• 제목/요약/키워드: seal ring

검색결과 113건 처리시간 0.025초

수차용 봉수장치의 마찰.마모특성에 관한 실험적 연구 (Experimental Study on the Friction and Wear Characteristics of Contact Sealing Unit for a Water Turbine)

  • 김청균;신인철;임광현
    • 한국신재생에너지학회:학술대회논문집
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    • 한국신재생에너지학회 2006년도 추계학술대회
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    • pp.515-518
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    • 2006
  • This paper presents the friction and wear characteristics of contact type sealing unit for a water turbine of a small hydro-power generation, which Is to stop a leakage of a circulating water from a outside of an impeller to an inside of a rolling bearing. The surface wear strongly affect to the seal life of a mechanical face seal. In this study, the hardness of a stainless steel in which is a heat-treated is 892.8 in Vickers hardness and the hardness of silicone carbide of SiC is 714.1 in Vickers hardness. The surface hardness of a heat-treated stainless steel is 25% high compared with that of a ceramic material of SiC. The contact modes of rubbing surfaces aye a dry friction a water film friction and a mixed friction that is contaminated by a dust, silt and moistures, etc. These two factors of a contact rubbing modes and a material property are very important parameters on the tribological performance such as a friction and wear between a seal ring and a seal seat. The experimental result shows that the surface hardness of a seal material is very important on the friction coefficient and a wear volume. Thus, the results recommend higher hardness of a seal material, which may reduce a friction loss and increase a wear life of primary seal components

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7톤급 터보펌프 기계평면실의 성능 시험 연구 (Study on the Mechanical Face Seal Performance for a 7-ton-Class Turbopump)

  • 배준환;곽현덕;최창호
    • Tribology and Lubricants
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    • 제32권5호
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    • pp.154-159
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    • 2016
  • This paper presents an experimental study of the leakage performance and endurance performance of a mechanical face seal in the 7-ton-class turbopump of the Korea Space Launch Vehicle 2 third-stage engine. We install a mechanical face seal between the fuel pump and turbine to prevent the mixing of the fuel and turbine gas. We design and manufacture a prototype mechanical face seal, which has two parts, namely, a bellows seal assembly and mating ring. We set up a test facility to measure the leakage and endurance of the mechanical face seal. For the similarity tests, we use water under real operating conditions such as high rotational speed, high temperature, and high pressure. Through investigation of the leakage and carbon wear rate, it is possible to evaluate the performance of the mechanical face seal. The results of the leakage and endurance performance test demonstrate the absence of any leakage from the prototype mechanical face seal after a trial run and clarify that the acceptable wear rate fully satisfies the turbopump requirements. Finally, we install a qualified mechanical face seal in a 7-ton-class turbopump and perform a validation test in the turbopump real-propellant test facility in the Korea Aerospace Research Institute. The test results confirm that the mechanical face seal works well under real operating conditions.

베어링 용 고무시일의 접촉력에 관한 실험적 연구 (Experimental Study on the Contact Force of Rubber Seals for a Ball Bearing)

  • 전인기;심우전;최인혁;김청균
    • Tribology and Lubricants
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    • 제9권1호
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    • pp.32-37
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    • 1993
  • The equations are derived for the evaluation of the axial contact forces. The contact forces of rubber seals are analyzed as a function of the ratio of real contact length, the thickness of seal lip, the inclined angle of seal lip, and the interference between the edge of seal lip and the rotating inner ring. The experimental apparatus is developed for the test of seal lip contact force. The data for designing rubber seals are presented in terms of the ratio of real contact length, initial inclined lip angle, lip thickness. and the interference. The results obtained from the derived equation for the contact force are in good agreement with the experimental results.

KSLV-I 킥모터 플렉시블 씰 수압 구동 시험 (The hydrostatic actuation test on flexible seal of KSLV-I Kick Motor)

  • 김병훈;권태훈;조인현
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2009년도 제33회 추계학술대회논문집
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    • pp.153-156
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    • 2009
  • KSLV-I 2단에 적용된 킥모터는 피치, 요축 자세제어를 위해 고무와 보강제가 번갈아가며 적층된 플렉시블 씰을 사용하였다. 제작된 플렉시블 씰은 노즐에 조립되기 전에 플렉시블 씰의 성능을 확인하기 수압 구동 시험을 수행 하였다. 수압 시험을 통해 플렉시블 씰의 제작 상태를 확인하였으며, 압력 변화에 따른 피치, 요축의 구동 토크 및 축 방향 밀림량을 확인하였다. 수압 시험결과 제작된 플렉시블 씰의 구동 토크는 60kgf-m/deg이하이며, 축 방향 밀림량은 최대 6mm이하를 보이고 있다.

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기계평면시일에서 온도전파를 위한 파속도의 이론적해석 (ANALYSIS OF WAVE VELOCITY FOR TEMPERATURE PROPERGATION IN A MECHANICAL FACE SEAL)

  • 김청균
    • 한국윤활학회:학술대회논문집
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    • 한국윤활학회 1987년도 제5회 학술강연회초록집
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    • pp.50-56
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    • 1987
  • A mechanical face seal is most commonly used to seal liquids and gases at various speeds, pressures and temperatures. The primary seal ring is in sliding contact with the seal seat and as a result heat in the vicinity of the interface is generated. Local temperatures at points along the circumferential direction will fluctuate as asperities on the surfaces pass. This kind of fluctuation of temperature has been investigated to take place. This may lead to the hot spots phenomenon between the contacting asperities. Sibley and Allen showed photographic evidence of systemically moving hot spots in the contact zone. The appearance of such a temperature disturbance has been attributed to a kind of thermoelastic instabilities between two surfaces: This involves a feedback loop which comprises localized elevation of frictional heating, resultant localized thermal bulding, localized pressure increase as the result of the bulging and futher elevation of frictional heating as the result of the pressure increase. The heating of hot spots will be continued until the expanded material due to the frictional heating is worn off. Therefore to predict the speed of temperature propagation into the body is essential to the analysis of heat transfer on the edge of the seal.

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복합소재 O-링 접합계면의 단열특성에 관한 컴퓨터 시뮬레이션 (Computer Simulation on Insulation Characteristics of Composite Material O-rings)

  • 김청균;김성원;조승현
    • 한국윤활학회:학술대회논문집
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    • 한국윤활학회 2002년도 제35회 춘계학술대회
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    • pp.291-295
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    • 2002
  • O-ring seal is usual component part in various mechanical apparatus for sealing that makes efficient performance of the equipments. The sealing performance of O-ring is affected in environments of the O-rings, like that applied pressure, working temperature, pre-compressed ratio and materials. In this paper, a pressurized, compressed elastomeric bi-polymer O-ring inserted into a rectangular groove is analyzed numerically using the MARC finite element program. The calculated FEM results showed that bi-polymer O-ring that is manufactured by NBR for an inner and FFKM for an outer ring shows a low temperature distribution among various bi-polymer O-ring models. But, the normal contact stress between the flange and upper part of the O-ring is small compared to other bi-polymer model.

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75톤급 터보펌프 추진제 혼합 방지 실의 성능 시험 (Inter Propellant Seal Performance test for 75 ton Class Turbopump)

  • 전성민;곽현덕;박민주;김진한
    • 한국추진공학회지
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    • 제14권5호
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    • pp.57-64
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    • 2010
  • 75톤급 터보펌프용 추진제 혼합 방지 실의 누설 성능 및 내구 성능을 평가하기 위한 수류환경 성능 시험을 수행하였다. 추진제 혼합 방지 실 시제품은 연료펌프 부와 산화제펌프 부 각각 누적 시험 시간 2,100초 동안 수류환경에서 내구 성능 시험이 이루어 졌다. 1단의 카본 플로팅 링 실로 구성된 연료펌프 부는 성능 시험 동안 평균 실 차압 9.4 bar에서 평균 누설 유량 13.7 gram/sec의 결과를 얻었다. 반면, 2단의 카본 플로팅 링 실로 구성된 산화제펌프 부는 성능 시험 동안 평균 실 차압 9.5 bar에서 평균 누설 유량 7.3 gram/sec의 결과를 얻었다. 내구 성능 시험 후, 추진제 혼합 방지 실은 양호한 상태를 보였다. 향후 액체 질소를 시험 매질로 하는 극저온 환경에서 추진제 혼합 방지 실 누설 성능 시험이 수행될 예정이다.

유한요소해석을 이용한 이물질이 고무 오링에 미치는 영향과 성능 평가 (Study on the performance of elastomeric O-ring subjected to foreign objects using finite-element analysis)

  • 백인석;이희장;이석순
    • 항공우주시스템공학회지
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    • 제10권3호
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    • pp.52-58
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    • 2016
  • The elastomeric O-ring is the most-commonly-used seal due to its excellent sealing capacity, and its availability in various costs and sizes; furthermore, its importance has lasted over a long duration. However, a dearth of research exists in Korea regarding the elastomeric O-ring and the corresponding techniques. The constituent parts of elastomeric rubber are important; to determine their properties, the uni-axial tension and equi-biaxial tension need to be tested. Also, the non-linear analysis method reduces the design cost. An O-ring failure causes leaks and vibration. In this paper, foreign objects are used to affect an O-ring and its performance so that all angles of the O-ring design can be considered. This paper presents a solution for the O-ring-failure problem using a finite-element analysis.

Mechanical Seal의 이상설계 감시에 관한 연구

  • 임순재;최만용;남궁석
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 1992년도 추계학술대회 논문집
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    • pp.166-171
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    • 1992
  • Mechanical seals are generally used in the fields of industries as sealing devices. The failure of mechanical seals like crack, leakage, breakage fast and severe wear, excessive torque, and squeaking result in big problems. For the development of monitoring system, this study was carried out to identify abnormal phenomina on alumina(AI $\_$2/ O /sub3/) seal ring and resin bonded carbon ring, and to propose the proper parameter for monitoring failure on mechanical seals. Sliding were tests are conducted at 12 experimental conditions that contains 3 different contact pressure and 4 surface conditions. Torque, temperature, and acoustic emission are measured. Optical microstructure and scanning electron microscopy are observed for the wear processing every 10 minute sliding at rotation speed of 1750 RPM.

기계평면시일의 기하학적 형태가 압력분포에 미치는 영향에 관한 연구 (Geometric Effects on Pressure Distribution in Mechanical Face Seals)

  • 김청균;이일권
    • Tribology and Lubricants
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    • 제5권2호
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    • pp.48-54
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    • 1989
  • The effects of angular misalignment, coning and the temperature difference between the primary seal ring and the seal seat on the pressure distribution in mechanical face seals are analyzed. The modified Reynolds equation for the temperature dependent viscosity was solved by a finite difference approximation and Gauss-Seidel method. It is shown that the amplitude of pressure is significantly affected by the misalignment of the seals and a large temperature difference between the rotor and the stator.