• 한국식품영양과학회지
• /
• 제35권9호
• /
• pp.1251-1255
• /
• 2006

대두단백 필름을 코팅한 라이너지의 효과를 알아보기 위하여 대두단백 $2\sim8%$의 농도 범위에서 필름을 제조하였다. 필름 제조시 친수성 소재인 대두단백의 불용화를 위하여 모든 필름은 formaldehyde로 포화된 데시케이터에서 2시간 동안 흡착하여 사용하였다. 필름의 연신강도, 연신율, 투습도 및 수분용해도를 측정한 뒤 최적 농도를 5%로 판단하였다. 필름의 제조적성을 위해 첨가된 가소제 glycerol은 대두단백 대비 40% 농도에서 필름제조에 가장 적합하였다. 앞의 조건을 이용하여 제조된 용액을 라이너지에 코팅하여 그 물성과 수분저항성을 측정하였다. Formaldehyde 처리된 대두단백 코팅 라이너지는 미처리 라이너지에 비하여 연신강도는 15 에서 21 MPa로 증가하였고, 수분용해도와 투습계수는 1.17%와 $2.06ng{\cdot}m/m^2{\cdot}s{\cdot}Pa$로 감소하여 물리적 성질과 수분저항성 모두 증진된 것을 알 수 있었다.

• 한국연소학회:학술대회논문집
• /
• 한국연소학회 1997년도 제15회 KOSCO SYMPOSIUM 논문집
• /
• pp.135-151
• /
• 1997

The preliminary design and performance test for determining dimensions of gas turbine combustor were investigated. The combustor design program was developed and applied to design our combustor. and detailed design for determining of swirler. dome and liner holes were performed experimentally. The swirler. which govern the combustion characteristics of combustor, was determined $40^{\circ}$ as swirl angle at first performance test. After second performance test the swirler was re-determined by 24 mm i.d.. 34 mm o.d., and swirl angle of $45^{\circ}$. The geometry of liner holes were determined by considering the flame stability and recirculation zone size. It was found that flame can be more easily stabilized by adjusting the swirier dimensions rather than liner holes. The geometry of swirler and liner holes were re-determined by final performance test with dilution holes. Also. the performance of combustor was evaluated by analysis of exhaust gases.

• 대한기계학회논문집A
• /
• 제26권8호
• /
• pp.1608-1614
• /
• 2002

This Paper presents a novel piston friction force measurement system that has characteristics of relieving the Pressure force acting on the upper surface of the liner; the system uses general rubber O-rings for combustion chamber sealing, and does not need special changes to the piston top land. The lower supporter of the floating liner increases stiffness in liner axial direction, and results in the increase of natural frequency. The upper supporter has multi-layer structure designed fer low axial stiffness and high radial stiffness. With the use of the present system, the effects of variation in clearance and piston ring tension were studied.

• Tribology and Lubricants
• /
• 제14권4호
• /
• pp.37-43
• /
• 1998

The friction loss between piston rings and cylinder liner is due to the tension of the piston rings. Lubricant is usually supplied to reduce the friction. However, the sliding speed of the piston varies during the reciprocating cycle and is very low near TDC(Top Dead Center)/BDC(Bottom Dead Center), where the hydrodynamic lubrication cannot be sustained. Since the lubrication regime is shifted from the hydrodynamic to the boundary lubrication near TDC/BDC, wear particles are easily generated so that the friction loss becomes bigger and bigger due to the plowing effect of wear particles. In this study, for the purpose of reducing the friction loss, an undulated surface is adopted to the cylinder liner to trap wear particles. The friction force variations, which are measured by strain gaged, show that the concept of undulated surface is one of the promising methods to effectively reduce the friction between piston rings and cylinder liner.

• 대한기계학회:학술대회논문집
• /
• 대한기계학회 2008년도 추계학술대회B
• /
• pp.2984-2988
• /
• 2008

Numerical analyses are carried out in order to understand complex thermal characteristics of a gas turbine combustor liner such as combustion gas temperatures, wall temperatures and heat transfer distributions. As results, The maximum internal and external heat transfer is $2218W/m^2K$ and $2358W/m^2K$, respectively. The combustion gas temperatures range is 673K to 1760K. A range of temperature on TBC is 676K to 1382K. Lastly, temperature range on outer surface of combustion liner cooled by compressed air is 676K to 1188K.

• 대한기계학회논문집A
• /
• 제31권12호
• /
• pp.1214-1220
• /
• 2007

The vertical roller mill, which performs the grinding and partly blending of raw material, is the one of the important machine to produce ordinary portland cement. It has been reported that an unexpected fatigue failure occurred in a table liner in the course of grinding portland cement. The life of table liner is estimated to $4{\times}10^7$ cycles in the design stage, but at the field, when its operating time reaches to $2{\times}10^6{\sim}8{\times}10^6$ cycles, the fracture of table liner begins to be found. The fracture of table liner is initiated from the outside edge of grinding path contacting with the grinding roller. Its maintenance normally take 30 % of the total maintenance costs of the roller mill. Therefore, this study shows the clarification of the reasons occurring the fatal destruction of the table liner by fatigue fracture analysis utilizing fracture mechanics and by the finite element method. And, the results from Goodman diagram illustrate relationship of including information on the transition between tensile and bending fatigue strength in the fatigue characterization of table liner.

• 소성∙가공
• /
• 제22권4호
• /
• pp.204-215
• /
• 2013

As a pressure vessel, a small seamless aluminum liner with inner volume of about 6.75L is made from an initial billet material of AA6061-O. To produce the aluminum liner, warm forging including backward extrusion and head nosing was numerically simulated using a billet initially pre-heated to about $480^{\circ}C$. Compression tests on the billet material were performed at various temperatures and strain rates, and the measured mechanical properties were used in the numerical simulations. For the backward extrusion and the head nosing, the tool geometries were designed based on the desired configuration of the aluminum liner. Furthermore, the structural integrity of the tooling was evaluated to ensure adequate tool life. The seamless aluminum liner has an endurance limit of about 1.47MPa ($15Kg_f/cm^2$), estimated based on the required inner pressure. The results confirm that the small seamless aluminum liner of AA6061-O can be successfully made by using the two stage warm forging procedures without any bursting failures.

• 한국지반신소재학회논문집
• /
• 제7권2호
• /
• pp.49-52
• /
• 2008

현재 사용되고 있는 폐기물 매립지의 최종복토 차단층으로는 다짐점토층(Compacted Clay Liner; CCL)을 일반적으로 오랫동안 사용하고 있으나 압축성이 높은 폐기물 위에서는 시공이 어려우며, 고농도 유기물에 의한 붕괴를 유발하여 선진국 등에서 널리 사용되고 있는 부직포 등 토목합성물질 사이에 차수성이 뛰어난 벤토나이트를 삽입한 토목합성수지점토라이너(Geosynthetic Clay Liner; GCL)를 대체재로 많이 사용하고 있다. GCL은 설치 전, 후로 뚫림이 있을 수 있는 단점이 있어 CCL은 여전히 우리나라에서 널리 사용되고 있다. 하지만 CCL은 앞서 언급한 문제보다 국내의 기후 및 지형적인 여건으로 점토의 부족문제가 더 크게 작용하고 있어 그 대체물질의 개발이 시급히 요구되고 있다. 그 대체물질로 최근 슬러지가 주목을 받고 있는데 대부분의 슬러지는 매립지에 처분되거나 해양투기를 하고 있지만 2012년부터 런던협약에 따라 전면적으로 금지될 전망이기 때문에 슬러지의 친환경적인 처리 처분이 긴급히 요구되고 있는 실정이다. 이 문제를 해결하기 위한 혁신적인 방법의 하나로 열가수분해에 의한 처리기술을 들 수 있다. 본 연구에서는 부족한 양질의 점토를 대체하기 위해 하수슬러지를 열가수분해 처리하고 나온 부산물을 이용하여 첨가제를 혼합하여 최적배합비로 혼합한 다짐혼합재(Compacted Mixing Materials; CMM)를 차수능이 높은 GCL과 비교하여 CMM의 최종복토 차단층재로의 이용가능성을 평가하였다

• 한국연소학회:학술대회논문집
• /
• 한국연소학회 2014년도 제49회 KOSCO SYMPOSIUM 초록집
• /
• pp.239-242
• /
• 2014

• 한국건설순환자원학회지
• /
• 제12권2호
• /
• pp.50-55
• /
• 2017