• 한국초전도ㆍ저온공학회논문지
• /
• 제13권4호
• /
• pp.30-35
• /
• 2011

This paper describes experimental study and performance improvement of 2 stage Gifford-McMahon (G-M) type pulse tube cryocooler for cryopump. The objective of this study is to improve the efficiency of 2 stage pulse tube cryocooler for substituting 2 stage G-M cryocooler used in cryopump. The target cooling capacities are 5 W at 20 K and 35 W at 80 K for the $1^{st}$ and the $2^{nd}$ stage, respectively. These values are good cooling capacities for vacuum level in medium size ICP 200 cryopump. Design of the 2 stage pulse tube cryocooler is conducted by FZKPTR(Forschungs Zentrum Karlsruhe Pulse Tube Refrigerator) program. In order to improve the performance of 2 stage pulse tube cryocooler, U-type pulse tube cryocooler is fabricated and connecting tubes are minimized for reducing dead volumes and pressure losses. Also, to get larger capacities, orifice valves and double inlet valves are optimized and the compressor of 6 kW is used. On the latest unit, the lowest temperatures of 2 stage pulse tube cryocooler are 42 K ($1^{st}$ stage) and 8.3 K ($2^{nd}$ stage) and the cooling capacities are 40 W at 82.9 K ($1^{st}$ stage) and 10 W at 20.5 K ($2^{nd}$ stage) with 6.0 kW of compressor input power. This pulse tube cryocooler is suited for commercial medium size cryopump. In performance test of cryopump with 2 stage pulse tube cryocooler, pumping speed for gaseous nitrogen is 4,300 L/s and the ultimate vacuum pressure is $7.5{\times}10^{-10}$ mbar.

• 한국유체기계학회 논문집
• /
• 제14권3호
• /
• pp.23-27
• /
• 2011

Due to a roots type medium vacuum pump is operated in condition of $1{\sim}10^{-3}$ torr vacuum, it could be applied for production and process of industrial parts, such as precise processing, vaporization, enrichment, separation, casting, metaling, welding, transportation. Therefore, the demand of this pump is increasing nowadays in our industrial markets of semiconductor, electric, electronic, automobile, material, environmental and transporting industries. However, the pumps are almost imported, because the domestic pumps are inferior in fields of vacuum range as under $10^{-1}$torr, relevant techniques(design, fabrication, casting, test, etc.) to the imported ones. In this study, essential parts of the development pump are designed with using of CFD and 3D decodes, FEM for analysing strength and deformation, generated heat, vibration and noise control, and are casted with using of mechanochemistry techniques for decreasing of weights, increasing of heat resistances and abrasion durability of materials for pump caing and impellers especially. Besides, in order to achieve ultimate vacuum around $10^{-3}$torr, this pump is composed of 6 stages, among which 1st stage is operated separately from remained stages. Additionally, a test rig for prototype pumps(300$m^3/h$ and 2,500$m^3/h$) is designed and procured as to apply for multi-staged rootz type vacuum pump, with modification of the test method recommended by KS B 6314 "Positive-displacement oil-sealed rotary vacuum pumps".

• 한국산업융합학회 논문집
• /
• 제20권2호
• /
• pp.105-113
• /
• 2017

Recently the direct injection diesel engine is the most efficient one available for road vehicles, so this fundamental advantage suggests the compression injection diesel engine are a wise choice for future development efforts. The compression ignition diesel engine, with its bigger compression ratios if compared to the SI engine, offers a higher thermodynamic efficiency, also additionally the diesel engine with its less pumping losses due to the throttled intake charge as in a SI engine has higher fuel economy. But the largest obstacle to the success of this engine is meeting emission standards for Nitric oxides and particulate matter while maintain fuel consumption advantage over currently available engines. Thus its use should be largely promoted, however, diesel engine emits more Nitric oxides and particulate matter than other competing one. There has been a trade-off between PM and NOx, so efforts to reduce NOx have increased PM and vice versa, but trap change this situation and better possibility emerge for treating NOx emission with engine related means, such as injection timing, equivalence ratio, charge composition, and engine speed. The common rail direct injection system is able to adjust the fuel injection timing in a compression ignition engine, so this electronically controlled injection system can reduce the formation of NOx gas without increase in soot. In this study it is designed and used the engine test bed which is installed with turbocharge and intercooler. In addition to equipped using CRDI by controlling injection timing with mapping modulator, it has been tested and analyzed the engine performance, combustion characteristics, and exhaust emission as operating parameters.

• Journal of applied mathematics & informatics
• /
• 제41권1호
• /
• pp.51-70
• /
• 2023

The flow of an incompressible Ellis fluid in an inclined asymmetric channel, driven by peristaltic waves was studied under low Reynolds number and long wavelength assumptions. The wave on each side of the channel are assumed to be an infinite train of sinusoidal waves, both having the same constant wave speed and wavelength however, they vary in wave amplitude, channel half width and phase angle. We derived expressions for the axial and transverse velocities, volume flow rate, pressure rise per unit wavelength and streamlines. The effects of varying the wave amplitudes, the phase angle, the channel width, the angle of inclination of the channel as well as the fluid parameters on the flow were analyzed. Trapping conditions were determined and the presence of reflux highlighted using the streamlines for the necessary channel and fluid conditions. By varying the fluid parameters, changes in the fluid that deviated from the Newtonian case resulted in a reduction in the axial velocity in the neighborhood of the center of the channel and a simultaneous increase in the velocity at the periphery of the channel. A nonlinear relation was observed with the pressure rise and the volume flow rate. This nonlinear relation is more pronounced with an increase in the absolute value of the volume flow rate. For Newtonian fluids a linear relation exists between these two variables. The fluid parameters had little effects on the streamlines. However, variations of the wave amplitudes, volume flow, channel width and phase angle had greater effects on the streamlines and hence the trapped region.

• 한국전기전자재료학회논문지
• /
• 제37권4호
• /
• pp.382-393
• /
• 2024

유체 디스펜싱(fluid dispensing) 방식인 Microplotter 시스템은 압전 소자를 통한 초음파 펌핑(pumpin)을 기반으로 유체를 분사한다. 이 기법은 넓은 범위의 점도를 가진 다양한 물질들이 마이크로 사이즈로 프린팅 되는 것을 가능하게 한다. 본 논문에서는 디스펜서 프린팅 기술에 대해 소개하고 장비를 이용한 다양한 공정을 이해 및 응용에 목적을 두고 있다. 또한, 분사 강도, 분사 시 팁의 높이, 분사 속도와 같은 매개변수들을 조절하여 장비의 최적화 방법에 대해 설명하고자 한다. 금속 나노 입자, 탄소나노튜브, DNA, 단백질 등 광범위한 유체와 호환된다는 Microplotter의 장점을 이용함으로써 인쇄전자, 생명공학, 화학공학 등 다양한 분야에서 활용될 것으로 기대된다.

• Journal of Biosystems Engineering
• /
• 제3권1호
• /
• pp.1-19
• /
• 1978

Power tiller is a major unit of agricultural machinery being used on farms in Korea. About 180.000 units are introduced by 1977 and the demand for power tiller is continuously increasing as the farm mechanization progress. Major farming operations done by power tiller are the tillage, pumping, spraying, threshing, and hauling by exchanging the corresponding implements. In addition to their use on a relatively mild slope ground at present, it is also expected that many of power tillers could be operated on much inclined land to be developed by upland enlargement programmed. Therefore, research should be undertaken to solve many problems related to an effective untilization of power tillers on slope ground. The major objective of this study was to find out the travelling and tractive characteristics of power tillers being operated on general slope ground.In order to find out the critical travelling velocity and stability limit of slope ground for the side sliding and the dynamic side overturn of the tiller and tiller-trailer system, the mathematical model was developed based on a simplified physical model. The results analyzed through the model may be summarized as follows; (1) In case of no collision with an obstacle on ground, the equation of the dynamic side overturn developed was: $$\sum_n^{i=1}W_ia_s(cos\alpha cos\phi-{\frac {C_1V^2sin\phi}{gRcos\beta})-I_{AB}\frac {v^2}{Rr}}=0$$ In case of collision with an obstacle on ground, the equation was: $$\sum_n^{i=1}W_ia_s\{cos\alpha(1-sin\phi_1)-{\frac {C_1V^2sin\phi}{gRcos\beta}\}-\frac {1}{2}I_{TP} \( {\frac {2kV_2} {d_1+d_2}\)-I_{AB}{\frac{V^2}{Rr}} \( \frac {\pi}{2}-\frac {\pi}{180}\phi_2 \} = 0 $$ (2) As the angle of steering direction was increased, the critical travelling veloc\ulcornerities of side sliding and dynamic side overturn were decreased. (3) The critical travelling velocity was influenced by both the side slope angle .and the direct angle. In case of no collision with an obstacle, the critical velocity $V_c$ was 2.76-4.83m/sec at $\alpha=0^\circ$, $\beta=20^\circ$ ; and in case of collision with an obstacle, the critical velocity $V_{cc}$ was 1.39-1.5m/sec at $\alpha=0^\circ$, $\beta=20^\circ$ (4) In case of no collision with an obstacle, the dynamic side overturn was stimu\ulcornerlated by the carrying load but in case of collision with an obstacle, the danger of the dynamic side overturn was decreased by the carrying load. (5) When the system travels downward with the first set of high speed the limit {)f slope angle of side sliding was $\beta=5^\circ-10^\circ$ and when travels upward with the first set of high speed, the limit of angle of side sliding was $\beta=10^\circ-17.4^\circ$ (6) In case of running downward with the first set of high speed and collision with an obstacle, the limit of slope angle of the dynamic side overturn was = $12^\circ-17^\circ$ and in case of running upward with the first set of high speed and collision <>f upper wheels with an obstacle, the limit of slope angle of dynamic side overturn collision of upper wheels against an obstacle was $\beta=22^\circ-33^\circ$ at $\alpha=0^\circ -17.4^\circ$, respectively. (7) In case of running up and downward with the first set of high speed and no collision with an obstacle, the limit of slope angle of dynamic side overturn was $\beta=30^\circ-35^\circ$ (8) When the power tiller without implement attached travels up and down on the general slope ground with first set of high speed, the limit of slope angle of dynamic side overturn was $\beta=32^\circ-39^\circ$ in case of no collision with an obstacle, and $\beta=11^\circ-22^\circ$ in case of collision with an obstacle, respectively.

• 대한전자공학회논문지TC
• /
• 제42권7호
• /
• pp.35-40
• /
• 2005

본 논문에서는 900MHz 대역 중저속 무선 통신용 칩에 이용되는 3차 ${\Delta}{\sum}$ modulator를 사용한 Fractional-N PLL 주파수 합성기를 설계 및 제작하였다 우수한 위상노이즈 특성을 얻기 위해 노이즈 특성이 좋은LC VCO를 사용하였다. 그리고 고착시간을 줄이기 위해서 Charge Pump의 펌핑 전류를 주파수 천이 값에 따라 조절할 수 있도록 제작하였고 PFD의 참조 주파수를 3MHz까지 높였다. 또한 참조 주파수를 높이는 동시에 PLL의 최소 주파수 천이 간격을 10KHz까지 줄일 수 있도록 하기위하여 36/37 Fractional-N 분주기를 제작하였다. Fractional Spur를 줄이기 위해서 3차 ${\Delta}{\sum}$ modulator를 사용하였다. 그리고 VCO, Divider by 8 Prescaler, PFD, 및 Charge Pump는 0.25um CMOS공정으로 제작되었으며, 루프 필터는 외부 컴포넌트를 이용한 3차RC 필터로 제작되었다. 그리고 Fractional-N 분주기와 3차 ${\Delta}{\sum}$ modulator는 VHDL 코드로 작성되었으며 Xilinx Spartan2E을 사용한 FPGA 보드로 구현되었다. 측정결과 PLL의 출력 전력은 약 -11dBm이고, 위상노이즈는 100kHz offset 주파수에서 -77.75dBc/Hz이다. 최소 주파수 간격은 10kHz이고, 최대 주파수 천이는 10MHz이고, 최대 주파수 변이 조건에서 고착시간은 약 800us이다.

• 한국화재소방학회논문지
• /
• 제30권6호
• /
• pp.48-56
• /
• 2016

지난 2014.4.4.(금)14:50, 울산소재 대형 옥외저장탱크에 원유 충전 중 누출사고가 발생하여 사고현장에 긴급구조통제단이 가동됐다. 사고업체, 소방기관 및 유관기관이 지휘소에 모여 대응과 수습방안을 논의한 뒤 전원차단 및 시설작동금지, 가스농도 측정, 유증기 발생 억제, 누출 원유를 타탱크와 공정과정으로 이송, 해양오염 방지조치 등의 협업체계를 구축하여 수습하였다. 이 수습과정에서 유증기 발생방지와 점화원 차단을 가장 중시하여 조치함으로써 사고업체와 소방기관이 가장 우려했던 폭발과 화재사고는 발생하지 않았다. 이에 본 연구는 일반적인 재난의 긴급구조통제단과는 달리 운영해야 할 옥외탱크의 유류 누출, 폭발 및 화재 시의 긴급구조통제단 운영체계개선을 제시하고, 옥외탱크 유류 누출로 인한 폭발과 화재사고로 전이했을 경우를 가정한 방유제 바닥 종류에 따른 화염 확산속도와 연소시간을 실험 비교하였다. 또한, 소방차 포 노즐의 방사각도와 펌프압력에 따른 방사거리와 포의 도포면적을 실험 분석하여, 이후 옥외저장탱크의 유류 누출로 인한 폭발과 화재 시를 대비한 효과적인 현장대응과 수습방안을 제시하는 데 중점을 두었다.

• 한국진공학회지
• /
• 제19권1호
• /
• pp.1-9
• /
• 2010

진공게이지의 비교교정 방법으로 교정이 가능하고-비교교정은, 2차표준기라고 부르는 교정되어진 게이지와 교정할 다른 게이지의 지시값을 읽어 비교는 방법- 다른 진공관련 실험을 할 수 있는 기체 유량 시스템을 개발하였다. 교정시스템에의 진공용기는 터보분자펌프(TMP)에 의해서 배기하고, 후면에 스크롤펌프를 배치하여 배기시스템을 꾸몄다. 터보분자펌프의 최대허용가능 압력은 펌프의 주입구에서 0.1 Pa까지이며, 이보다 압력이 높아지면 배기속도가 감소하며 압력대 이하의 환경을 조절하기가 매우 어렵게 된다. 현재 133 Pa까지의 높은 압력을 발생시킬 수 있는 새롭게 개발된 기체유량조절시스템은 바이패스 라인에 맞도록 설계된 컨덕턴스-리듀서를 설치하여 터보분자펌프를 안전하게 운용할 수 있도록 하였다. 추가로 진공용기안에 전체압력 범위(0.1 Pa ~ 133 Pa)의 압력을 생성하며 기체 주입과 압력구배를 연구하였다. 압력의 최대 편차는 용기의 위쪽 방향에 위치한 가스 주입구에서 가까운 위치 C에서 1.6%로 나타났다.

• 한국진공학회지
• /
• 제19권4호
• /
• pp.243-248
• /
• 2010

진공용 기체 유동측정 표준기로 사용하고자 소닉노즐을 ISO 9300에서 제시한 사양에 맞추어 목직경 0.03 mm와 0.2 mm의 소닉 노즐을 제작하였다. 한국표준과학연구원에서 진공용 유량측정 장치로 개발된 정적형 유량계를 이용하여 제작된 2종의 소닉노즐의 유출계수를 확장불확도 3% 이내로 교정하였다. 교정된 소닉노즐의 유량 측정범위는 약 0.6~1,800 cc/min 범위를 갖는 것으로 나타났으며, 사용유동 조건에 해당되는 레이놀드 수(Reynolds number) 범위는 26~12,100으로 확인되었다. 이러한 결과는 교정된 소닉노즐을 이용하여 진공공정에서 필요한 극 미세 유량의 정밀측정을 가능하게 한 새로운 연구결과로 판단된다. 교정된 소닉노즐을 이용하여 진공펌프의 배기속도 측정결과는 기 구축된 정적법을 이용한 배기속도 측정결과와 1% 이내의 오차범위내로 매우 잘 일치함을 보였다. 교정된 소닉노즐은 향후 반도체 및 디스플레이 공정에 사용되는 다양한 건식 진공펌프들의 배기속도를 현장에서 간단하게 평가할 수 있는 현장 성능평가 장치에 활용할 예정이며, 현재 공정현장에서 배기속도 측정에 널리 사용중인 MFC를 대체할 수 있을 것으로 예상된다.