• 플랜트 저널
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• 제12권1호
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• pp.29-36
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• 2016

최근 늘어가는 에너지 수요를 화석연료에만 의존 할 수 없게 되면서 대체 에너지의 중요성이 대두되고 있으며, 이러한 상황에서 유기랭킨 사이클(Organic Rankine Cycle, 이하 ORC)등 산업체 폐열, 태양열, 지열, 해수 온도차 등의 저등급 에너지를 효과적으로 활용하기 위한 많은 연구가 진행되고 있다. 본 연구에서는 지역난방 축열시 회수수를 혼합하지 않고 ORC를 이용하여 하부사이클을 구성하여 성능해석 상용프로그램으로 작동유체 및 운전특성을 예측하였다. 지역난방수 운전조건인 열원 온도 $120^{\circ}C$, 열원 유량 $163m^3/h$(회수수 유량을 고려한 값)로 하고 이 온도에 적합한 다수의 작동유체를 선정하여 성능해석을 수행하였으며, 최고의 성능이 나타난 R245fa의 경우 269.2kW출력과 6.37%효율을 얻을 수 있었다. 또한 ORC 시스템의 응축기 압력변화에 따라 지역난방 회수수 온도가 $57.3{\sim}85^{\circ}C$범위에 형성됨으로서 보일러 입구온도상승에 따른 연료 절감 효과가 예상되었다.

• 청정기술
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• 제19권4호
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• pp.355-369
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• 2013

재생 원료인 바이오매스를 이용한 에너지 생산에 있어서 경제성은 가장 중요한 인자 중 하나이다. 이러한 관점에서 슬러지 혐기소화에 의해 생산되는 바이오가스는 다른 바이오매스에 비해 매우 저렴하며 처분 비용 절감으로 얻는 이익이 부가적으로 발생하기 때문에 경제성이 매우 높다. 슬러지 혐기소화에서 기질의 가수분해 속도는 전체 소화 성능을 결정짓는 인자이며 혐기소화 속도를 향상시키기 위한 슬러지 전처리 기술이 많이 개발되었다. 슬러지 전처리는 생물학적, 열 가수분해, 초음파, 기계적 방법 등 다양한 기술이 실제 시설에 적용되었다. 전처리는 슬러지 가용화를 촉진하고 고형물을 감소시키면서 바이오가스 생산을 늘리는 등 혐기소화 효율을 향상시켰다. 본문에서는 전처리 방법의 기술적 특성을 소개하고 각 전처리 방법의 에너지 수지와 경제성을 비교하여 적절한 전처리 기술을 선정하기 위한 기준을 마련하고자 하였다. 조사 결과 고온 혐기소화와 열 가수분해가 가장 경제성이 높고 다음으로 Cell rupture$^{TM}$, OpenCEL$^{TM}$, MicroSludge$^{TM}$, 초음파의 순서로 평가되었다. 경제성 평가에 있어서 슬러지의 최종 처분 비용이 가장 큰 요소가 되며 따라서 최종 처분 슬러지의 수분 함량이 경제성 평가에 결정적인 역할을 하였다.

• 터널과지하공간
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• 제33권3호
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• pp.189-207
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• 2023

In the present study, the thermoshearing experiment on a rough rock fracture were modeled using a three-dimensional grain-based distinct element model (GBDEM). The experiment was conducted by the Korea Institute of Construction Technology to investigate the progressive shear failure of fracture under the influence of thermal stress in a critical stress state. The numerical model employs an assembly of multiple polyhedral grains and their interfaces to represent the rock sample, and calculates the coupled thermo-mechanical behavior of the grains (blocks) and the interfaces (contacts) using 3DEC, a DEM code. The primary focus was on simulating the temperature evolution, generation of thermal stress, and shear and normal displacements of the fracture. Two fracture models, namely the mated fracture model and the unmated fracture model, were constructed based on the degree of surface matedness, and their respective behaviors were compared and analyzed. By leveraging the advantage of the DEM, the contact area between the fracture surfaces was continuously monitored during the simulation, enabling an examination of its influence on shear behavior. The numerical results demonstrated distinct differences depending on the degree of the surface matedness at the initial stage. In the mated fracture model, where the surfaces were in almost full contact, the characteristic stages of peak stress and residual stress commonly observed in shear behavior of natural rock joints were reasonably replicated, despite exhibiting discrepancies with the experimental results. The analysis of contact area variation over time confirmed that our numerical model effectively simulated the abrupt normal dilation and shear slip, stress softening phenomenon, and transition to the residual state that occur during the peak stress stage. The unmated fracture model, which closely resembled the experimental specimen, showed qualitative agreement with the experimental observations, including heat transfer characteristics, the progressive shear failure process induced by heating, and the increase in thermal stress. However, there were some mismatches between the numerical and experimental results regarding the onset of fracture slip and the magnitudes of fracture stress and displacement. This research was conducted as part of DECOVALEX-2023 Task G, and we expect the numerical model to be enhanced through continued collaboration with other research teams and validated in further studies.

• 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.