• Journal of the Korean Society of Propulsion Engineers
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• v.14 no.6
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• pp.60-68
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• 2010

In this study, the conventional plane tip, double squealer tip, and various groove tip blades were tested in a linear cascade in order to measure the effect of the tip shapes on tip surface heat transfer coefficient distributions. Detailed heat transfer coefficient distributions were measured using a hue-detection based transient liquid crystals technique. Two tip gap clearances of 1.5% and 2.3% of blade span were investigated and the Reynolds number based on cascade exit velocity and chord length was $2.48{\times}10^5$. Results showed that the overall heat transfer coefficients on the tip surface with various grooved tips were lower than those with plane tip blade. The overall heat transfer coefficient on grooved along suction side tip was lower than that on the squealer tip.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2010.05a
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• pp.311-318
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• 2010

In this study, the conventional plane tip, double squealer tip, and various groove tip blades were tested in a linear cascade in order to measure the effect of the tip shapes on tip surface heat transfer coefficient distributions. Detailed heat transfer coefficient distributions were measured using a hue-detection based transient liquid crystals technique. Two tip gap clearances of 1.5% and 2.3% of blade span were investigated and the Reynolds number based on cascade exit velocity and chord length was $2.48{\times}10^5$. Results showed that the overall heat transfer coefficients on the tip surface with various grooved tips were lower than those with plane tip blade. The overall heat transfer coefficient on grooved along suction side tip was lower than that on the squealer tip.

• Proceedings of the Korean Information Science Society Conference
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• 2008.06c
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• pp.478-481
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• 2008

기존 핑거 트래킹(Finger Tracking)을 수행하는데 있어 핑거팁(Finger-tip)을 구하는 방법 중 가장 일반적인 방법은 먼저 피부색 정보(Skin Color)를 추출한다. 그 다음 블럽(Blob) 함수의 블럽 컬러링(Blob Coloring) 알고리즘을 통하여 피부 윤곽선(Skin Contour)를 구하고, 그 중 가장 최상위 점을 핑거팁으로 정한다. 그러나 이 방법은 밴딩 핑거(Bending Finger) 상태에서 핑거팁 위치를 측정할 때 실제 손가락 끝이 아닌 잘못된 위치를 잡는 문제점을 가지고 있다. 본 논문에서 제안하는 방법은 밴딩 핑거 상태에서의 핑거 트래킹시 잘못된 핑거팁을 측정하는 문제점을 사용자들의 성향을 통해 미리 예상하고 보정함으로써 성능을 향상시키고자 한다.

• Proceedings of the Korean Vacuum Society Conference
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• 2010.02a
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• pp.352-352
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• 2010

일반적인 근접장 현미경은 광섬유 팁 (tip) 끝에 수십 nm 크기의 구멍을 이용하여 근접장을 발생시키거나 측정한다. 근접장은 전파되는 빛보다 미세한 구조의 정보를 반영하게 되는데 수십 나노미터의 구멍대신 FRET (fluorescence resonance energy transfer)이라는 현상을 근접장 현미경에 적용하고자 한다. 10 nm 이내의 거리에서 상호작용을 하는 이 현상을 이용하여 광학적 분해능을 향상시킬 수 있다. FRET 현상의 도우너(donor)로서는 양자점을 사용하였으며 억셉터(acceptor) 로서는 Cy5 염료를 사용하였다. 팁으로는 광섬유를 에칭한 팁에 Cy5 염료를 코팅한 팁과 광섬유의 코어(core) 부근에 양자점이 포함된 광 폴리머를 응고시켜서 만들어진 팁을 사용하였다. 팁에 위치한 도우너와 시료로 사용되는 억셉터를 FRET 상호 작용 거리 내로 접근시키기 위하여 tuning fork를 이용한 shear force control을 사용하였다. 한 점에서의 접근 과정에서 FRET의 현상의 특징으로서 도우너인 양자점의 형광이 약해지고 Cy5의 형광이 강해지는 것을 측정하였다. 또한, 양자점을 Cy5 염료에 근접시켰을 때 발광 생존시간 (lifetime)이 짧아지는 것을 관찰하여 FRET 현상을 재확인 하였다.

• Proceedings of the Korean Reliability Society Conference
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• 2004.07a
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• pp.139-145
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• 2004

용접산업이 발전함에 따라 가스메탈아크 용접에서 고내마모성의 콘택트 팁이 요구되어지고 있다. 현재 국내외에서는 콘택트팁에 대한 수명평가 기준이 없으며, 일부 업계에서 자체 규격을 제정하여 운용하고 있지만 근거가 명확하지 않다. 따라서 본 연구에서는 콘택트팁의 신뢰성 평가기준을 제정하고자 하였다. 팁의 주요 파손기구로는 고온 마찰마모, 전기적 에로존, 번백 등이 있다. 신뢰성 평가는 경도 시험, 열처리 후 경도, 용접 마모, 전기전도도를 시험으로 구성되었다. 팁의 수명은 마모가 45%에 도달했을 경우 송급된 와이어 총 길이로 하였으며, 4시간까지 마모시험 한 결과를 근거로하여 한계수명을 추정하였다. 본 연구에서는 세 가지 조성의 다섯 가지의 콘택트팁에 대하여 4시간동안 내마모성 실험을 하였으며, 마모정도는 1시간 단위로 면적비를 백분율로 환산하여 측정하였다. 실험 결과 가공경화형팁은 1시간이내에 재결정 및 입자성장에 의한 경도 저하로 가공경화가 팁 수명에 지속적 영향을 주지 못하였다. 반면, 석출경화형팁은 석출경화 효과가 지속되어 가공경화형팁보다 수명이 향상 되었다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2010.11a
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• pp.33-36
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• 2010

Lots of studies about turbine loss have been done especially about tip leakage loss. But these studies deals with small tip clearances which is less than 5 percent chord. Now, like turbopumps, small turbines have larger tip clearance and it is hardly found related papers in open literature. On this study, with varying tip clearance 1% to 20% chord, loss is measured under inlet velocity at 30m/s and Reynolds number based on chord at 210000. It is found that maximum loss coefficient is 0.113 at 10% clearance, and when tip clearance is larger than 10%, loss is not linearly increased anymore.

• 전자공학회논문지 IE
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• v.44 no.3
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• pp.1-5
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• 2007

A new field emission tip array was realized by Ti silicidation of Ti coated Si tip, which has long term durability, chemical stability, and high emission current density. The fabricated Ti silicided FE tip array under high vacuum condition of about $10^{-8}Torr$ shows that the turn-on voltage is about 40V and the emission current is about $69{\mu}A$ when the bias of 150V is applied between anode and cathode of $100{\mu}m$ distance.

• The Journal of Korean Academy of Prosthodontics
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• v.52 no.3
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• pp.177-185
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• 2014

Purpose: This study is designed to investigate the various impacts of different types of scaler tips such as cooper alloy base tip and the others on the surface roughness of teeth and implant by the method which is currently in clinical use. Materials and methods: Four different types of disc shaped porcelain, titanium, zirconia, and Type III gold alloy dental materials sized 15 mm diameter, 1.5 mm thickness were used for the experiment. Plastic hand curette (Group PS), cooper alloy new tip (Group IS), and stainless steel tip (Group SS) were used as testing appliances. A total of 64 specimens were used for this study; Four specimens for each material and appliance group. Surface roughness was formed with 15 degree angle in ultrasonic scaler tip and with 45 degree angle in hand curette of instrument tip and the specimen surface with 5 mm long, one horizontal-reciprocating motion per second for 30 seconds by 40 g force. To survey the surface roughness of each specimen, a field emission scanning electron microscope, an atomic force microscope, and a surface profiler were used. (Ra, ${\mu}m$). Results: According to SEM, most increased surface roughness was observed in SS group while IS groups had minimal roughness change. Measurement by atomic force microscope presented that the surface roughness of SS group was significantly greater than those of PS, IS and control groups in the type III gold alloy group (P<.05). IS group showed lesser surface roughness changes compared to SS group in porcelain and gold alloy group (P<.05). According to surface profiler, surface roughness of SS group showed greater than those of PS, IS and control groups and IS group showed lesser than those of SS group in all specimen groups. Type III gold alloy group had large changes on surface roughness than those of porcelain, titanium, zirconia (P<.05). Conclusion: The result of this study showed that newly developed copper alloy scaler tip can cause minimal roughness impacts on the surface of implant and dental materials; therefore this may be a useful alternative for prophylaxis of implant and restored teeth.

• Korean Journal of Optics and Photonics
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• v.10 no.4
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• pp.267-272
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• 1999

We attached a fiber tip on the branch of a quartz crystal oscillator in order to make a feedback control system for near field optical microscope. The electrical impedance of the quartz crystal oscillator depends on the distance between the surface of the sample and the tip caused by the surface damping. Using this method, we can directly monitor the distance between the sample and the tip without inserting extra beam which might give extra optical noise. We characterize the XY scanning resolution and the amplitude of the vibrating tip and the Z-dependent decay of the evanescent wave.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2008.11a
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• pp.145-148
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• 2008

Korea Aeronautics Research Institute (KARI) is developing a turbo pump that has 1-stage impulse turbine and relatively high tip clearance for safety. The objective of this research is to investigate the effect of reaction on tip clearance loss in axial turbines. Both cascades were tested in a subsonic wind tunnel. In each cascade, total pressure was measured for tip clearance ranging from 1% to 20% of chord. In results, increasing tip clearance, total pressure loss in reaction turbines is continually increased but impulse turbines keep almost same level of mass averaged total pressure loss. When tip clearance becomes more than 10% of chord, mass-averaged total pressure loss in impulse turbines is less than in reaction. This means that when tip clearance is more than 10% of chord, impulse turbines have better efficiency than reaction turbines.