• Title/Summary/Keyword: Pulse gun

Search Result 107, Processing Time 0.03 seconds

900MHz RFID Passive Tag Frontend Design and Implementation (900MHz 대역 RFID 수동형 태그 전치부 설계 및 구현)

  • Hwang, Ji-Hun;Oh, Jong-Hwa;Kim, Hyun-Woong;Lee, Dong-Gun;Roh, Hyoung-Hwan;Seong, Yeong-Rak;Oh, Ha-Ryoung;Park, Jun-Seok
    • The Journal of Korean Institute of Communications and Information Sciences
    • /
    • v.35 no.7B
    • /
    • pp.1081-1090
    • /
    • 2010
  • $0.18{\mu}m$ CMOS UHF RFID tag frontend is presented in this paper. Several key components are highlighted: the voltage multiplier based on the threshold voltage terminated circuit, the demodulator using current mode, and the clock generator. For standard compliance, all designed components are under the EPC Global Class-1 Generation-2 UHF RFID protocol. Backscatter modulation uses the pulse width modulation scheme. Overall performance of the proposed tag chip was verified with the evaluation board. Prototype Tag Chip dimension is neary 0.77mm2 ; According to the simulation results, the reader can successfully interrogate the tag within 1.5m. where the tag consumes the power about $71{\mu}W$.

Experimental Study on the Combustion Stability of Full Scale Rocket Combustor (실물형 액체로켓 연소기의 연소안정성에 대한 시험적인 고찰)

  • Lee Kwang-Jin;Seo Seong-Hyeon;Kang Dong-Hyeuk;Song Ju-Young;Lim Byoung-Jik;Han Yeoung-Min
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2005.11a
    • /
    • pp.240-246
    • /
    • 2005
  • A series of combustion tests of a 30-tonf-class full scale liquid rocket thrust chamber under development has been carried out to verify its design. The test results revealed decent performance in the aspects of efficiency. The combustion stability is one of the most important parameters of liquid rocket engine in addition to the efficiency. Assessment tests of combustion stability must be accomplished to confirm the possibility of combustion instability due to spontaneous or external disturbances. The combustion stability rating tests of the full scale thrust chamber with temporary baffles made of stainless steel were carried out utilizing pulse guns to estimate combustion stability characteristics. The tests results show highly stable combustion stability characteristics. The outcome acquired from the present experimental study will be used to design an actively cooled baffle that can survive for the life time operation of the thrust chamber.

  • PDF

A Model for Nowcasting Commodity Price based on Social Media Data (소셜 데이터 기반 실시간 식자재 물가 예측 모형)

  • Kim, Jaewoo;Cha, Meeyoung;Lee, Jong Gun
    • Journal of KIISE
    • /
    • v.44 no.12
    • /
    • pp.1258-1268
    • /
    • 2017
  • Capturing real-time daily information on food prices is invaluable to help policymakers and development organizations address food security problems and improve public welfare. This study analyses the possible use of large-scale online data, available due to growing Internet connectivity in developing countries, to provide updates on food security landscape. We conduct a case study of Indonesia to develop a time-series prediction model that nowcasts daily food prices for four types of food commodities that are essential in the region: beef, chicken, onion and chilli. By using Twitter price quotes, we demonstrate the capability of social data to function as an affordable and efficient proxy for traditional offline price statistics.

A Study on Characteristics of Temperature and Radicals in Laminar Non-premixed H2/N2 Flame Using LIPF and LRS (레이저 유도 선해리 형광법과 래일레이 산란법에 의한 층류 비예혼합 수소/질소 화염의 온도 및 라디칼 특성에 관한 연구)

  • Jin, Seong Ho;Park, Kyoung Suk;Kim, Gun Hong;Kim, Gyung Soo
    • Transactions of the Korean hydrogen and new energy society
    • /
    • v.13 no.3
    • /
    • pp.169-180
    • /
    • 2002
  • Rayleigh scattering and laser induced predissociative fluorescence are used to obtain two-dimensional images of temperature and species concentration in a laminar non-premixed flame of a diluted hydrogen jet. Rayleigh scattering cross-sections are experimentally obtained at 248nm. Planar images of OH and $O_2$ with tunable KrF excimer laser which has a) $0.5cm^{-1}$ linewidth, b) 0.5nm tuning range, c) 150mJ pulse energy, and d) 20ns pulse width are obtained to determine spatial distributions of OH and $O_2$. The technique is based on planar laser induced predissociative fluorescence (PLIPF) in which collisional quenching is almost avoided because of the fast predissociation. Dispersed LIPF spectra of OH and $O_2$ are also measured in a flame in order to confirm the excitation of single vibronic state of OH and $O_2$. OH and $O_2$ are excited on the $P_2$(8) and $Q_1$(11) line of the $A^2{\Sigma}^{+}({\nu}^{'}=3)-X^{2}{\Pi}({\nu}^{''}=o)$ band and R(17) line of the Schumann-Runge band $B^{3}{\Sigma}_{u}{^-}(\nu^{'}=0)-X^{3}{\Sigma}_{g}{^-}({\nu}^{''}=6)$, respectively. Fluorescence spectra of OH and Hot $O_2$ are captured and two-dimensional images of the hydrogen flame field are successfully visualized.

A Low-Power MPPT Interface for DC-Type Energy Harvesting Sources (DC 유형의 에너지 하베스팅 자원을 활용한 저전력의 MPPT 인터페이스)

  • Jo, Woo-Bin;Lee, Jin-Hee;Yu, Chong-Gun
    • Proceedings of the Korean Institute of Information and Commucation Sciences Conference
    • /
    • 2018.10a
    • /
    • pp.35-38
    • /
    • 2018
  • This paper describes a low-power MPPT interface for DC-type energy harvesting sources. The proposed circuit consists of an MPPT controller, a bias generator, and a voltage detector. The MPPT controller consists of an MPG (MPPT Pulse Generator) with a schmitt trigger, a logic gate operating according to energy type (light, heat), and a sample/hold circuit. The bias generator is designed by employing a beta multiplier structure, and the voltage detector is implemented using a bulk-driven comparator and a two-stage buffer. The proposed circuit is designed with $0.35{\mu}m$ CMOS process. The simulation results show that the designed circuit consumes less than 100nA of current at an input voltage of less than 3V and the maximum power efficiency is 99.7%. The chip area of the designed circuit is $1151{\mu}m{\times}940{\mu}m$.

  • PDF

Simultaneous Removal Characteristics of NOx, SOx from Combustion Gases using Pulse Corona induced Plasma Chemical Processing (PPCP에 의한 연소가스 중 NOx, SOx 동시제거 특성)

  • Park, Jae-Yoon;Koh, Yong-Sul;Jung, Jang-Gun;Kim, Jung-Dal
    • Journal of Korean Society of Environmental Engineers
    • /
    • v.22 no.2
    • /
    • pp.211-216
    • /
    • 2000
  • In this paper, experimental investigations were carried out to remove NOx, SOx simultaneously from a simulated combustion flue gas [$NO(0.02%)-SO_2(0.08%)-CO_2-Air-N_2$] by using a pulse corona induced plasma chemical processing. Discharge domain of wire-cylindrical plasma reactor was separated from a gas flow duct to avoid unstable discharge by aerosol particle deposited on discharge electrode and grounded electrode. The NOx, SOx removal was experimentally investigated by a reaction induced to ammonium nitrate, ammonium sulfate using a low price of aqueous NaOH solution and a small quantity of ammonia. Volume percentage of aqueous NaOH solution used was 20% and $N_2$ flow rate was $2.5{\ell}/min$ for bubbling aqueous NaOH solution. Ammonia gas(l4.82%) balanced by argon was diluted by air and was introduced to a main simulated flue gas duct through $NH_3$ injection system which was in downstream of reactor. The $NH_3$ molecular ratio(MR) was determined based on [$NH_3$] and [$NO+SO_2$]. MR is 1.5. The NOx removal rates increased in the order of DC, AC and pulse, but SOx removal rates was not significantly effected by source of electricity. The NOx removal rate slightly decreased with increasing initial concentration. but SOx removal rate was not significantly affected by initial concentration. The NOx, SOx removal rates decreased with increasing gas flow rate.

  • PDF

Effect of Different Misfired Source on Seismic Survey Quality (불발 음원이 탄성파탐사 성능에 미치는 영향)

  • 유해수;장재경;양승진
    • The Journal of the Acoustical Society of Korea
    • /
    • v.18 no.7
    • /
    • pp.75-79
    • /
    • 1999
  • The beam patterns of source array and changes in the far-field signatures are compared and analyzed each other in order to identify the seismic capability affected by the misfired source at the multi-channel seismic source array. In the primary pulse amplitude of far-field signature, the 66% of seismic capacity are sustained if approximately 40% of source are misfired among whole gun volume. When the sources with the same distances are misfired at the 154㎐, the beam width of the long- and wide-array which is identical regardless of arraying pattern. The beam width has a tendency to narrow now from 41 to 34 according to increase the volume of misfired source at the long-array beam pattern. Therefore, the source array of small volume are suitable for the shallow seismic survey because of producing adequate beam patterns with narrow beam width.

  • PDF

A High-Efficiency High-Power Step-Up Converter with Low Ripple Content

  • Kang Jeong-il;Roh Chung-Wook;Moon Gun-Woo;Youn Myung-Joong
    • Proceedings of the KIPE Conference
    • /
    • 2001.10a
    • /
    • pp.708-712
    • /
    • 2001
  • A new phase-shifted parallel-input/series-output (PI SO) dual inductor-fed push-pull converter for high-power step­up applications is proposed. This converter is operated at a constant duty cycle and employs an auxiliary circuit to control the output voltage with a phase-shift between the two modules. It features a voltage conversion characteristic which is linear to changes in the control input, and high step-up ratio with a greatly reduced switch turn-off stress resulting in a significant increase in the converter efficiency. It also shows a low ripple content and low root-mean-square (RMS) current in the output capacitor. The operational principle is analyzed and a comparative analysis with the conventional pulse-width-modulated (PWM) PISO dual inductor-fed push-pull converter is presented. A 50kHz, 800W, 350Vdc prototype with an input of 20-32Vdc has also been constructed to validate the proposed converter. The proposed converter compares favorably with the conventional counterpart and is considered well suited to high-power step-up applications.

  • PDF

Development of Mixed Hydrogen Gas Generator Power Conversion System (Mixed Hydrogen Gas Generator용 전력변환장치 개발)

  • Jung, Jang-Gun;Mun, Sang-Pil;Cho, Gil-Je;Kim, Chang-Il
    • Proceedings of the KIEE Conference
    • /
    • 2007.11c
    • /
    • pp.88-92
    • /
    • 2007
  • In this paper, the basic experiment, electrolytic cell design and basic manufacturing have been made to interpret the characteristics of Hydrogen-Oxygen-Gas-Generator. As for the detailed matters, the data research on basic technology on Hydrogen-Oxygen-Gas and analysis on characteristics of Hydrogen-Oxygen-Gas from basic experiment. Also the experiment of characteristics and comparative evaluation between constant current source using IGBT converter from existing method and constant current source using new phase shift PWM control method converter. As results when it has injected constant DC current, we has compared Gas quantities by variable ripple frequencies using phase shift PWM control method converter. Therefore, in linear region, it has not different Gas quantities by constant DC current and by phase shift PWM control method converter. Also, it has increased Gas quantities wilder linear region when put ripple frequency at saturation region. Through, Gas quantities and input power, it has acquired higher input power per Gas quantities at put pulse curren. Therefore, when designing converter or inverter for electrolysis, which has ripple current.

  • PDF

Combustion Stability Evaluation of 30 ton-f Class Liquid Rocket Engine Combustor (30톤급 엑체로켓엔진 연소기의 연소안정성 평가)

  • Lim, Byoung-Jik;Lee, Kwang-Jin;Kim, Mun-Ki;Kang, Dong-Hyuk;Yang, Seung-Ho;Seo, Seong-Hyeon;Han, Yeoung-Min;Choi, Hwan-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
    • /
    • 2008.05a
    • /
    • pp.163-167
    • /
    • 2008
  • This paper presents pressure fluctuation characteristics of a 30 ton-f class liquid rocket engine combustor. Combustion stability of the combustor was evaluated using the results 46 firing tests performed with a varying O/F ratio and chamber pressure. The RMS value of pressure fluctuation during the steady state combustion was less than 2.6% of the static chamber pressure, demonstrating static stability of the combustion phenomenon. The decay time of pressure fluctuation caused by forced disturbance of a pulse gun was found to be less than 3.5 msec verifying dynamic stability of the combustor.

  • PDF