• Title/Summary/Keyword: 미끄럼실험

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Development of Calibration Equation of Portable Slip Meter(ONO·PPSM) through Comparative test of O-Y·PSM and ONO·PPSM (경사인장형 미끄럼시험기(O-Y·PSM)와의 비교실험을 통한 휴대형 미끄럼시험기(ONO·PPSM)의 교정식 작성)

  • Shin, Yoon-Ho;Choi, Soo-Kyung
    • Journal of the Korea Institute of Building Construction
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    • v.9 no.5
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    • pp.155-161
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    • 2009
  • This paper is the result of an investigation of a PORTABLE SLIP METER(ONO PPSM) by means of an experiment to determine its validity as a slip meter. ONO PPSM is a portable slip meter that was designed to address the weak points of PULL SLIP METER(O-Y PSM), which can be used to obtain an accurate measurement of slip resistance, but is very heavy and difficult to operate. To determine the stability of the measurement result of ONO PPSM, we measured the slip resistance against 4 different kind of floor materials. Our findings showed that the coefficient of variability of CSR' is less than 0.05. Furthermore, we verified the relationship between CSR' and CSR. More specifically, by performing the slip test against 7 different kinds of inorganic matter floor materials, we increased the usability of ONO PPSM as a slip meter by suggesting a method of sharing the evaluation index of slip of CSR' and C.S.R.

An Experiment Study on Sideslip Angle Effect of Lambda Wing Configuration (람다 날개 형상의 옆미끄럼각 효과에 대한 실험적 연구)

  • Shim, HoJoon;Park, Seung-O;Oh, Se-Yoon
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.43 no.3
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    • pp.224-231
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    • 2015
  • An experimental study on aerodynamic coefficients of a lambda wing configuration was performed at the low speed wind tunnel of Agency for Defense Development. The main purpose of this study was to investigate the effects of sideslip angle on various aerodynamic coefficients. In the case of $0^{\circ}C$ sideslip angle, nose-up pitching moment rapidly increases at a specific angle of attack. This unstable pitching moment characteristic is referred to as pitch break or pitch up. As the sideslip angle increases, the pitch break is found to be generated at a higher angle of attack. Rolling moment is found to show similar behavior pattern to 'pitch break' style with angle of attack at non-zero sideslip angles. This trend gets severer at greater sideslip angles. Yawing moment also shows substantial variation of the slope and the unstable directional stability with sideslip angles at higher angles of attack. These characteristics of the three moments clearly implies the difficulty of the flight control which requires efficient control augmentation system.

A Comparative Study on Skid Resistance Performance Evaluation Methods for Maintenance of Skid Resistance Pavement (미끄럼방지포장 유지관리를 위한 미끄럼저항 성능평가방법 비교 연구)

  • Hyun-Woo Cho;Sang-Kyun Noh;Bong-Chun Lee;Yoon-Seok Chung
    • Journal of the Korea institute for structural maintenance and inspection
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    • v.27 no.6
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    • pp.79-85
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    • 2023
  • Skid resistance pavement is an accessory to the road and is a facility for the safe driving of cars by increasing the skid resistance of road pavement. In particular, in bad weather conditions such as snow, rain, and black ice, the skid resistance performance of skid resistance pavement greatly affects the safety of road traffic and drivers. However, BPT(British Pendulum Tester) has a test area of only 0.009 m2, making it difficult to represent the overall packaging surface. A reliable method of evaluating slip resistance performance is needed for maintaining non-slip packaging. In this study, the conventional BPT test and the skid resistance performance evaluation method of the PFT(Pavement Friction Tester) and µGT(Micro Grip Tester) tests were compared through guidelines and standard investigations and applied to the field skid resistance performance evaluation. In addition, skid resistance pavement with different skid resistance performance was installed at the test-bed and actual road demonstration sites to compare BPN(British Pendulum Number), SN(Skid Number), GN(Grip Number), and to derive correlations for each performance evaluation method. As a result of the experiment, SN and GN showed similar skid resistance performance, and the GN value was derived similar to BPN × 0.01.

Experiments on Slip Coefficients of High-Strength Bolt Connection with Weathering Steel (I) (내후성강재 고장력볼트 이음부 미끄럼계수 평가 실험 (I))

  • Park, Yong Myung;Seong, Taek Ryong
    • Journal of Korean Society of Steel Construction
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    • v.12 no.2 s.45
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    • pp.167-175
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    • 2000
  • An experimental research to evaluate the slip coefficient of high-strength slip-critical-type bolt connection of weathering steel plate has been performed in this paper. Experiments were performed with several surface conditions such as clean mill scale with hand or power brush cleaning, shot blast cleaned, inorganic zinc primer coated, and weather coated surfaces. Also, the relaxation of bolt clamping force was estimated during 500 hours. It was ascertained from the experiments that slip coefficients are greater than 0.40 in all faying surface conditions except mill scale surface with power brushing. The quantify of relaxation depended on the surface conditions and was $3{\sim}8%$, i.e., less than 10%.

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Experiments on Slip Coefficients of High-Strength Bolt Connection with Weathering Steel (II) (내후성강재 고장력볼트 이음부 미끄럼계수 평가 실험 (II))

  • Park, Yong Myung;Seong, Taek Ryong
    • Journal of Korean Society of Steel Construction
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    • v.12 no.2 s.45
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    • pp.177-185
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    • 2000
  • An experimental research to evaluate the slip coefficients of high-strength friction-type bolt connection of weathering steel plate has been performed in this paper. The test specimens with mill scale or shot blast had been exposed in open air during 3 and 6 months and cleaning of rust surface by hand brushing, power tool brushing and no cleaning was considered. The relaxation of bolt clamping force had also been measured during 600 hours. It was found that slip coefficients increased to the value over 0.6 with exposure except mill scale surface by power tool brushing. The relaxation of bolt tension force in exposed specimens also increased and maximum value reached to about 10%.

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구름 미끄럼 타원 접촉시 피로균열 시작수명 예측

  • 김태완;이상돈;조용주
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2004.05a
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    • pp.117-117
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    • 2004
  • 일반적으로 접촉 피로 마멸은 구름 또는 미끄럼 접촉시 작용하는 반복 응력에 의해 표면과 표면 아래에 균열이 형성되고 성장 및 합체의 과정을 거쳐 표면의 일부가 떨어져 나가는 손상으로 기어나 캠-롤러, 구름 베어링과 같이 구름-미끄럼 접촉상태로 운전하는 기계요소에서 가장 중요하게 고려되어야 할 파손 메커니즘이다. 특히 기어나 구름 베어링 같이 고주기 접촉 피로 특성을 지니는 기계요소의 수명은 피로수명 실험과 통계적 기법을 이용한 Weibull 이론을 기초로 한 수명식을 대부분 사용하고 있다.(중략)

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Wear and Wear transition mechanism in $Al_2O_3$ during sliding) ($Al_2O_3$에서 미끄럼시의 미모 및 마모천이 기구)

  • 한국표준연구소
    • Proceedings of the Korean Society of Tribologists and Lubrication Engineers Conference
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    • 1988.11a
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    • pp.67-74
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    • 1988
  • 고온성질 및 내마모 성질이 우수한 것으로 알려져 있는 요업재료가 아직 그 사용 영역이 크게 확장되지 못하고 있는 이유는 마모문제 때문이다. 종래 엔진재료로써 사용될 수 있을 것으로 크게 기대되어 왔던 사실과는 달리 아직도 성공하지 못하고 있는 것이 좋은 예이다. 이와 같이 요업재료에서의 마모가 중요한 문제로 대두함에 따라 최근 마모를 이해하기 위한 연구들이 실험적으로 또 이론적으로 활발히 진행되어 왔다. 그러나 마모는 접촉표면 및 부표면(subsurface)에서의 탄성 및 소성변형 또 화학적 반응등이 통상 복합적으로 작용하여 나타나는 매우 복잡한 것이기 때문에 아직도 그 기구는 분명하지 않다. 따라서, 요업재료에서 마모가 어떻게 일어나는 지를 밝히는 것은 아직도 매우 중요하다. 본 연구의 목적은 요업재료에서 미끄럼시의 마모기구를 실험적으로 밝히는 것이다. 비교적 제 성질이 잘알려져 있는 $Al_2O_3$를 모델계로 택하여 마모시험을 행하였으며, 미끄럼 시간에 따른 마모양상의 변화 및 접촉표면과 부표면에서의 미세구조 변화를 관찰하여 마모기구를 규명하였다.

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The Experimental Study on Load Transfer Mechanisms in Non-slip Device of Steel Pipe Pile Cap (강관말뚝 머리결합부의 미끄럼 방지턱에 관한 하중전달 메카니즘 연구)

  • Kim, Young-Ho
    • Journal of the Korea institute for structural maintenance and inspection
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    • v.8 no.1
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    • pp.221-229
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    • 2004
  • In Recent experimental research results of connection method between steel pipe pile and concrete footing are provided based on various experimental observations. It gives a shedding light toward developing better connection method for steel pipe pile at the field application. In this study, the newly developed method is tested for compressive, pull put and combination load including moment with carefully designed monitoring system. The measured data show that new method have at least equivalent or better load resistant capacities compared with those of specified method in Korea Road Design Specification. It is also tried to define and investigate the load transfer mechanism for new method.

Test Methods for Evaluation of Slip-Resistance Force of Clamp for Plastic Greenhouse (플라스틱 온실 죔쇠의 미끄럼 저항력 평가를 위한 실험 방법)

  • Choi, Man-Kwon;Song, Ho-Sung;Cho, Myeong-Whan;Yu, In-Ho;Shin, Young-An;Lim, Seong-Yoon;Ryu, Hee-Ryong
    • Journal of Bio-Environment Control
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    • v.25 no.3
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    • pp.193-199
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    • 2016
  • The research discussed experimental results on slip resistance force of rafter-purlin connection of plastic greenhouse and suggested a test method for evaluating slip resistance performance of the connection. Slip resistance forces were measured by four kinds of constraint conditions for specimens, for example, fixing or rolling the end of specimen. According to tests, it is noticed that constraint condition is able to significantly affect the slip resistance force. From a post-hoc comparison result, slip resistance force of test under fixing ends condition was larger than those under the other three constraint conditions. But the slip resistance force results in the fixing ends condition had greater measure of dispersion and three times of standard deviation than those from other constraint conditions. Based on the results obtained, effect of constraint condition for specimen on the slip test should be studied to enhance reliability of evaluation test of the slip resistance performance.

Papers : Effect of Sideslip on the Vortex Flow over a Delta Wing (논문 : 옆미끄럼각이 삼각 날개 와류에 미치는 영향)

  • Son,Myeong-Hwan;Lee,Gi-Yeong;Baek,Seung-Uk
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.30 no.1
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    • pp.1-8
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    • 2002
  • The effects of sideslip on the vortex over a delta wing was investigated experimentallu at a free strean velocity of 40 m/sec, corresponding to a Reynolds number of 1.76$\times$$10^6$, based on the root chord. The angles of attack ranged from $16{^{\circ}}$ to $28{^{\circ}}$, and the sideslip angles treated were $0{^{\circ}}$, $-10{^{\circ}}$, and $-20{^{\circ}}$. It was observed that the sideslip decreased the strengths of the vortices of both windward and leeward sides of the wing, and promoted the vortex breakdown on the windward side. At sideslip angle of $-10{^{\circ}}$, the vortex strength of leeward side was increased as the angle of attack increased. This asymmetric development and breakdown of vortices in sideslip condition would cause an abrubt change of the rolling moment at a high angle of of attack, which could be considered as a rolling moment instability.