• JSTS:Journal of Semiconductor Technology and Science
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• 제1권2호
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• pp.125-131
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• 2001

When the program voltage is applied to a word line, a part of the boosted channel charge in inhibited bit lines is lost due to the coupling between the string select line (SSL) and the adjacent word line. This phenomenon causes the program disturbance in the cells connected to the inhibited bit lines. This program disturbance becomes more serious, as the word line pitch is decreased. To reduce the word line coupling, the rising edge of the word-line voltage waveform was changed from a pulse step into a ramp waveform with a controlled slope. The word-line ramping circuit was composed of a timer, a decoder, a 8 b D/A converter, a comparator, and a high voltage switch pump (HVSP). The ramping voltage was generated by using a stepping waveform. The rising time and the stepping number of the word-line voltage for programming were set to $\mutextrm{m}-$ and 8, respectively,. The ramping circuit was used in a 512Mb NAND flash memory fabricated with a $0.15-\mutextrm{m}$ CMOS technology, reducing the SSL coupling voltage from 1.4V into a value below 0.4V.

• 대한치과보철학회지
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• 제45권4호
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• pp.482-491
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• 2007

Statement of problem: The screws of dental implant, having various thread types, can be categorized into different classes by their geometrical form, and each type transmits dissimilar amount and form of stress to alveolar bone. Purpose: The purpose of this study was to find an inclination angle of the screw thread that is favorable in distributing the stresses to alveolar bone. Material and methods: In this study, We used three dimensional finite element analysis with modeling having three types of thread inclination angles and fixed pitch-0.8 mm (single thread type with $3.8^{\circ}$ inclination, double thread type with $7.7^{\circ}$ inclination, triple thread type with $11.5^{\circ}$ inclination). Results: The results obtained from this study were as follows; 1. When the number of thread increased, the amount of Von-Mises stress was reduced since the generated stress was effectively distributed. 2. Since the maximum principal stress affects on the alveolar bone can influence deeply on the longevity of the implants when comparing the magnitude of the maximum principal stress double thread had least amount of stress. This shows that the double thread screw gave best result. Conclusion: In conclusion, double, and triple thread screws were found to be more effective on distribution of the stress than the single thread screws. But, increasing in the thread inclination angle such as triple thread screw relate on the magnitude of the maximum principal stress affecting on the alveolar bone can become problematic. Thus, effective combination of thread number and thread inclination angle can help prolonging the longevity of implant.

• Journal of Biosystems Engineering
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• 제37권6호
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• pp.352-358
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• 2012

Purpose: The inexpensive black box system was developed to acquire and save driving information, to give the slope information, and to transmit SOS and theft signal. Method: The device consists of a main micro controller to acquire and save data, a GPS sensor module, a CDMA module, a touch LCD module, a RF (Radio Frequency) ID module, a SD (Secure Digital) card module, an emergency electric power source, a theftproof circuit, and a sensing device. The sensing device consists of a 8 bit micro controller, a accelerometer to detect impulse, two slope sensors to detect roll and pitch angle and a circuit to detect operation of 6 lighting devices. Results: Test results are as follows: 1) a tractor can be start up only with an electronic key (password or RFID card), 2) theft signal was transmitted when a tractor moved without an electronic key, 3) SOS was transmitted at conditions that rollover or crash happened. 4) 5 more than per 1s data are recorded at 5 minute intervals as new file name in SD card. Conclusions: This system can be used to save travelling record, reduce accident, prevent theft and rescue life in the accidents.

• Ocean and Polar Research
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• 제33권spc3호
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• pp.397-407
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• 2011

To understand the vertical structure of ocean currents from raw data observed by lowered-ADCP (LADCP), these data require post-processing. Data were processed using Krahman's version 10.8 processing software based on Matlab. It is estimated the influence of auxiliary data affecting the processed current structure. The bottom-tracked velocities and the GPS information significantly contribute the offset on reference velocities in the bottom layer and barotropic ones in the middle layer, respectively. Good quality data can be obtained when LADCP is least tilted in pitch and roll during observation. In situ application of LADCP to the (northward) volume transports of Kuroshio in the East China Sea proved to be 24.8. Sv (= $1{\times}10^6m^3s^{-1}$) in October 2007, and 28.2 Sv in June 2008, respectively. The volume transport is relatively large over the continental slope when compared to the shelf or the deep sea.

• 한국운동역학회지
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• 제18권3호
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• pp.1-10
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• 2008

운동화의 바닥에서 발생하는 마찰력은 착용자의 기동 능력에 많은 영향을 미친다. 이러한 마찰력은 아웃솔의 경도와 마모율, 소재, 바닥재, 바닥제의 상태, 그리고 무늬의 모양에 영향을 받는다. 본 연구는 운동화 아웃솔의 무늬와 바닥에서 발생하는 마찰력과의 상관 상관관계를 연구하고자 한다. 현장에서 생산 판매되고 있는 운동화를 조사하여 바닥창의 무늬를 분류하고 상호 비교를 위한 설계인자를 도출하였다. 기본적인 바닥창의 무늬 중에 일자형 무늬, W자형 무늬, 물결형 무늬와 O형을 검토의 대상으로 선정하였으며, 아울러 무늬의 깊이, 피치, 기울기를 설계인자로 선정하였다. 각각의 무늬와 설계 인자에 대하여 시편을 제작하고, 실험을 수행하여 마찰계수를 구하고 통계적 방법을 이용하여 설계인자에 대한 영향을 분석하였다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2008년 영문 학술대회
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• pp.671-679
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• 2008

The effect of Pre-cooled Turbojet Engine installation and nozzle exhaust jet on Hypersonic Turbojet EXperimental aircraft(HYTEX aircraft) were investigated by three-dimensional numerical analyses to obtain aerodynamic characteristics of the aircraft during its in-flight condition. First, simulations of wind tunnel experiment using small scale model of the aircraft with and without the rectangular duct reproducing engine was performed at M=5.1 condition in order to validate the calculation code. Here, good agreements with experimental data were obtained regarding centerline wall pressures on the aircraft and aerodynamic coefficients of forces and moments acting on the aircraft. Next, full scale integrated analysis of the aircraft and the engine were conducted for flight Mach numbers of M=5.0, 4.0, 3.5, 3.0, and 2.0. Increasing the angle of attack $\alpha$ of the aircraft in M=5.0 flight increased the mass flow rate of the air captured at the intake due to pre-compression effect of the nose shockwave, also increasing the thrust obtained at the engine plug nozzle. Sufficient thrust for acceleration were obtained at $\alpha=3$ and 5 degrees. Increase of flight Mach number at $\alpha=0$ degrees resulted in decrease of mass flow rate captured at the engine intake, and thus decrease in thrust at the nozzle. The thrust was sufficient for acceleration at M=3.5 and lower cases. Lift force on the aircraft was increased by the integration of engine on the aircraft for all varying angles of attack or flight Mach numbers. However, the slope of lift increase when increasing flight Mach number showed decrease as flight Mach number reach to M=5.0, due to the separation shockwave at the upper surface of the aircraft. Pitch moment of the aircraft was not affected by the installation of the engines for all angles of attack at M=5.0 condition. In low Mach number cases at $\alpha=0$ degrees, installation of the engines increased the pitch moment compared to no engine configuration. Installation of the engines increased the frictional drag on the aircraft, and its percentage to the total drag ranged between 30-50% for varying angle of attack in M=5.0 flight.

• 대한치과보철학회지
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• 제51권1호
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• pp.1-10
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• 2013

연구 목적: 임플란트 나사선 경사각이 치조골의 응력분포에 미치는 영향을 검토하여 어떤 임플란트가 응력분산에 유리한 지 알아보고자 하였다. 연구 재료 및 방법: 피치는 0.8 mm로 일정하게 하고 나사선의 줄(thread) 수를 다르게 하여 나사선 경사각의 변화를 준 1줄 나사선 임플란트(single thread type: 경사각 $3.8^{\circ}$)와 2줄 나사선 임플란트(double thread type: 경사각 $7.7^{\circ}$) 그리고 3줄 나사선 임플란트(triple thread type: 경사각 $11.5^{\circ}$)의 세 가지 모델을 통해 3차원 유한요소 응력분석을 시행하였다. 임플란트가 치조골의 치아 장축에 대하여 $0^{\circ}$, $10^{\circ}$, $15^{\circ}$ 경사지게 식립된 것으로 가정하여 9 가지 모델을 만들었다. 200 N의 수직 방향의 하중과, 200 N의 임의의 $15^{\circ}$ 경사 하중을 가한 경우에 임플란트와 치조골에서 발생된 응력분포를 3차원 유한요소법으로 분석하였다. 결과:1. 임플란트의 경사 식립 각도가 클수록 치조골과 임플란트의 등가응력(von-Mises stress)과 최대주응력이 높게 나타났다. 2. 수직하중보다 경사하중을 가할 경우 치조골과 임플란트의 등가응력과 최대주응력이 높게 나타났다. 3. 임플란트의 나사선 줄 수가 증가할수록 응력분산 효과가 커서 등가응력과 최대주응력의 크기가 감소되었다. 4. 치조골에 작용하는 최대주응력의 크기는 수직하중 시에나 경사하중 시에 3줄 나사선을 가진 임플란트가 가장 작고 다음으로 2줄 또는 1줄 나사선의 순으로 나타나 3줄 나사선의 경우가 가장 우수한 결과를 보였다. 결론: 이상의 결과는 3줄 나사선 임플란트가 1줄 및 2줄 나사선 임틀란트보다 응력분산 효과 면에서 우수하며, $10^{\circ}$ 이상 경사지게 식립된 경우에라도 나사선 경사각이 커지면서 줄 수가 증가할수록 치조골에서 발생하는 최대 주응력 값이 감소하므로 임플란트 나사선 줄 수와 경사각을 최적화함으로써 임플란트 응력분산에 도움이 될 수 있음을 시사하였다.

• 한국공작기계학회논문집
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• 제16권2호
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• pp.14-22
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• 2007

In this paper, the acoustic emission(AE) behaviors were investigated with single-and 2-spot resistance spot welded SPCC specimens. Test specimens were welded horizontally and/or vertically according to the rolling direction of base netal in 2-spot welding. In the case of 2-spot welding, when tensile-shear test has below amplitudes: crack initiation $50{\sim}60dB;$ tear fracture $40{\sim}50dB$. And when cross tensile test has below amplitudes: early stage $75{\sim}85dB;$ yielding point $65{\sim}75dB;$ post yielding $40{\sim}60dB;$ plug fracture $70{\sim}80dB\;or\;90{\sim}100dB$. Also, from the b-value that is slope of AE amplitude, we knew that there are lots of low amplitudes if b-value is big(i.e., tensile-shear $specimen{\rightarrow}tear$ fracture or shear fracture), and there are lots of high amplitudes if b-value is small(i.e.. cross tensile $specimen{\rightarrow}plug$ fracture). As the results of fiacture mechanism analyses through AE amplitude distributions, change of the b-value represented fracture patterns of materials. Correspondingly, low amplitude signals appeared in crack initiation, and high amplitude signals appeared in base metal fracture. We confirmed that these amplitude distributions represented the change or degradation of materials.

• 한국자동차공학회논문집
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• 제22권3호
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• pp.114-122
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• 2014

Sensor fusion is the one of the main research topics. It offers the highly reliable estimation of vehicle movement by processing and mixing several sensor outputs. But unfortunately, every sensor has drift which degrades the performance of sensor. It means a single degraded sensor output may affect whole sensor fusion system. Drift in most research is ideally assumed to be zero because it's usually a nonlinear model and has sample variation. Plus, it's very difficult for the acceleration to separate drift from the output signal since it contains many contributors such as vehicle acceleration, slope angle, pitch angle, surface condition and so on. In this paper, modified spline interpolation is introduced as a dynamic temperature compensation method covering sample variation. Using the last known output and the first initial output is suggested to build and update compensation factor. When the system has more compensation data, the system will have better performance of compensated output because of the regression compensation model. The performance of the dynamic temperature compensation system is evaluated by measuring offset drift between with and without the compensation.

• 지구물리와물리탐사
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• 제14권4호
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• pp.298-304
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• 2011

한국해양연구원에서는 2011년 4월에 쇄빙선 아라온호, Oceaneering사의 ROV (Remotely Operated Vehicle) 및 삼성분자력계(Three component vector magnetometer)를 이용하여 남서태평양 라우분지에 위치한 TA25해산 칼데라 서측 사면에 대하여 심해자력탐사를 실시하였다. 연구지역은 약 900 m ~ 1200 m의 수심대역을 보인다. 이 심해탐사를 위하여 국내 최초로 3000 m급 심해 삼성분자력계를 제작하였다. 자력계센서부분은 ROV의 상부에, 자력계로거부분은 ROV의 하부에 장착하였으며, ROV는 ROV의 정확한 위치를 알려주는 USBL (Ultra Short Base Line)과 고도계를 이용하여 정해진 측선을 따라 해저면에서 약 25 ~ 30 m의 수직 간격을 유지하며 이동하였다. 삼성분자력계는 자기장의 X(북쪽성분), Y(동쪽성분)과 Z(수직성분)의 벡터성분을 측정하므로 모션센서를 이용하여 ROV의 움직임(피치, 롤, 요)에 대한 보정을 실시하였다. 자력센서자료와 모션센서자료는 ROV의 광케이블과 아라온호의 네트워크를 이용하여 노트북에 저장되며 ROV의 정확한 위치자료인 USBL자료는 후처리를 통하여 병합하였다. 이렇게 획득한 심해 삼성분자력자료는 조사지역의 유망한 열수광상을 유추하는데 유용하게 활용될 것으로 판단된다.