• Title/Summary/Keyword: Smoke-wire

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과전류 상태에서 고전압이 전선의 위험성에 미치는 영향

  • Baek, Seung-Myeong;Ryu, Gyeong-Hui;Kim, Sang-Hyeon;Kim, Hyeon-Hui
    • Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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    • 2009.11a
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    • pp.235-235
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    • 2009
  • This paper is that study transformation and insulating performance decrease of HIV wire which is using at general electricity structure or home interior wiring of less than AC 600V by over current. When current raised 1A at 1sec, HIV wire insulator is partial charred with white smoke at 86A and conductor of HIV wire is exposed at 90A. When keep time for 5 minutes, insulating performance of the HIV wire decreased rapidly at 45A.

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Properties and Development of Halogen Free Flame Retardant Cable (Halogen Free 난연 케이블의 제특성 및 개발)

  • Choi, W.K.;Choi, W.;Seo, S.J.;Yang, H.J.;Won, J.H.
    • Proceedings of the KIEE Conference
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    • 1992.07b
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    • pp.768-770
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    • 1992
  • Conventional flame retardant cable using PVC or CR materials generate considerable amount of toxic and acidic gas (HCI etc.) together with excessive black smoke during a fire. The newly developed halogen free materials have dissolved the problem of halogen acid gases. This paer describes the development of this power cable insulation and sheath, using halogen free materals.

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Experimental and Computational Investigation of Aerodynamic Characteristics of Hovering Coleoptera

  • Saputra, Saputra;Byun, Do-Young;Yoo, Yong-Hoon;Park, Hoon-Choel;Byun, Yong-Hwan
    • Proceedings of the KSME Conference
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    • 2007.05a
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    • pp.384-388
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    • 2007
  • Aerodynamic characteristics of Coleoptera species of Epilachna quadricollis and Allomyrina dichotoma are experimentally and numerically investigated. Using digital high speed camera and smoke wire technique, we visualized the continuous wing kinematics and the flight motion of free-flying coleoptera. The experimental visualization shows that the elytra flapped concurrently with the main wing both in the downstroke and upstroke motions. The wing motion of Epilachna quadricollis was captured and analyzed frame by frame to identify the kinematics of the wings and to implement it in the movement of a model wing (thin plate) in the simulation. The two-dimensional simulation of Epilachna quadricollis hovering flight was performed by assuming the wing cross section shape as a thin plate, even though most of insect's wings are made of curved corrugated membrane. The effect of Reynolds number are investigated by the simulation. Meanwhile, in order to investigate the role and effect of elytra, the flow visualization of Allomyrina dichotoma was carried on using smoke wire visualization technique. Here, we confirmed that the vortex generated by elytra due to its movement is strongly influence the vortex dynamic generated by hind wings.

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A Transitional Behavior of a Premixed Flame and a Triple Flame in a Lifted Flame(II) (부상화염에서 예혼합화염과 삼지화염의 천이적 거동(II))

  • Jang Jun Young;Kim Tae Kwon
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.29 no.3 s.234
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    • pp.376-383
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    • 2005
  • In the paper we investigate characteristics of a transitional behavior from a premixed flame to a triple flame in a lifted flame according to the change of equivalence ratio. In previous study, we showed that the stabilized laminar lifted flame regime is categorized by regimes of premixed flame, triple flame and critical flame. A gas-chromatograph is used to measure concentration field, a smoke-wire system is used to measure streak line, and a PIV system is used to measure velocity field in lifted flame. In the visualization experiment of smoke wire, the flow divergence and redirection reappeared in premixed flame as well as triple flame. Thus we cannot express the flame front of lifted flame has a behavior of triple flame with only flow divergence and redirection. In PIV measurement, flow velocity for those three flames has minimum value at the tip of flame front. To differentiate triple flame and premixed flame, $\Phi$ value of partially premixed fraction is employed. The partially premixed fraction $\Phi$ was constant in premixed flame. In critical flame small gradient appears over the whole regime. In triple flame, typical diffusion flame shape is obtained as parabolic distribution type due to diffusion flame trailing.

Heat Transfer of a Two-Dimensional Jet Impinging on the Wall with Transverse Repeated Ribs of Square Cross-Section (四角리브를 갖는 傳熱面에 衝突하는 2次元 噴流의 熱傳達에 관한 硏究)

  • 김상필;서정윤
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.11 no.2
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    • pp.214-221
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    • 1987
  • The purpose of this study is augmentation of heat transfer without additional power in the case of rectangular air jet which impinges vertically on the heating surface. The experimental results are obtained heat transfer augmentation of a two-dimensional impinging jet using the surface roughness of transverse repeated-rib type. The integral average heat transfer coefficient of ribbed plate is about two times larger than that of flat plate. In order to supplement the information about the mechanism of heat transfer augmentation, the flow structure in the stagnation region is visually studied by using the smoke wire technique. The heat transfer augmentation is due to the effect of stretching of large scale vortex in the stagnation region.

A Review on Swirling Flow by Using Flow Visualization Techniques in the Circular Tubes (원형관 내에서 유동가시화 기법을 이용한 선회유동에 관한 연구고찰)

  • Chang, Tae-Hyun;Doh, Deog-Hee;Lee, Kwoon-Soo
    • Journal of the Korean Society of Visualization
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    • v.8 no.3
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    • pp.12-21
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    • 2010
  • Swirling flows are found in very wide range of applications, for examples, cyclone separators, spraying machines, heat exchangers and jet pumps, ect. Relatively, little work has been done on the swirl flow using flow visualization techniques. This study deals with many visualization techniques to study on swirling flow. These techniques are related to oil films methods, smoke, dye liquids, liquid crystal, stroboscope light, smoke wire, white light, naphthalene sublimation, LDV(lase doppler Velocimetry) and PIV(particle image velocimetry). The present work has handled single, annular, carved tube, swirl expansion and swirl wake using several visualization methods in the vertical and horizontal circular tube.

The Flow Characteristics around Circular Cylinder of Pressure Interference with Slits (표면압력이 상호 간섭되는 슬릿을 가진 원주의 후류 유동 특성)

  • 부정숙;김진석;류병남
    • Journal of Advanced Marine Engineering and Technology
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    • v.27 no.6
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    • pp.736-744
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    • 2003
  • This study is conducted to investigate aerodynamic forces and wake structures about the pressure interference of a circular cylinder with slits. An experimental investigation of a circular cylinder with slits is carried out in uniform flow in the range of Reynolds number from 8,000 to 32,000 using X-type hot wire. Flow visualization is executed by smoke-wire method to understand the mechanism of these vortex formation process. Inspection in the wake at X/D=5.5 of the cylinder with the slits suggested that a strong vortex-shedding pattern for these cylinders is revealed compare with a circular cylinder without slits. It is found that the rolling up position of shear layer of the cylinder with slits is shorten compare with a circular cylinder without slits.

An Experimental Investigation of Swirl Angle in a Horizontal Round Tube by Flow Visualization Method

  • Tae-Hyun Chang
    • Journal of Advanced Marine Engineering and Technology
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    • v.27 no.7
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    • pp.879-888
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    • 2003
  • Swirling air flow in a horizontal round tube was experimentally studied for its visualization. The present investigation deals with swirl angle, flow visualization studies and accompanying vortex core behavior by using oil smoke and a hot wire anemometer for Re = 40,000 and 50000 at X/D = 41, 59 and 71. In the swirl air flow, a vortex core was formed at high swirl intensity along the test tube. The swirl angle and the vortex core depended on the swirl intensity along the test tube. The results of swirl angles measured by flow visualization and hot wire reasonably agree with those of previous studies.

A study on the safety of the Environment Corrosion of Suspension Insulater of a Catenary Trolley Wire Systems (카테나리 전차선로 현수애자의 환경부식에 따른 안전성 연구)

  • Lee, Jae-Bong;So, Sun-Young
    • Proceedings of the KSR Conference
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    • 2007.05a
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    • pp.864-874
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    • 2007
  • Suspension insulator in Catenary Trolley Wire Systems must have two characteristics, electric insulation and mechanical endurance. Because suspension insulator is used in supporting and insulating position between power supply parts and earth conducted supporting parts. The insulator's electric characteristics can be influenced by surface pollution and damage from the environment such as humidity, dust, smoke, salt. etc. And, the insulating parts can be electrically short. These electrically damaged insulator can cause serious accidents that have far-reaching effect. So appropriate management basis of suspension insulator is needed. And we present appropriate cleaning and the changing period of suspension insulator on the basis of actual data.

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The Study on Changes of Mixing Layer Caused by Acoustic Excitation (음향 여기에 의한 혼합층 유동구조의 변화에 대한 연구)

  • 정양범
    • Journal of Advanced Marine Engineering and Technology
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    • v.24 no.6
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    • pp.120-127
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    • 2000
  • This study is concerned with evaluating the effects of acoustic excitation on the development of two stream mixing layer generated by split plate. The ratios of two velocities U1 and U2 either side of the splitter plate were such that $U_1/U_2$=1.0 (uniform flow) or $U_1/U_2$<1.0(shear flow). The mixing layers were disturbed acoustically through the edge of split plate. Quantitative data were obtained with hot-wire anemometry. Flow visualization with smoke-wire was also employed for qualitative study. the results show that the large scale structures of mixing layers are strongly affected by excitation frequency and amplitude in both uniform and shear flows. The maximum streamwise and vertical turbulent intensities of the excited flow fields are apt to be decreased as compared with those of without excitation. The flow characteristics of uniform flow are more influenced by acoustic excitation than those of shear flow.

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