• Journal of Advanced Navigation Technology
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• v.23 no.5
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• pp.386-391
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• 2019

This paper presents analysis results for the effect of the directional group delay of the antenna to implement a precision radio navigation system. The analysis was conducted through antenna simulation and test, and the test was performed in an anechoic chamber. The directional group delay of the antenna was calculated in phase-based analysis method. The results showed that a variation of up to 7.7ns in group delay occurred per antenna direction. The group delay variation from the analysis is 2.31 meters when converted into distance. It was tested using a real radio navigation system based on the time of arrival (TOA). The test verified the distance variation of 2.1 meters, and this value is similar to those obtained from the simulation and chamber test analysis.

• Journal of Korean Tunnelling and Underground Space Association
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• v.26 no.2
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• pp.91-111
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• 2024

Most of utility cable tunnels are constructed utilizing shield TBM as part of the underground transmission line project. The TBM chamber is the only space inside the tunnel that encounters rock and soil, and is the place with the highest frequency of accident exposure, such as collapse and collision accidents. Since there is currently no way to measure the disc cutter wear from outside the chamber, frequent inspection by workers is essential. Accordingly, in this study, in order to prevent safety accidents inside the TBM chamber and expect the effect of shortening the construction period by reducing the number of chamber openings, the concept of disk cutter wear measurement technology was established and a prototype was produced. By considering prior technology and determining that magnetic sensors are most suitable for the excavation environment, wear measurement sensor package were developed integrating magnetic sensors, wireless communication modules, power supply, external casing, and monitoring systems. To verify the performance of the prototype in an actual excavation environment, a full-scale tunnelling test was performed using a 3.6 m EPB shield TBM. Based on the full-scale tests, five prototypes were operated normally among eight prototypes. It was analyzed that sensor measurement, wireless communication, and durability performance were secured within a maximum thrust of 3,000 kN and a rotation speed of 1.5 RPM.

• Proceedings of the Korea Air Pollution Research Association Conference
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• 2006.04a
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• pp.191-192
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• 2006

• Bulletin of the Korean Space Science Society
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• 2006.04a
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• pp.102-102
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• 2006

• Bulletin of the Korean Space Science Society
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• 2006.10a
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• pp.170-170
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• 2006

• Proceedings of the Korean Society of Marine Engineers Conference
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• 2011.06a
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• pp.223-223
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• 2011

• Proceedings of the Korean Vacuum Society Conference
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• 2008.08a
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• pp.198-198
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• 2008

• Proceedings of the Korea Air Pollution Research Association Conference
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• 2008.04a
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• pp.700-702
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• 2008

• Proceedings of the Korean Vacuum Society Conference
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• 2016.02a
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• pp.165.1-165.1
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• 2016

Zn의 수요는 매년 증가하지만 매장량의 한계로 대체용 물질계가 개발이 필요한 시점이다. Zn보다 상대적으로 풍부하고 동일 두께의 Zn 코팅층과 비교하여 우수한 내식성을 보이는 Al과 Mg의 코팅층을 제작하여 Al-Mg 코팅 강판의 특성 분석 및 평가를 실시하였다. Al-Mg 코팅층은 99.99%의 Al, 99.9%의 Mg target을 사용하여 스퍼터링을 이용하여 냉연강판 위에 코팅하였다. 증발물질과 기판과의 거리는 7cm 이며, 기판은 세척을 실시한 후 클리닝 챔버에 장착하고 ~10-5 Torr 까지 진공배기를 실시하였다. 클리닝 챔버가 기본 압력까지 배기되면 아르곤 가스를 주입하고 기판 홀더에 -800 V의 직류 전압을 인가하여 약 30분간 글로우 방전 청정을 실시하였다. 기판의 청정이 끝나면 아르곤 가스를 차단하고 코팅 챔버로 시편을 이송 후 코팅층 성분의 구성형태에 따라 Al과 Mg을 코팅하였다. Al-Mg 코팅층은 $3{\mu}m$의 두께를 기준으로 Mg wt.%의 비율을 5% ~ 90%까지 변화시키며 코팅하였다. 그리고 후속 공정으로 질소 분위기 $400^{\circ}C$에서 10분간 열처리를 하였다. Al-Mg 코팅층을 주사전자현미경으로 관찰한 결과, 표면에서는 Al-Mg 코팅층에 존재하는 Mg 함량이 높아질수록 grain의 크기가 증가하였고 단면에서는 열처리 전의 치밀한 구조에서 열처리 후에는 주상구조 혹은 grain 구조가 선명해지는 것을 볼 수 있었으며 글로우방전분광기로 Al과 Mg의 성분 비율변화를 확인할 수 있었다. 또한 Al-Mg가 코팅된 강판을 염수분무시험을 통해서 내부식 특성을 확인하였다. Al-Mg 코팅 강판의 염수분무시험 결과, Mg 함량이 낮은 Al-Mg 코팅층은 열처리 후 뚜렷한 내식성 향상을 보였으며 Mg 조성 변화에 따라 일정한 경향성을 보였다. 하지만 Mg 함량이 높은 Al-Mg 코팅층은 열처리 후 급격한 내식성 저하와 함께 시편간의 편자가 커지는 것을 확인 할 수 있었다. 최적의 내식성을 보이는 Mg의 조성을 확인하기 위해서는 향후 보다 변별력이 높은 평가가 결과가 필요하다고 판단되어진다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2008.05a
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• pp.321-327
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• 2008

Performance characteristics of the axi-symmetric supersonic exhaust diffuser (SED) with a second throat are numerically investigated. Computational strategy repeats those for a straight exhaust diffuser with zero-secondary flows. Renolds-Average Navier-Stokes equations with a standard ${\kappa}-{\varepsilon}$ turbulence model incorporated with standard wall function are solved to simulate the diffusing evolutions of the nozzle plume. The methodology is validated with accuracy. To predict the improvement of starting performance by second throat diffuser, diffuser characteristic curve due to the SED equipped with the second throat is speculated with respect to that of a straight area type as a function of nozzle stagnation pressure. Principal physics caused by the of the second throst is also addressed in terms of a second throat area ratio.