• 한국초전도ㆍ저온공학회논문지
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• 제21권1호
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• pp.25-30
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• 2019

This paper presents a conceptual design approach of air-cored synchronous machine with high temperature superconductor (HTS) field winding. With a given configuration of a target machine, boundary conditions are set in the cylindrical coordinate system and analytic field calculation is performed by solving a governing equation. To set proper boundary conditions, current distributions of the field winding and the armature winding are expressed by the Fourier expansion. Based on analytic magnetic field calculation results, key machine parameters are calculated: 1) inductance, 2) critical current of field winding, 3) weight, 4) HTS conductor consumption, and 5) efficiency. To investigate all potential design options, 6 sweeping parameters are determined to characterize the geometry of the machine and the parameter calculation process is performed for each design options. Among design options satisfying constraints including >80 % critical current margin and >95 % efficiency, in this paper, a first-cut design was selected in terms of overall machine weight and HTS conductor consumption to obtain a lightweight and economical design. The goal is to design a 5-MW machine by referring to the same capacity machine that was previously constructed by another group. Our design output is compared with finite element method (FEM) simulation to validate our design approach.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2005년도 춘계학술대회 논문집
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• pp.541-546
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• 2005

Tracking control of an automatic pipe cutting robot (APCROMB) is studied. Using magnetic force APCROMB, which is designed and developed in Kyung Hee University, binds itself to the pipe and executes unmanned cutting process. The gravity effect on the movement of APCROMB varies as it rotates around the cylindrical pipe laid in the gravitational field. To maintain a constant velocity and consistent cutting performance against the varying gravitational effect, the authors adopt a multi-rate repetitive learning controller (MRLC), which learns the required effort to cancel the repetitive tracking errors caused by nonlinear effect. In addition to the varying gravity effect other types of nonlinear disturbances including backlash in the driving system and the slip between the wheels of APCROMB and the pipe also cause degradation in the cutting process. In order to identify those nonlinear disturbances the position estimation based on the encoder attached at the motor is not good enough. To identify the absolute angular position of APCROMB the authors propose the angular position estimation based on the signals from a MEMS-type two-axis accelerometer mounted on APCROMB. The tracking performances of APCROMB with a MRLC using the encoder-based position estimation is experimentally measured and results are shown. Also the difference between the encoder-based angular displacement measurement and the accelerometerbased angular displacement measurement is included.

• 한국추진공학회지
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• 제17권5호
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• pp.27-36
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• 2013

본 연구에서는 고체로켓 모터의 연소 불안정성을 예측하고 분석 할 수 있는 해석도구의 개발을 위해 음향에너지의 분석과 선형 안정성 해석을 수행하였다. 음향 해석의 경우 상용 프로그램인 COMSOL을 이용하여 단면적이 일정한 실린더 형상의 연소실 음향 해석 및 모드 해를 도출하였다. Culick에 의해 정립된 고체추진 로켓의 선형 안정성 해석에 기초하여 연소 불안정성을 진단하였으며 압력결합, 노즐감쇠, 입자감쇠의 안정성 요소(stability alpha) 외에 유동방향변환(flow turning) 요소와 점성감쇠(viscous loss) 요소를 추가하여 연료 표면 근처의 유동 및 점성효과를 포함하는 연소 불안정의 경향을 파악하였다. 또한 입자의 크기에 따른 주파수 영역별 연소 불안정 감쇠 특성을 파악하였다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2010년도 제34회 춘계학술대회논문집
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• pp.210-213
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• 2010

최근의 실험 결과를 통해 하이브리드 로켓 연료의 표면에 연소가 진행되지 않은 채 남아있는 고립된 부분들이 존재함을 확인하였다. 이러한 불규칙적인 spot은 연료의 기화로 인한 분출유동(wall blowing)과 산화제의 유동 사이에서 발생하는 경계층 교란에 의한 현상인 것으로 여겨진다. 본 연구에서는 23,000의 높은 Reynolds수와 벽면분출 현상을 효과적으로 처리할 수 있도록 LES 기법을 이용하여, 연료 표면 근처의 난류 유동 특성을 해석하였다. 원형 단면을 갖는 하이브리드 로켓 모터의 그레인 형상을 사실적으로 모사하기 위하여 곡률효과를 포함한 3차원 실린더 형태의 지오메트리를 고려하였다. 연료 표면에서 발생하는 불규칙한 spot의 발생은 경계층과 분출되는 유동이 상호 간섭함으로써 난류구조들의 기구학적 특성을 변경시키기 때문인 것으로 추측되는 결과들을 얻을 수 있었다.

• 한국추진공학회지
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• 제22권2호
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• pp.38-51
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• 2018

무노즐 부스터의 성능을 향상시키기 위한 연구를 수행하였다. 알루미늄 금속연료와 비교하여 고 밀도를 갖는 지르코늄을 사용한 고밀도 추진제를 개발하였고, 이 추진제를 이용하여 세장비에 따른 성능 특성을 알아보았다. 알루미늄 조성의 추진제 성능과 비교하여 모든 세장비에서 지르코늄 조성의 추진제가 비추력을 제외하고 높게 나타났다. 지르코늄 조성의 추진제의 비추력은 세장비가 증가함에 따라 시험조건 내에서 알루미늄 조성의 추진제와 비교하여 88%까지 감소하였다. 그러나, 추진제의 밀도차이로 인하여 모든 세장비에서 알루미늄 조성의 추진제보다 지르코늄 조성의 추진제가 높게 나타났다.

• 한국추진공학회지
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• 제23권3호
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• pp.51-57
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• 2019

HTPB 고체 추진제 기계적 물성의 후경화 효과에 대하여 시편 시험을 통하여 평가하였다. 후경화 반응 완료 후 시편 가속노화 시험을 실시하여 Arrhenius 식의 계수를 획득하였다. 확인을 위하여 원통형 모사 충전체를 설계, 제작하여 가속노화 시험을 수행하였으며, 시험 후 추진제 표면 부위, 중앙 부위, 접착 부위에 대하여 시편을 채취하여 노화 물성을 평가하였다. 측정된 결과에 대하여, 획득된 가속노화 식으로 예측하여 비교하였다. 그 결과 JANNAF 시편 시험을 통한 가속노화 식은 추진제 재료의 노화를 잘 예측하였으나 접착 부위에서는 실제 측정 결과와 차이를 나타내었다. 따라서 실기형 추진기관에서 노화 시료를 채취하는 경우 시험 목적에 부합하도록 시편 채취 부위를 선정해야 한다.

• 수산해양기술연구
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• 제19권1호
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• pp.17-24
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• 1983

흑, 적, 녹색의 그물무늬의 시각막을 15.0, 37.4, 62.9cm/sec의 속도로 회전시켰을 때의 송사리 Orizias latipes의 방어 Seriola quinqueradiata의 시각운동반응을 조사한 결과는 다음과 같다. 1. 시각운동반응율은 송사리가 95%, 방어가 94%였다. 2. 송사리가 잘 반응하는 시각막의 색상은 흑, 적, 녹색의 순이며, 흑색에 대한 적, 녹색의 차이는 뚜렷했으나 적색과 녹색의 차이는 뚜렷하지 않았다. 3. 방어가 잘 반응하는 시각막의 색상은 흑, 적, 녹색의 순이며, 색상에 따른 차이는 뚜렷하지 않았다. 4. 시어가 잘 반응하는 시각막의 속도는 62.9, 37.4, 15.0cm/sec의 순이며, 속도에 따른 차이는 뚜렷했다

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2011년도 제36회 춘계학술대회논문집
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• pp.1-2
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• 2011

Hybrid rockets have lately attracted attention as a strong candidate of small, low cost, safe and reliable launch vehicles. A significant topic is that the first commercially sponsored space ship, SpaceShipOne vehicle chose a hybrid rocket. The main factors for the choice were safety of operation, system cost, quick turnaround, and thrust termination. In Japan, five universities including Hokkaido University and three private companies organized "Hybrid Rocket Research Group" from 1998 to 2002. Their main purpose was to downsize the cost and scale of rocket experiments. In 2002, UNISEC (University Space Engineering Consortium) and HASTIC (Hokkaido Aerospace Science and Technology Incubation Center) took over the educational and R&D rocket activities respectively and the research group dissolved. In 2008, JAXA/ISAS and eleven universities formed "Hybrid Rocket Research Working Group" as a subcommittee of the Steering Committee for Space Engineering in ISAS. Their goal is to demonstrate technical feasibility of lowcost and high frequency launches of nano/micro satellites into sun-synchronous orbits. Hybrid rockets use a combination of solid and liquid propellants. Usually the fuel is in a solid phase. A serious problem of hybrid rockets is the low regression rate of the solid fuel. In single port hybrids the low regression rate below 1 mm/s causes large L/D exceeding a hundred and small fuel loading ratio falling below 0.3. Multi-port hybrids are a typical solution to solve this problem. However, this solution is not the mainstream in Japan. Another approach is to use high regression rate fuels. For example, a fuel regression rate of 4 mm/s decreases L/D to around 10 and increases the loading ratio to around 0.75. Liquefying fuels such as paraffins are strong candidates for high regression fuels and subject of active research in Japan too. Nakagawa et al. in Tokai University employed EVA (Ethylene Vinyl Acetate) to modify viscosity of paraffin based fuels and investigated the effect of viscosity on regression rates. Wada et al. in Akita University employed LTP (Low melting ThermoPlastic) as another candidate of liquefying fuels and demonstrated high regression rates comparable to paraffin fuels. Hori et al. in JAXA/ISAS employed glycidylazide-poly(ethylene glycol) (GAP-PEG) copolymers as high regression rate fuels and modified the combustion characteristics by changing the PEG mixing ratio. Regression rate improvement by changing internal ballistics is another stream of research. The author proposed a new fuel configuration named "CAMUI" in 1998. CAMUI comes from an abbreviation of "cascaded multistage impinging-jet" meaning the distinctive flow field. A CAMUI type fuel grain consists of several cylindrical fuel blocks with two ports in axial direction. The port alignment shifts 90 degrees with each other to make jets out of ports impinge on the upstream end face of the downstream fuel block, resulting in intense heat transfer to the fuel. Yuasa et al. in Tokyo Metropolitan University employed swirling injection method and improved regression rates more than three times higher. However, regression rate distribution along the axis is not uniform due to the decay of the swirl strength. Aso et al. in Kyushu University employed multi-swirl injection to solve this problem. Combinations of swirling injection and paraffin based fuel have been tried and some results show very high regression rates exceeding ten times of conventional one. High fuel regression rates by new fuel, new internal ballistics, or combination of them require faster fuel-oxidizer mixing to maintain combustion efficiency. Nakagawa et al. succeeded to improve combustion efficiency of a paraffin-based fuel from 77% to 96% by a baffle plate. Another effective approach some researchers are trying is to use an aft-chamber to increase residence time. Better understanding of the new flow fields is necessary to reveal basic mechanisms of regression enhancement. Yuasa et al. visualized the combustion field in a swirling injection type motor. Nakagawa et al. observed boundary layer combustion of wax-based fuels. To understand detailed flow structures in swirling flow type hybrids, Sawada et al. (Tohoku Univ.), Teramoto et al. (Univ. of Tokyo), Shimada et al. (ISAS), and Tsuboi et al. (Kyushu Inst. Tech.) are trying to simulate the flow field numerically. Main challenges are turbulent reaction, stiffness due to low Mach number flow, fuel regression model, and other non-steady phenomena. Oshima et al. in Hokkaido University simulated CAMUI type flow fields and discussed correspondence relation between regression distribution of a burning surface and the vortex structure over the surface.