• Title/Summary/Keyword: test miner

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Fatigue Life Predictions for Variable Load Histories (변동하중하의 피로수명예측)

  • 하재선;송지호;이시중
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.12 no.4
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    • pp.760-780
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    • 1988
  • Using the fatigue test results obtained in the SAE Fatigue Cumulative Damage Test Program, prediction methods of fatigue crack initiation life for notched members undergoing random loaming histories were discussed in detail. Conventional fatigue life predictions based on so-called modified Miner's rule were found to be apt to give nonconservative estimate, due to lack of sufficient consideration for stress-interaction effect. A modified .epsilon.-N curve concept was proposed to account for the stress-interaction effect. The predicted fatigue life based on the modified .epsilon.-N curve concept was in good agreement with the experimental results of SAE Test Program. Specifically for the cases when fatigue data was not available at hand, was proposed a procedure to give conservative estimate of fatigue life.

Investigation on Structural Design and Impact Damage for a Small Wind Turbine Blade (소형 풍력발전기 블레이드의 구조설계 및 충격손상 안전성 연구)

  • Kong, Changduk;Choi, Suhyun;Park, Hyunbum
    • Journal of Aerospace System Engineering
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    • v.2 no.2
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    • pp.1-7
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    • 2008
  • Recently the wind energy has been alternatively used as a renewable energy resource instead of the mostly used fossil fuel due to its lack and environmental issues. This work is to propose a structural design and analysis procedure for development of the low noise 100W class small wind turbine system which will be applicable to relatively low speed region like Korea and for the domestic use. Structural analysis including load cases, stress, deformation, buckling, vibration and fatigue life was performed using the Finite Element Method, the load spectrum analysis and the Miner rule. In order to evaluate the designed structure, the structural test was carried out and its test results were compared with the estimated results. In addition, the blade should be safe from the impact damage due to FOD(Foreign Object Damage) including the bird strike. In order to analize the bird strike penomena on the blade, MSC. Dytran was used, and the applied method Arbitrary Lagrangian-Eulerian was evalud by comparison with the previous study results.

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Structural Design of Composite Blade and Tower for Small Wind Turbine System

  • Jang, Mingi;Lee, Sanggyu;Park, Gwanmun;Park, Hyunbum
    • International Journal of Aerospace System Engineering
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    • v.2 no.1
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    • pp.38-42
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    • 2015
  • This work is to propose a structural design and analysis procedure for development of the low noise 1kW class small wind turbine system which will be applicable to relatively low speed region like Korea and for the domestic use. The proposed structural configuration has a sandwich composite structure with the E-glass/Epoxy face sheets and the Urethane foam core for lightness, structural stability, low manufacturing cost and easy manufacturing process. Structural analysis including load cases, stress, deformation, buckling, vibration and fatigue life was performed using the Finite Element Method, the load spectrum analysis and Miner rule. In order to evaluate the designed structure, the structural test was carried out and its test results were compared with the estimated results. Moreover Investigation on structural safety of tower was verified through structural analysis by FEM.

An Analysis on Fatigue Fracture of Nuclear Pump Impeller Alloys by Ultrasonic Vibratory Cavitation Erosion (원전 해수 펌프 임펠러 합금의 케비테이션 피로 손상 해석)

  • Hong Sung-Mo;Lee Min-Ku;Kim Gwang-Ho;Rhee Chang-Kyu
    • Journal of the Korean institute of surface engineering
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    • v.39 no.1
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    • pp.35-42
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    • 2006
  • In this study, the fatigue properties on the cavitation damage of the flame quenched 8.8Al-bronze (8.8Al-4.5Ni-4.5Fe-Cu) as well as the current nuclear pump impeller materials (8.8Al-bronze, STS316 and SR50A) has been investigated using an ultrasonic vibratory cavitation test. For this the impact loads of cavitation bubbles generated by ultrasonic vibratory device quantitatively evaluated and simultaneously the cavitation erosion experiments have been carried out. The fatigue analysis on the cavitation damage of the materials has been made from the determined impact load distribution (e.g. impact load, bubble count) and erosion parameters (e.g. incubation period, MDPR). According to Miner's law, the determined exponents b of the F-N relation ($F^b$ N = Constant) at the incubation stage (N: the number of fracture cycle) were 5.62, 4.16, 6.25 and 8.1 for the 8.8Al-bronze, flame quenched one, STS316 and SR50A alloys. respectively. At the steady state period, the exponents b of the F-N' curve (N': the number of cycle required for $1{\mu}m$ increment of MDP) were determined as 6.32, 5, 7.14 and 7.76 for the 8.8Al-bronze, flame quenched one, STS316, and SR50A alloys, respectively.

Probabilistic Estimation of the Structural Integrity of an Electric Car Bogie Frame (전동차 대차 프레임의 확률론적 구조 건전성 평가)

  • Goo, Byeong-Choon;Seo, Jung-Won;Kim, Nam-Po;Kim, Won-Gyung
    • Proceedings of the KSME Conference
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    • 2001.11a
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    • pp.161-165
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    • 2001
  • Bogie frame of the electric car is an important structural member for the support of vehicle loading. In general, more than 25 years' durability is necessary. Much study has been carried out for the prediction of the structural integrity of the bogie frame in experimental and theoretical domains. One of the useful methods is reliability-based approach. The objective of this paper is to estimate the structural integrity of the bogie frame of an electric car, which is under the running test. We used two approachs. In the first approach probabilistic distribution of S-N curve is used. In the second approach, limit state function is used.

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The Development of Corner Membrane for LNG Storage Tank (LNG저장탱크용 코너 멤브레인 개발)

  • Kim, Y.K.;Hong, S.H.;Yoon, I.S.;Oh, B.T.;Seo, H.S.
    • Proceedings of the KSME Conference
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    • 2001.06a
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    • pp.800-805
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    • 2001
  • Both analytical and experimental studies are presented to investigate the strength of the membrane which is designed by Kogas and will be used as a sealing for a LNG tank. Kogas has already developed the Ring-Knot type membrane, but new type had yet to be developed. This paper reports on the results of investigations into this new type of membrane. Various theorical analyses using FEM and experiments are conducted on the basis of RPIS, and it is found that the RPIS is fully satisfied.

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Strength analysis of the driving shift gears for a 67 kW class agricultural tractor according to tire type

  • Baek, Seung Min;Kim, Wan Soo;Kim, Yeon Soo;Baek, Seung Yun;Lee, Nam Gyu;Moon, Seok Pyo;Jeon, Hyeon Ho;Choi, Young Soo;Kim, Taek Jin;Kim, Yong Joo
    • Korean Journal of Agricultural Science
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    • v.47 no.4
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    • pp.1147-1158
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    • 2020
  • The purpose of this study was to measure the engine torque and rotational speed of a 67 kW class agricultural tractor according to tire type during plow tillage and to analyze the gear strength of the driving shift for the tractor. A field test was performed under the condition with a single tire (Test A) and dual tires (Test B) to increase the ground width of the rear tires. A load monitoring system was developed, and the engine torque and rotational speed were measured using controller area network (CAN) communication. The engine torque and rotational speed during plow tillage were calculated as the equivalent torque and speed using Palmgren Miner's rule. As a result, the equivalent torque and speed in Test A and Test B were 181.0 Nm and 1,913 rpm and 206.1 Nm and 2,130 rpm, respectively. As the ground width of the rear tire was increased, the bending stress in Test B was about 9.9 to 10.5% higher than that of the Test A, and the contact stress was about 4.6 to 4.9% higher than that of the Test A. Under all conditions, the safety factor for the bending and contact stress was 1 or more. Thus, the driving shift gears for the dual tire type are considered safe.

Estimation of Fatigue Integrity for Small Aircraft Engine Mount Strut (소형 항공기 엔진 마운트 구조물의 피로 건전성 평가)

  • Lee, Mu-Hyoung;Park, Ill-Kyoung;Kim, Sung-Joon;Ahn, Seok-Min
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.19 no.4
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    • pp.58-66
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    • 2011
  • The estimation of fatigue integrity is very important for aerospace structures such as engine mount strut. The reason is that the fatigue integrity is essential analysis process to establish the structural stability in aerospace field. Therefore, in this paper, the process of fatigue analysis and test was performed for engine mount strut to prove the structural fatigue integrity. First of all, the fatigue load spectrum is constructed by considering the small aircraft operating condition. Fatigue analysis is done for the cluster near the welding zone which may have F.C.L.(fracture critical location). The fatigue life of engine mount strut was estimated by the Miner's rule which is the damage summation method. Finally, Fatigue test is performed to verify the fatigue integrity. The estimation process of fatigue integrity for engine mount strut of small aircraft may help the design.

The Study of Kogas Membrane Performance Test for LNG Storage Tank (Kogas 멤브레인 성능평가에 관한 연구)

  • Kim Y.K.;Hong S.H.;Yoon I.S.;Oh B.T.;Seo H.S.
    • Journal of the Korean Institute of Gas
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    • v.6 no.4 s.18
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    • pp.17-22
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    • 2002
  • LNG demand has been rapidly increasing in Korea for a variety of reasons including stable supply, non-polluting, and high combustion efficiency characteristics. One of the most important structural core element of the LNG storage tank is the membrane, consisting of stainless steel. The membrane to be applied inside of LNG storage tank is provided with corrugations to absorb thermal contraction and expansion caused by LNG temperature. Experimental studies are presented to investigate the deformation and strength of the membrane which is designed by Kogas. All experiments are conducted on the basis of RPIS, and we found the results is fully satisfied with the RPIS.

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Analysis on fatigue life distribution of composite materials (복합재료 피로 수명 분포에 관한 고찰)

  • 황운봉;한경섭
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.12 no.4
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    • pp.790-805
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    • 1988
  • Static strength and fatigue life scattering of glass fiber reinforced epoxy composite materials has been studied. Normal, lognormal, two-parameter and three-parameter Weibull distribution functions are used for strength and one-stress fatigue life distribution. The value of mean fatigue life is analysed using mean fatigue life, mean log fatigue life and expected value of 2 and 3-parameter Weibull distribution functions. Modification on non-statistical cumulative damage models is made in order to interpret the result of two-stress level fatigue life scattering. The comparison results show that 3-parameter Weibull distribution has better predictions in static strength and one-stress level fatigue life distributions. However, no advantage of 3-parameter Weibll distribution is found over 2-parameter Weibull distribution in two-stress level fatigue life predictions. It is found that two-stress level fatigue life prediction by the expanded equal rank assumption is close to the experimental data.