevent vibration damping during the running of aircraft equipped with this type of pulsation hydraulic pump. In order to understand the root cause of this matter, fracture and component analyses were carried out and also integral type dampener fitting was applied to prevent recurrence of the crack as a subject of design improvements. Structural integrity stress analysis, fatigue analysis, qualification test and aircraft system equipped test was conducted to verify the design validity in application to integral type dampener fitting. The test results were sufficiently satisfactory with the demand lifetime of the material from the various types of test as conducted and the subject of design improvement in this study could be objectively evaluated that shall be applied to the operational aircraft.

Flexible Durability of Ultra-Thin FPCB (초박형 FPCB의 유연 내구성 연구)

  • Jung, Hoon-Sun;Eun, Kyoungtae;Lee, Eun-Kyung;Jung, Ki-Young;Choi, Sung-Hoon;Choa, Sung-Hoon
    • Journal of the Microelectronics and Packaging Society
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    • v.21 no.4
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    • pp.69-76
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    • 2014
  • In this study, we developed an ultra-thin flexible printed circuit board(FPCB) using the sputtered flexible copper clad laminate. In order to enhance the adhesion between copper and polyimide substrate, a NiMoNb addition layer was applied. The mechanical durability and flexibility of the ultra-thin FPCB were characterized by stretching, twisting, bending fatigue test, and peel test. The stretching test reveals that the ultra-thin FPCB can be stretched up to 7% without failure. The twisting test shows that the ultra-thin FPCB can withstand an angle of up to $120^{\circ}$. In addition, the bending fatigue test shows that the FPCB can withstand 10,000 bending cycles. Numerical analysis of the stress and strain during stretching indicates the strain and the maximum von Mises stress of the ultra-thin FPCB are comparable to those of the conventional FPCB. Even though the ultra-thin FPCB shows slightly lower durability than the conventional FPCB, the ultra-thin FPCB has enough durability and robustness to apply in industry.