• Transactions of the Korean Society of Mechanical Engineers A
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• v.35 no.6
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• pp.643-649
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• 2011

For the development of butterfly valves used in liquefied natural gas (LNG) vessels, the seat tightness is one of the important factors to be taken into account in the valve-design process. An O-ring-type metal seal with a retaining ring showing good seat tightness at cryogenic temperatures has been widely used, despite the high manufacturing costs involved. As an alternative, a flexible solid metal seal offers not only sufficient tightness of the butterfly valve, meeting specification requirements, but also relatively low manufacturing costs. In this study, a design criterion to ensure the seat tightness of the butterfly valve using the flexible solid metal seal is proposed. The contact pressure can be calculated by the simulation of the frictional contact behavior between the surface of the metal seal and the valve disc. The geometry of the flexible solid metal seal is determined so that it satisfies the design criterion for sufficient seat tightness, and is verified by experiments according to BS6755 and BS6364.

• 월간 기계설비
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• s.15
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• pp.124-129
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• 1991

• 월간 기계설비
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• s.17
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• pp.132-138
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• 1991

• 월간 기계설비
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• s.19
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• pp.140-143
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• 1991

• 월간 기계설비
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• s.16
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• pp.124-127
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• 1991

• 월간 기계설비
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• s.18
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• pp.168-172
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• 1991

• 전기의세계
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• v.44 no.4
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• pp.42-49
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• 1995

산업이 고도로 발달하게 됨에 따라 가스관, 상하수도관, 송유관등의 시설이 필요하게 되고 이런 시설들은 도심에서 지하에 매설되게 된다. 지하에 매설되는 금속배관은 토양중에서 부식환경에 놓이게 되며 자연부식을 방지하기 위하여 도장등의 방식방법과 병행하여 전기화학적 반응을 이용한 전기 방식 방법을 채택하여 실시하고 있다. 그러나 도시 교통난 해소를 위하여 직류로 운행되는 전기철도가 시설되면서 직류전기철도에서 누설전류가 발생하게 되고 누설전류는 지하매설물에 영향을 미쳐 심각한 부식을 일으키게 된다. 본 글에서는 금속의 부식과 직류전류에 의한 전식에 대하여 기술하고 여러가지 전기방식방법과 직류전기철도에 의한 전식방지대책 적용 및 시공사례, 기타 전식방지대책에 대하여 기술한다.

• Journal of the Korean Society of Safety
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• v.7 no.3
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• pp.108-116
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• 1992

가스누설에 의한 화재는 폭발을 동반하는 경우가 많을 뿐만아니라 연소가 급격하게 이루어지고, 피해 또한 크기 때문에 이를 미연에 방지하기 위하여 지하가등 일정규모 이상의 특정방화 대상물에서 가스연소기를 사용할 경우에는 가스누설 화재경보설비의 설치를 의무화하고 있다.(중략)

• Journal of the Korean Society of Propulsion Engineers
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• v.14 no.5
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• pp.57-64
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• 2010

A performance test of inter propellant seal for a 75 ton class turbopump is conducted using water to evaluate leakage and endurance performance. Each part of fuel pump side and oxidizer pump side for a prototype inter propellant seal has been tested for verifying endurance performance during total accumulated test time 2,100 sec in water. The fuel pump side part with one-stage seal of carbon floating ring shows average leakage rate 13.7 gram/sec under average seal differential pressure 9.4 bar. On the other hand, the oxidizer pump side part with two-stage seal assembly of carbon floating rings shows average leakage rate 7.3 gram/sec under average seal differential pressure 9.5 bar. After the endurance performance test, the inter propellant seal shows good physical condition. A leakage performance test of the inter propellant seal for cryogenic environment will be performed using LN2 in the near future.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2010.05a
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• pp.47-53
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• 2010

A performance test of a 75 ton class turbopump inter propellant seal is conducted using water to evaluate leakage and endurance performance. Each fuel pump side part and oxidizer pump side part of a prototype inter propellant seal has been tested for verifying endurance performance during total accumulated test time 2,100 sec in water. The fuel pump side part with 1 stage carbon floating ring seal shows average leakage rate 13.7 gram/sec under average seal differential pressure 9.4 bar. On the other hand, the LOx pump side part with 2 stage carbon floating ring seal shows average leakage rate 7.3 gram/sec under average seal differential pressure 9.5 bar. After the endurance performance test, the inter propellant seal shows good physical condition. A cryogenic leakage performance test of the inter propellant seal will be performed using LN2 in the near future.