• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2009년도 춘계학술대회 논문집
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• pp.376-381
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• 2009

The increasing needs for higher cargo capacity in the container vessels' fleet has led to ship builder's demand for higher power output rating engine to meet the propulsion requirement, thus, leading to the development of super large two stroke low speed diesel engines. This large sized bore engines with more than 12 cylinders are capable of delivering power output up to more than 100,000 bhp at maximum continuous rating. The thrust variation force due to axial vibration occurring in propulsion shafting of these ships are transmitted to ship structure via thrust bearing. This force may vibrate the super structure of ship in the fore-aft direction and the fatigue strength of crank shaft can be decreased by additional bending stress increase in crank shaft pin and journal. In this paper, the axial vibration of propulsion shafting system on the 14RT-flex96C super large diesel engine with 14 cylinders is identified by theoretical analysis and vibration measurement.

• 대한전기학회논문지:전기기기및에너지변환시스템부문B
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• 제53권4호
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• pp.213-223
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• 2004

In the machine tool industry, direct drive linear motor technology is of increasing interest as a means to achieve high acceleration, and to increase reliability. The advantages of such a motor are that it has a good linearity and has no need of such mechanical energy conversion parts, which change rotary motion into linear motion, as screws, gears, chains etc In this paper, two structures of LOA are analyzed. One is the moving-coil type LOA and the other is moving-magnet type LOA. Two types of LOA are analyzed, with reference to the following parameters as variables: magnetic field, flux linkage, motor thrust and back emf. These variables are derived by the use of analytical method in terms of two-dimensional rectangular coordinate system. The maximum values of thrust according to such design parameters as air-gap length and magnet height for each model is also represented. The results are validated extensively by comparison with finite element method. In particular, we experiment moving-coil LOA which is already manufactured and confirm that the experimental results are shown in good agreement with analysis through the comparison of between analytical and experimental results

• 한국추진공학회지
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• 제13권6호
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• pp.17-23
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• 2009

정확한 추력 및 비추력 특성을 파악하기 위하여 액체로켓엔진용 연소기에 추가적으로 임시 노즐확장부를 장착함에 있어, 그 열/구조적 건전성을 파악하였다. 이 열/구조적 건전성은 재질 및 차폐막(TBC)의 두께 효과를 살펴봄으로써 검토하였다. TBC가 없는 경우에는 열/구조적 건전성을 유지할 수 없음을 파악할 수 있었다. TBC의 두께에 따라서 노즐확장부 벽면에서의 최대온도는 많이 감소하였다. 노즐확장부를 steel로 제작하는 경우에는 TBC를 적용해야만 연소시험동안 확장부의 열/구조적 건전성이 보장될 것으로 예상된다.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2003년도 유체기계 연구개발 발표회 논문집
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• pp.549-554
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• 2003

EPRI PPM (Performance Prediction Methodology), a method used for the prediction of required thrust of valves, can not be applied to unbalanced-disk globe valves operated in the fluid when the fluid temperature is above $150^{\circ}F$ because the thrust increase caused by the friction between the valve disk and body is not considered in the PPM. In order to apply PPM to the valves, EPRI suggested new friction prediction method to be added in the code. This paper analyzes the applicability of the prediction method comparing the disk-to-body friction load predicted from the method with the measured friction load from the field tests. The maximum values from the prediction method and those obtained from the test were 268lbs and about 1500lbs, respectively. It is included that the prediction method should be improved for the realistic prediction of disk-to-body friction load.

• 한국항공우주학회지
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• 제47권1호
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• pp.1-8
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• 2019

비례제어밸브를 이용한 초음속 추력편향제어의 특성을 관찰하기 위한 실험적 연구가 진행되었다. 노즐 압력비에 따라 세 가지 서로 다른 추력편향 제어특성이 나타나고, 밸브작동에 따른 강한 이력현상이 관찰되었다. 아울러 이차챔버의 압력이 추력편향에 영향을 주는 주요 인자 중의 하나임이 확인되었다. 이에 이력현상을 회피하고 밸브제어에 따른 안정된 추력편향을 구현하기 위하여 이차챔버의 압력계수를 이용한 제어 알고리즘이 적용되었다. 그 결과 비례제어밸브를 통하여 최대 추력편향각 $20^{\circ}$ 범위에서 안정적인 추력편향제어가 구현 가능함이 확인되었다.

• 한국항공우주학회지
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• 제37권9호
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• pp.939-945
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• 2009

액체로켓 연소기 재생냉각 챔버의 제작에 사용되는 구리합금의 성형한계 곡선을 얻기 위하여 돔 장출 시험과 인장시험을 수행하였다. 성형한계 곡선에 대한 실험적인 연구를 위하여 인장시편을 사용하여 인장-압축 변형률 상태의 데이터를 얻었으며, 인장-인장의 변형률 상태를 얻기 위하여 돔 장출 시험용 시편을 사용한 돔 장출 시험 또한 수행하였다. 시험에 사용한 모든 시편은 제작방향에 따라 종 방향과 횡 방향시편으로 구분하였다. 시험 결과 인장-인장 변형률 상태에서 최대 주 변형률과 부 변형률은 62.3%와 58.6%이며, 인장-압축 상태에서는 60.5%와 25.8%로 나타났다.

• 비파괴검사학회지
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• 제23권6호
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• pp.577-582
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• 2003

This paper describes a new technique for thickness measurement of a very thin layer less than one-quarter of the wavelength of ultrasonic wave used in the ultrasonic pulse-echo measurements. The technique determines the thickness of a thin layer in a tapered medium from constructive interference of multiple reflection waves. The interference characteristics are derived and investigated in theoretical and experimental approaches. Modified total reflection wave g(t) defined as difference between total and first reflection waves increases in amplitude as the interfacial layer thickness decreases down to zero. A layer thickness less than one-tenth of the ultrasonic wavelength is measured using the maximum amplitude of g(t) with a good accuracy and sensitivity. The method also requires no inversion process to extract the thickness information from the waveforms of reflected waves, so that it makes possible to have the on-line thickness measurement of a thin layer such as a lubricating oil film in thrust bearings and journal bearings during manufacturing process.

• 한국정밀공학회지
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• 제1권2호
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• pp.58-68
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• 1984

In this study, the static and dynamic components of cutting resistance were measured with tool dynamometer (Swiss, pieso-electric type) when S45C, A1-alloy and brass were drilled under the some variable conditions. The results obtained are as follows; 1) The dynamic components of these cutting resistance are not related to the depth of drilled hole. 2) The static and dynamic components of cutting resistance are increased in accordance with the increase of feed and drill diameter. 3) The dynamic components of thrust force are increased in accordance with the increase of spindle speed. 4) The rate of the dynamic component to the static component is 0.3 .approx. 0.5 in torque, 0.1 .approx. 0.2 in thrust force. 5) The characteristic of the tool system is affected in dynamic component of cutting resistance, and the creasted frequency and amplitude of the chip are determined by the crilled materials. 6) The maximum amplitude of the dynamic component is increased proportionally in accordance with the feed rate and the spindle speed.

• 한국철도학회:학술대회논문집
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• 한국철도학회 2007년도 추계학술대회 논문집
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• pp.1460-1465
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• 2007

In this paper, the conventional linear induction motor(LIM) used in propelling the MAGLEV in Korea is redesigned in order to reduce its weight. The specifications of the newly designed model for base speed, acceleration, rated thrust and maximum output is respectively 45km/h, 4.0km/h/sec, 5,200[N] and 65 [kW]. Weight reduction effect of the LIM according to the change of pole number from 8 to 6 is shown. Equivalent circuit analysis considering end effect and finite element method are used for the analysis of the redesigned model. Finally the weight reduction ratio of the newly designed LIM to the conventional model, thrust, attraction force, line current, temperature rise, flux density distribution are presented.

• Tribology and Lubricants
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• 제24권6호
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• pp.349-354
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• 2008

An inter-propellant seal (IPS) for high thrust turbopump is designed. With given operating conditions and requirements, the inter-propellant seal is designed to satisfy the leakage characteristics which is less than 0.1% of normal flow rate of pumps. A numerical analysis is developed to predict the leakage flow rate. The results show that the maximum leakage of LOX and kerosene are less than 0.1% of normal flow rate of pumps, respectively. Based on the numerical analysis results, the detail of IPS is performed. Finally a prototype of IPS is manufactured to perform sets of performance tests in the near future.