• Transactions of the Korean Society of Mechanical Engineers A
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• v.38 no.6
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• pp.663-668
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• 2014

Mechanical and electrical devices in various forms are used in many different fields. These can be exposed to external environmental factors such as shock. Therefore, a shock test machine is commonly used to test these devices and evaluate their shock resistance. In this test, the break-down or permanent deformation and malfunction of inner parts due to a high stress or acceleration can be evaluated. As part of a shock test machine, a velocity generator is needed to create shocks between objects. In this study, a hydraulic velocity generator was conceptually designed and an AMESim model was developed to simulate the velocity under different conditions. Simulation results using this model were compared with the test results from a reduced-size velocity generator, and we designed a velocity generator that fits the target payload and velocity using the simulation results.

• The Journal of the Korea institute of electronic communication sciences
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• v.19 no.2
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• pp.409-416
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• 2024

With the expansion of floating-point operation requirements for fast high-speed data signal processing and logic operations, the speed of the floating-point operation unit is the key to affect system operation. This paper studies the performance characteristics of different floating-point multiplier schemes, completes partial product compression in the form of carry and sum, and then uses a carry look-ahead adder to obtain the result. Intel Quartus II CAD tool is used for describing Verilog HDL and evaluating performance results of the floating point multipliers. Floating point multipliers are analyzed and compared based on area, speed, and power consumption. The FMAX of modified Booth encoding with Wallace tree is 33.96 Mhz, which is 2.04 times faster than the booth encoding, 1.62 times faster than the modified booth encoding, 1.04 times faster than the booth encoding with wallace tree. Furthermore, compared to modified booth encoding, the area of modified booth encoding with wallace tree is reduced by 24.88%, and power consumption of that is reduced by 2.5%.

• The Transactions of the Korean Institute of Power Electronics
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• v.4 no.3
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• pp.231-239
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• 1999

An improved version of current-regulated delta modulator (CRDM) is investigated for the output cunent control of v voltage-source inverters that have transformer-coupled series resonant load and are operated at the resonant frequency. Conventional CRDM has not only CUlTent offset problem but also transformer flux saturation problem when i it is applied to induction heating systems that have transformel-coupled loads. To cope with these problems, the effect of flux saturation is analysed, and simple method to av이d the problem is proposed. And integral type of CRDM is a adopted to remove the cunent offset. The boundaries of integrator gain for stable operation is calculated using the c concept of sliding mode controL The validity of proposed strategy is vel퍼ed through simulations and prototype e experiments.

• Proceedings of the Korean Vacuum Society Conference
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• 2014.02a
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• pp.108.2-108.2
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• 2014

잔류가스측정 질량분석기(RGA)는 진공챔버 내부의 진공상태 이상유무, 공정상태 확인 및 주입가스 농도제어 등 여러 종류의 작업에 응용되고 있다. 반도체용 박막 제조공정(PVD, CVD)에서 챔버 내의 수분 혹은 불순물 가스의 정확한 모니터링은 반도체 품질향상에 매우 중요하다. 1 Pascal 진공도의 증착용 챔버에 RGA를 직접 장착하여 작동시키기 위해서는 저진공용 RGA가 사용되어야 한다. 10-3 Pascal에서 6m 자유운동거리를 갖는 질소분자는 1 Pascal에서는 6 mm로 짧은 자유운동거리를 갖는다. 따라서 1 Pascal 저진공영역에서 이온을 생성시키고 mass filter를 사용하여 질량분석을 하기 위해서는 이온원과 mass filter 길이가 자유운동거리 수준으로 작아져야한다. 저 진공영역에서는 검출기와 전자방출용 필라멘트가 저진공에서 작동되도록 일반고진공용 RGA와는 완전히 다르게 소형으로 설계 제작되어야 한다. 10-7 Pascal 이상의 초고진공에서 사용되는 RGA는 이온원이 작동할 때 발생하는 outgassing을 낮추도록 설계가 되어야 초고진공의 유지가 가능하다. 한국표준과학연구원에서 현재 개발 중인 일반고진공용 RGA를 소개하고 저진공용과 초고진공용 RGA의 설계특성을 발표한다.

• Journal of the Korean Society of Propulsion Engineers
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• v.12 no.4
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• pp.42-47
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• 2008

The power control system of Smart UAV is similar to the propeller pitch governing concept of turboprop aircraft. The pilot adjusts the engine power directly and the pitch governor controls the propeller pitch to maintain the propeller rotational speed. The electronic engine controller(EEC) of PW206C engine developed for helicopter is not fit for the power control concept of Smart UAV, and therefore the manual back-up system of PW206C engine is used for the engine power control of Smart UAV. Engine performance estimation program is used to predict the control range of power lever angle(PLA) according to the variation of engine output shaft speed, flight altitude and flight speed. These data provide a guide for the PLA control in manual mode operation.

• Proceedings of the Korean Vacuum Society Conference
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• 2013.08a
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• pp.105.1-105.1
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• 2013

Schottky Emitter (SE)는 미국 FEI의 L. W. Swanson 그룹이 개발하여 상용화시킨 전자원이며, 고분해능 전자현미경용 전자원 시장에서 가장 큰 점유율을 차지하고 있다. 상온에서 작동하는 cold field emitter (CFE)에 비해 휘도(brightness)가 10~100배 정도 낮으나, 10-10 Torr 영역의 초고진공에서도 수시간 미만의 방출전류 안정성을 가진 CFE에 비해 수개월이상 안정된 방출전류를 전자현미경에 제공하므로, 반도체 측정, 검사 등과 같이 고분해능과 안정성이 동시에 요구되는 분야에서는 SE전자원은 필수 요소가 되어있다. 현재 SE 전자원은 일본, 미국, 영국의 4개사가 과점하고 있는 상태이다. SE 전자원이 안정되게 작동하기 위해서는 10~10 Torr 영역의 초고진공 환경이 요구된다. 한국 전자현미경 업체는 국책과제 등을 통해 SE 전자총을 개발해 왔으나, 진공기술과 광학계 설계기술이 부족하여 안정된 SE 전자총의 개발에 성공하지 못하였다. 본 발표에서는 10~10 Torr 영역에서 200 microA 이상의 전류를 안정되게 방출하는 SE 전자총의 전자빔 방출 및 진공특성을 보고한다. 시뮬레이션을 통해 구한 전차총의 전자원 위치 변화, 건렌즈 초점거리, 수차 등의 광학특성을 보여준다. 전자총을 전자현미경 경통에 탑재하고 제어하기 위해서는 전자총뿐만 아니라 전자현미경 전체의 광학특성을 이해할 필요가 있다. 전자총을 현미경에 통합 제어하기 위한 기술과제에 대해서도 간략히 보고한다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.37 no.3
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• pp.240-247
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• 2009

Wind tunnel test for Electro-Optical Targeting System(EOTS) has been conducted to investigate the aerodynamic characteristics, especially the torque characteristics of the rotating parts to insure the enough actuator power during the actual operation. The influence of EOTS's complex configuration, such as the observation window, has been investigated by comparing with the results of the simplified models made of half sphere and the cylinder. It has been found that the position of the observation window of EOTS has an effect on surface pressure distribution and the torque characteristics of the rotating observation part.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2011.11a
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• pp.515-519
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• 2011

Structural tests for the mixing head of a 75tonf class thrust chamber were performed to verify structural stability. The mixing head of a thrust chamber is loaded by high pressure with regeneratively cooled fuel and cryogenic liquid oxygen(LOx) as well as it transfers thrust load generated by liquid rocket engine. Therefore structural stability of mixing head is a very important factor to work without any plastic deformation or structural failure. In this study, two mixing heads were manufactured using different welding methods, Tungsten Inert Gas(TIG) welding and Electron Beam Welding(EBW) and evaluated a structural stability. The results of structural tests showed that the mixing head assembled by EBW can withstand the applied design load without any structural failures and be structurally more stable than that of TIG welding.

• Journal of IKEEE
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• v.22 no.2
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• pp.393-401
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• 2018

In this paper, a rectifier for WPC / A4WP wireless power transmission is designed. The proposed rectifier supports both WPC (Wireless Power Consortium) and A4WP (Alliance For Wireless Power) and is designed with full-bridge rectifier. WPC transmits power at the frequency of 100kHz to 205kHz and A4WP at the frequency of 6.75MHz. Since the bridge rectifier uses a MOSFET instead of a diode, the reverse current flows and the efficiency is affected if the output voltage is higher than the input voltage. Therefore, we added the reverse current detector that detects the current flowing through the MOSFET and shut off the reverse current. The frequency discriminator is used because the rectifier has different frequency band. The proposed rectifier was designed using $0.35{\mu}m$ CMOS high voltage process. The input voltage is up to 18V and the rectifier operates at 100kH to 205kHz, 6.78MHz frequency. The maximum efficiency is 94.8% and the maximum power transfer is 5.78W.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 1995.04a
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• pp.45-50
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• 1995

본 연구에서는 기존에 널리 사용되고 있는 스카이훅 제어 알고리즘(skyhook control algorithm)[3]을 바탕으로 확장 개발된 모드 스카이훅 제어(mode skyhook control) 개념 및 주파수 감응식 제어(frequency dependent control)개념[4][5]을 실용화하기 위하여 응답속도가 20msec이하의 비교적 빠른 응답 속도를 갖는 전자기식 작동기 (electro-magnetic actuator)에 의해 가변되는 4단 반능동형 가변 댐퍼 시스템을 개발한 후, 다음과 같은 성능의 향상을 시험결과를 통하여 보이고자 한다. -저속에서의 승차감 향상과 고속에서의 주행 안정성 향상 -커브 주행 또는 급격한 핸들 작동시의 롤안정성 (rolling stability) 향상 -제동 및 급발진시의 차체 피칭 운동 방지 (anti-dive, anti-squat)