• Title/Summary/Keyword: Failure factors

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Clinical Study on Acute Renal Failure after Valve Replacement Surgery (인공판막치환술후 발생한 급성신부전에 대한 임상적 고찰)

  • 신현종
    • Journal of Chest Surgery
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    • v.27 no.2
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    • pp.122-127
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    • 1994
  • A retrospective study of 737 consecutive patients surviving the first 24 hours who underwent valve replacement surgery from July 1980 to June 1993 was undertaken to determine the prevalence, variables that could be used to predict outcome and results of therapy for postoperative acute renal failure[ARF]. Twenty-one patients[2.8 %] developed acute renal failure. Positive risk factors noted in the development of postoperative renal failure included age, New York Heart Association class III & IV, endocarditis and elevated preoperative concentration of serum creatinine. The duration of cardiopulmonary bypass, aortic cross-clamping and the total duration of the operation also closely correlated with the incidence of ARF. The mortality rate for established ARF was 38.1% and ARF was associated with a significant increase in the length of hospitalization, ventilator support and intensive care unit stay. The incidence and mortality rate of oliguric renal failure was 38.1% and 85.7%. The highest mortality rate was associated with two or more postoperative complications and serum creatinine value exceeded 5 mg/dl. We concluded that therapy should be aimed at prevention of oliguric renal failure, or at least its conversion to nonoliguric renal failure, and early institution of renal replacement therapy with intensive support probably gives the best chance for survival.

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A Study on Rainfall Induced Slope Failures: Implications for Various Steep Slope Inclinations

  • Do, Xuan Khanh;Jung, Kwansue;Lee, Giha;Regmi, Ram Krishna
    • Journal of the Korean GEO-environmental Society
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    • v.17 no.5
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    • pp.5-16
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    • 2016
  • A rainfall induced slope failure is a common natural hazard in mountainous areas worldwide. Sudden and rapid failures which have a high possibility of occurrence in a steep slope are always the most dangerous due to their suddenness and high velocities. Based on a series of experiments this study aimed to determine a critical angle which could be considered as an approximate threshold for a sudden failure. The experiments were performed using 0.42 mm mean grain size sand in a 200 cm long, 60 cm wide and 50 cm deep rectangular flume. A numerical model was created by integrating a 2D seepage flow model and a 2D slope stability analysis model to predict the failure surface and the time of occurrence. The results showed that, the failure mode for the entire material will be sudden for slopes greater than $67^{\circ}$; in contrast the failure mode becomes retrogressive. There is no clear link between the degree of saturation and the mode of failure. The simulation results in considering matric suction showed good matching with the results obtained from experiment. A subsequent discarding of the matric suction effect in calculating safety factors will result in a deeper predicted failure surface and an incorrect predicted time of occurrence.

Comparative analysis of caisson sections of composite breakwaters evaluated by Level I reliability-based design method (Level I 신뢰성 기반 설계법에 의해 산정된 혼성제 케이슨 단면의 비교 분석)

  • Lee, Cheol-Eung;Park, Dong Heon;Kim, Sang Ug
    • Journal of Korea Water Resources Association
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    • v.51 no.7
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    • pp.543-554
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    • 2018
  • A methodology has been presented for evaluating the partial safety factors on the sliding failure mode of vertical caissons of composite breakwaters and for determining the cross sections of those by Level I reliability-based design method. Especially, a mathematical model has been suggested for the sake of a consistency of code format as well as convenience of application in practical design, for which the uncertainties associated with buoyancy and its own weight can be taken into account straightforwardly. Furthermore, design criteria equation has been derived by considering accurately the effect of uplift pressure, so that the cross sections of caissons can be assessed which must be safe against the sliding failure. It has been found that cross sections estimated from partial safety factors proposed in this paper are in very good agreement with the results of Level II AFDA and Level III MCS under the same target probability of failure. However, partial safety factors of the Technical Standards and Commentaries for Port and Harbour Facilities in Japan and Coastal Engineering Manual in USA tend to estimate much bigger or smaller cross sections in comparison to the present results. Finally, many reliability re-analyses have been performed in order to conform whether the stability level of cross section estimated by Level I reliability-based design method is satisfied with the target probability of failure of partial safety factors or not.

Slops Stability Analysis of Carsington Dam (Carsington 댐의 사면안정 해석)

  • 손준익;안상로
    • Proceedings of the Korean Geotechical Society Conference
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    • 1991.10a
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    • pp.75-86
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    • 1991
  • In this paper the failure of Carsington Dam was discussed based on the informations reported in the first edition of Korean Geotechnical Society News. The causes of dam failure and its influences were evaluated based on the results of the slope stability analysis. The effects of the shear strain pre-existing in the yellow clay disclosed by the post-failure site investigation and the progressive nature of the dam failure were preponderantly evaluated. Stability analysis was performed based on the proposed values of strength parameters characterizing possible field ground conditions at failure. The calculated safety factors were evaluated for different cases of strength parameters in order to find the most probable field ground condition at the dam failue.

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Structural safety factor for small unmanned aircraft (소형 무인기 구조 안전계수)

  • Kim, Sung-Joon;Lee, Seung-gyu;Kim, Tae-Uk
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.25 no.2
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    • pp.12-17
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    • 2017
  • Manned aircraft structural design is based on structural safety factor of 1.5, and this safety factor is equivalent to a probability of failure of between 10-2 and 10-3. The target failure probability of FARs is between 10-6 and 10-9 per flight according to aircraft type. NATO released STANAG 4703 to established the airworthiness requirements for small UAV which is less than 150kg. STANAG 4703 requires the Target Level of Safety according to MTOW. The requirements of failure probability for small UAV is between 10-4 and 10-5. In this paper, requirements of airworthiness certification for small UAV were investigated and the relationship of safety factors to the probability of structural failure is analyzed to reduce measure of safety factor and structural weight of unmanned aircraft.

Optimal Maintenance Scheduling in a Two Identical Component Parallel Redundant System Subject to Exponential Power Hazards

  • El-Damcese, M.A.;Helmy, A.N.
    • International Journal of Reliability and Applications
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    • v.9 no.2
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    • pp.141-152
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    • 2008
  • This paper presents equations, which can be used to evaluate the failure frequency and the failure rate of a two identical component parallel redundant system in which each component can operate in its wear out period, and the failure rate of each component is exponential power distribution. The optimum maintenance interval for a two identical component parallel redundant system can be obtained using these equations. The proposed approach is presented and illustrated using several numerical examples. The optimum maintenance interval for each component in a two identical parallel redundant system will depend on factors such as: failure rate, repair and maintenance times of each component in the parallel redundant systems.

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An Exploratory Study for the Telecommunications Service Failure Cases in South Korea (정보통신 서비스의 실패 요인: 한국의 텔레콤 서비스시장에서의 실패사례연구)

  • 안재현;권재원;김명수;이동주;이상윤;한상필
    • Journal of the Korean Operations Research and Management Science Society
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    • v.27 no.3
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    • pp.115-133
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    • 2002
  • In this paper, 15 South Korean telecommunications service failure cases were analyzed. Through the in-depth case study, 8 factors were found to be the major causes contributing to the telecommunications service failure. They were (1) ineffective marketing, (2) poor demand forecasting due to misjudgment of customer preference, (3) failure to satisfy technical specifications, (4) loss of cost advantage due to the price cut of competing services or new entry with lower price, (5) loss of utility advantage due to the increased utility of competing services or new entry with higher utility (6) decrease of market attractiveness due to change of customer preference, (7) impact of government policy, and (8) insufficient or low quality of contents. Additional analysis was done to derive managerial implications to the new telecommunications service development strategy. The findings from the paper will provide valuable Insight to the successful Implementation of new service development and service provisioning processes.

A Study on the Reliability and Maintainability Analysis Process for Aircraft Hydraulic System (항공기용 유압 시스템 신뢰도 및 정비도 분석 프로세스 고찰)

  • Han, ChangHwan;Kim, KeunBae
    • Journal of the Korean Society of Systems Engineering
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    • v.12 no.1
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    • pp.105-112
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    • 2016
  • An aircraft must be designed to minimize system failure rate for obtaining the aircraft safety, because the aircraft system failure causes a fatal accident. The safety of the aircraft system can be predicted by analyzing availability, reliability, and maintainability of the system. In this study, the reliability and the maintainability of the hydraulic system are analysed except the availability, and therefore the reliability and the maintainability analysis process and the results are presented for a helicopter hydraulic system. For prediction of the system reliability, the failure rate model presented in MIL-HDBK-217F is used, and MTBF is calculated by using the Part Stress Analysis Prediction and quality/temperature/environmental factors described in NPRD-95 and MIL-HDBK-338B. The maintainability is predicted by FMECA(Failure Mode, Effect & Criticality Analysis) based on MIL-STD-1629A.

A Study on The Sliding Failure Analysis of Embankment Slope in Soft Ground Area Under Construction (시공중인 연약지반 성토부 활동파괴의 원인분석에 관한 연구)

  • Chun, Byung-Sik;Kim, Il-Hwan;Lee, Young-Sub;Jung, Hyuk-Sang
    • Proceedings of the Korean Geotechical Society Conference
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    • 2008.03a
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    • pp.1036-1041
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    • 2008
  • In order to analysis the reason of sliding failure in embankment slope under construction in soft soil area, a model section located in Gimhae Region in Gyeongsangnam-Do, where the sliding failure had been occurred during embankment works in soft soil area, had been selected. This area had been firstly treated with the Pack Drain Method, and additional embankment works of 9.7 meters out of total 14 meters in thickness had been under construction. The results of analysis showed that the reason of sliding failure were overspeed in embankment construction and the overestimation of design factors in calculating strength of each layer of embankment and poor management and inaccuracy reading of measurement devices.

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Influence of Joint Spacing to Rock Slope Stability (절리 간격이 암반 사면의 안정성에 미치는 영향)

  • 윤운상;권혁신;김정환
    • Proceedings of the Korean Geotechical Society Conference
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    • 2000.11a
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    • pp.511-518
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    • 2000
  • Characteristics of joint orientation, length, spacing and their distribution are very important factors for slope stability, Especially, the effect of joint spacing is an essential factor of slope stability. This study is to analyze the effect of joint spacing in cases of sliding and toppling, which is a typical failure mode. Joint spacing can divided into vertical spacing(spacing) and horizontal spacing(gap). And then, the spacing/length ratio of joint directly affect rock slope failure. When the ratio is below 0.05, the possibility of failure is rapidly increased. In case of toppling, the possibility of failure depends on the ratio of spacing to height of slope ratio slope. As the ratio decreases, the possibility of toppling failure increased. The critical ratio of spacing to height of slope is determined by the dip angle of the slope and the orientation of joint sets.

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