• Title/Summary/Keyword: Wear Ring

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A Study on the Daesarye Ceremony Participants' Dress Style in the Yeong-Jo Era (영조대(英祖代) 대사례의(大射禮儀) 참여자의 복식 유형 고증)

  • Lee, Eun-Joo;Park, Ga-Young
    • Journal of the Korean Society of Costume
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    • v.57 no.2 s.111
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    • pp.100-114
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    • 2007
  • This study reports the dress style of Daesarye ceremony participants in the Yeong-Jo Era. The King Yeong-jo attending the archery practice ceremony wears Ikseonkwan(翼善冠), Golryongpo(袞龍袍), Okdae(玉帶), and Heukpihwa(黑皮靴) while royal family members and officers in the ceremony wear Heukdalryeong(黑團領). Each officer in Sangbok(常服) who shoots arrows wears a ring and a wristlet with an archery case on his waist. King's bodyguards wear Yungbok(戎服) or Sangbok(常服). Especially, Muyaebyeolgam(武藝別監) wears Hong-geon(紅巾) and a green Jikryeong(直領). Yujiang-gun(儀位軍) wear Pirip(皮笠) and Hongjuryi(紅紬衣) while Hyeopryeongun(狹輦軍) and Hyeopryeogun(狹輦軍) wear Hong-geon(紅巾), Hongyui((紅衣), Cheonghaengjeon(靑行纏), Hakchang(鶴雲), Hongmokdae(紅木帶), and Unhye(雲鞋). Gyeonmabae(牽馬陪) wear Hwangchorip(黃草笠) and Hwangyui(黃衣). Seupjeongun(拾箭軍) and Hwaekja(獲子) wear Jageon(紫巾), Jayui(紫衣), and Unhye(雲鞋). Jeonak(典樂) wears Mora- bokdu and Noksayui(綠抄衣), while Ak-kong(樂工) wear Hwahwabokdu, Hongjuyui(紅紬衣), Ojeongdae, and Heukpihwa(黑皮靴). Lastly, Hyeopryulrang(協律郎) wears Heukdalryeong(黑團領).

Development of Automatic Measuring Device for Cylinder Liner Wear Amount in Large Two Stroke Diesel Engine (대형 저속 디젤 엔진용 실린더 라이너 내면 마모량 자동 측정 장치 개발)

  • Kim, Jang-Kyu;Lee, Min-Cheol
    • Journal of Advanced Marine Engineering and Technology
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    • v.32 no.6
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    • pp.981-988
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    • 2008
  • This paper describes a development of automatic measuring device for cylinder liner wear amount. An operator should regularly measure the wear amount of the cylinder liner to prevent the wear amount of the cylinder liner from exceeding the maximum limit specific to the engine type. In previous methods. an operator entered the inside of the cylinder liner on a ladder and measured the amount of wear using a inside micrometer. Such method is unpleasant in severe environments and full of hazards. In addition, in order to enter the cylinder, the piston head had to be detached. requiring much time and money. In order to solve these problems, a new measuring device that consists of two measuring units and a special install jig is developed. The measuring units are installed through the scavenging air port by the install jig and measures the wear amount during 1 revolution of crankshaft. so detaching of the cylinder head and entering inside the cylinder liner are not required.

Development of Friction Reduction Method between Piston Ring and Cylinder Liner (피스톤 링과 실린더 라이너에서의 마찰저감 기술개발)

  • 김완호;차금환;김대은;임윤철
    • Tribology and Lubricants
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    • v.14 no.4
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    • pp.37-43
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    • 1998
  • The friction loss between piston rings and cylinder liner is due to the tension of the piston rings. Lubricant is usually supplied to reduce the friction. However, the sliding speed of the piston varies during the reciprocating cycle and is very low near TDC(Top Dead Center)/BDC(Bottom Dead Center), where the hydrodynamic lubrication cannot be sustained. Since the lubrication regime is shifted from the hydrodynamic to the boundary lubrication near TDC/BDC, wear particles are easily generated so that the friction loss becomes bigger and bigger due to the plowing effect of wear particles. In this study, for the purpose of reducing the friction loss, an undulated surface is adopted to the cylinder liner to trap wear particles. The friction force variations, which are measured by strain gaged, show that the concept of undulated surface is one of the promising methods to effectively reduce the friction between piston rings and cylinder liner.

Friction Characteristics of the Piston-Ring Assembly Varying Engine Operation Coditions (운전조건변화에 따른 피스톤-링 결합체 마찰특성)

  • 윤정의;김승수
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.18 no.6
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    • pp.1510-1519
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    • 1994
  • It is important to understand the friction characteristics between piston-ring assembly and cylinder wall for the friction loss reduction as well as the solution of problem such as scuffing wear and oil consumption. A new system was developed for the piston-ring assembly friction force measurement. This system was applied to the friction force measurement to find its functional relationship with variables such as engine speed, oil viscosity, and engine load. The friction mean effective pressure(fmep) was found to have a linear relationship with$(\vpsilon{U})^{0.42}$ under motering and with$(\vpsilon{U})^{0.45}$ under firing operations, where $\vpsilon$ is the kinematic oil viscosity and U is mean piston speed.

Critical Speeds Evaluation of Turbo Pump Unit with a Elastic-ring Inserted Ball Bearing (탄성 링을 갖는 볼 베어링 지지의 터보 펌프 임계 속도에 관한 연구)

  • 이용복;김창호;곽현덕;하태웅;우유철
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2001.05a
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    • pp.735-743
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    • 2001
  • This study was performed to evaluate the dynamic behavior of turbo pump unit. The acceptable separate margin of 1st critical speed was obtained by the use of elastic-ring inserted ball bearing, while the poor separate margin of 1$\^$st/ critical speed was appeared in the case without the elastic-ring. In addition, the results show that the stiffness and damping of plain seals gain more separate margin of 2nd critical speed. However the wear or the failure of seals could reduce the 2$\^$nd/ critical speeds near the operating speed.

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Oscillation of Camring and Detachment of Vanes from a Camring in a Variable Displacement Vane Pump (가변 용량형 유압 베인 펌프에서 베인의 이간과 캠링의 진동)

  • 장주섭;양광식;윤영환;이종철;한동철
    • Proceedings of the Korean Society of Tribologists and Lubrication Engineers Conference
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    • 1998.10a
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    • pp.190-195
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    • 1998
  • This paper reports on the theoretical and expetimental study of the vane and cam ring motions in a variable displacement vane pump which is already used widely in various industrial and automotive applications. Dynamic equations of vane and cam ring motion and flow continuity equations are derived and then solved simultaneously using the numerical method. Vane detachment cause the pressure tipples, noise, wear in cam ring, and decrease the volumetric efficiency. Consequently, Vane detachment occurs due to excess compression in the pumping chamber, and it can be reduced by adjustment of design parmeters.

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Efficiency of an SCM415 Alloy Surface Layer Implanted with Nitrogen Ions by Plasma Source Ion Implantation

  • Lyu, Sung-Ki;He, Hui-Bo;Lu, Long;Youn, Il-Joong
    • International Journal of Precision Engineering and Manufacturing
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    • v.7 no.4
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    • pp.47-50
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    • 2006
  • SCM415 alloy was implanted with nitrogen ions using plasma source ion implantation (PSII), at a dose range of $1{\times}10^{17}\;to\;6{\times}10^{17}\;N^+cm^{-2}$ Auger electron spectrometry (AES) was used to investigate the depth profile of the implanted layer. Friction and wear tests were carried out on a block-on-ring wear tester. Scanning electron microscopy (SEM) was used to observe the micro-morphology of the worn surface. The results revealed that after being implanted with nitrogen ions, the frictional coefficient of the surface layer decreased, and the wear resistance increased with the nitrogen dose. The tribological mechanism was mainly adhesive, and the adhesive wear tended to become weaker oxidative wear with the increase in the nitrogen dose. The effects were mainly attributed to the formation of a hard nitride precipitate and a supersaturated solid solution of nitrogen in the surface layer.

Performance Analysis of Mechanical Face Seal Used for Primary Heat Transport Pump in Heavy Water Reactor (중수로 냉각재 펌프용 미케니컬 페이스 실의 성능 해석)

  • Kim, Jeong-Hun;Kim, Dong-Wook;Kim, Kyung-Woong
    • Tribology and Lubricants
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    • v.27 no.5
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    • pp.240-248
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    • 2011
  • Mechanical face seal installed in primary heat transport pump used for heavy water reactor prevents leakage of working fluid using thin working fluid film between primary seal ring and mating ring. If the leakage of working fluid exceeds the allowable volume, serious accident can be happened by the trouble of primary heat transport pump. The thinner fluid film exists between primary seal ring and mating ring, the less working fluid leaks out. On the other hand, if the thickness of fluid film is not enough, the life of mechanical face seal will be reduced by friction and wear. Therefore appropriate design is necessary to maximize the performance and life of mechanical face seal. In this study, numerical analysis using finite volume method was conducted to investigate the performance of mechanical face seals which have same deep straight groove and 11 different net coning values. As results, equilibrium clearance between primary seal ring and mating ring, leakage volume of working fluid, friction torque on sealing surface and stiffness of working fluid film were obtained. With increasing net coning value, equilibrium clearance and leakage volume increase, and friction torque and stiffness of fluid film decrease.

Optimization Design on the Sealing Surface Profiles of Contacting Seal Units (접촉식 시일장치의 밀봉 접촉면 형상에 대한 최적화 설계연구)

  • Kim, Chung-Kyun
    • Journal of the Korean Society of Manufacturing Technology Engineers
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    • v.20 no.6
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    • pp.761-766
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    • 2011
  • In this study, the optimized design profiles between a seal ring and a seal seat of contacting seal units has been proposed based on the FEM computed results. The maximum temperatures, the thermal distortions in axial and radial directions, and maximum contact normal stresses between a seal ring and a seal seat have been analyzed for various contact sealing profiles. The FEM computed results present that the contact area between seal rings and seal seats is very important for a good tribological performance such as low friction heating, low wear, high contact normal stress in a primary sealing components. The seal surface model III in which has a small sealing contact area shows low dilatation of primary sealing components, and high contact stress between a seal ring and a seal seat. This model with small contact surface of a seal ring produces high friction heating and contact stress. But the model III produces very small deformations of contacting sealing surface because of high convection heat transfer by cooling water circulation around the seal ring surface. Thus, the analysis results recommend a short width of a primary sealing unit rather than a big width of contact surfaces of contacting seal units for reducing a leakage and axial deformation of primary seal components.

Measurements of Vibration and Pressure of an Oxidizer Pump for a 7-tonf Turbopump with a Modified Rear Floating Ring Seal (수정된 후방 플로팅 링 실을 적용한 7톤급 터보펌프 산화제 펌프의 진동 및 압력 측정)

  • Bae, JoonHwan;Kwak, Hyun-Duck;Choi, ChangHo;Choi, JongSoo
    • Tribology and Lubricants
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    • v.36 no.5
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    • pp.253-261
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    • 2020
  • In this paper, we present an experimental investigation of the frequency characteristics and a visual inspection of an oxidizer pump with a modified rear-floating ring seal for a 7-tonf turbopump. An oxidizer pump typically operates at high rotational speeds and under cryogenic conditions. Despite its low hydraulic efficiency, the floating ring seal is frequently employed as a leakage control solution for turbomachinery because it effectively reduces abrasion by friction. When the oxidizer pump starts up, the floating ring moves excursively but locks up stably against the pump casing when the contact pressure increases. The compressive force on the floating ring depends on the hydrodynamic forces induced by the flow through the floating ring. This force is controlled by the nose position of the floating ring. Based on a validation test for a 7-tonf turbopump with two types of floating rings, we concluded that the floating ring with a small diameter nose can move easily with a low contact pressure in the cooling path. This leads to instability of the pressure fluctuation around the floating ring. In contrast, a floating ring with a large diameter nose has a high contact pressure and attaches strongly to the casing, which causes wear and frictional oxidation between the contact surfaces of the impeller and the floating ring.