• Title/Summary/Keyword: 펌핑손실

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The Pumping Node Architecture to Solve the Traffic Congestion Problem due to the Crowds of Mobile Nodes in Wireless Sensor Networks (고정 노드와 이동 노드가 상존하는 센서 네트워크에서 이동 노드 몰림 현상으로 인한 폭주 현상 해결을 위한 펌핑 노드 구조)

  • Lee, Dong-Kyu;Kim, Byung-Chul;Park, Sung-Ho;Kang, Soon-Ju
    • The Journal of Korean Institute of Communications and Information Sciences
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    • v.34 no.8B
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    • pp.777-785
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    • 2009
  • In recent wireless sensor networks, stationary nodes and mobile nodes co-exist to provide a diverse service. However, because there are multiple mobile nodes located in the wireless sensor network, there is a potential for the instability due to the frequent network reconfiguration and the traffic caused by densely concentration of mobile nodes while mobile nodes are switching locations. In order to solve this problem, we propose the pumping node architecture to solve this traffic congestion problem due to the crowds of mobile nodes. The pumping node can be reduced heavy traffic by pumping through the backbone network caused by the densely concentration of the mobile nodes. As a result, the architecture reduces the traffic in the sensor network with high reliability.

Numerical Analysis for Prediction of the Residual Gas Fraction, Volumetric Efficiency and Pumping Loss with Continuous Variable Valve Lift System in an SI Engine (가변밸브 작동기구를 적용한 가솔린 기관의 잔류가스분율, 체적효율, 펌핑손실 예측을 위한 해석적 연구)

  • Cho, Yong-Seok;Lee, Seang-Wock;Jang, Ik-Kyoo;Park, Jung-kwon;Yoon, Yu-Bin;Park, Young-Joon;Kim, Hyun-Chul;Na, Byung-Chul
    • Transactions of the Korean Society of Automotive Engineers
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    • v.18 no.2
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    • pp.7-13
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    • 2010
  • To satisfy the needs on fuel economy and engine performance, continuous variable valve lift systems are applying to engines. In the CVVL system, fuel economy can be improved by reducing pumping loss during the induction process, and engine performance can be also improved by controlling volumetric efficiency and the residual gas fraction. Because the residual gas fraction directly affects volumetric efficiency, engine performance, combustion efficiency and emissions in SI engines, controlling residual gas fraction is one of the important things in engine development process. This analysis investigates the residual gas fraction and volumetric efficiency with changes of intake valve lifts and intake valve timings. In this study, unsteady state solutions were solved during exhaust and induction processes. Results show variation of the residual gas fraction and volumetric efficiency by changing intake valve timing and lift. Decreasing intake valve lift leads to increase the residual gas fraction and to decrease volumetric efficiency.

Output Characteristics of the Longitudinally Pumped 946 nm Nd:YAG Laser with Laser Diode (반도체 레이저로 종펌핑하를 946 nm Nd:YAG 레이저의 출력 특성)

  • Park, Cha-Gon;Choo, Han-Tae;Kim, Gyu-Ug
    • Korean Journal of Optics and Photonics
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    • v.18 no.4
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    • pp.270-273
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    • 2007
  • We have investigated the output characteristics of the 946 nm Nd:YAG laser which is longitudinally pumped by a fiber coupled laser diode. The temperature of a Nd:YAG crystal mount was kept constant by a controller with thermoelectric cooler. As a result, we measured more intense output at a low temperature, and then the maximum output power was measured to be 870 mW when the pumping power and the temperature were 9.95 W and $5^{\circ}C$, respectively. It appeared that output was decreased above 10 W pump power because of the thermal effects in gain medium.

Optimal Design for the Rotor Overlap of a Supersonic Impulse Turbine to Improve the Performance (초음속 충동형 터빈 성능개선을 위한 동익 오버랩 최적설계)

  • Cho, Jong-Jae;Seo, Jong-Chul;Kim, Kui-Soon
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.11a
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    • pp.325-330
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    • 2011
  • A rotor overlap technique was adapted to improve the performance of a axial turbine. The technique secured sufficient flow passage by additional height at the rotor tip and hub. especially in a supersonic turbine, the technique reduced the chance of chocking in the rotor passage, and made to be satisfied the design pressure ratio. However, the technique also made additional losses, like a pumping loss, expansion loss, etc. Therefore, a optimization technique was appled to maximize the improvement of the turbine performance. An approximate optimization method was used for the investigation to secure the computational efficiency. The design variables was shape factors of a rotor overlap. Results indicated that a significant improvement in turbine performance can be achieved through the optimization of the rotor overlap.

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Effects of Variable Valve Timing Operation Modes on Engine Performance (가변 밸브개폐시기 기구 운전의 엔진 성능에의 영향)

  • 구준모;배충식
    • Transactions of the Korean Society of Automotive Engineers
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    • v.9 no.6
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    • pp.24-29
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    • 2001
  • Adaptive valve timing control is one of the promising techniques to accomplish the optimized mixture formation and combustion depending on the load and speed, which is needed to meet the future challenges in reducing fuel consumption and exhaust emissions. The behavior and the effect of adaptive valve timing control system has been investigated by computer simulation, which simulates the gas dynamics in engines. Improved fuel economy can be achieved by reduction of pumping loss under low and mid load conditions. EIVC(Early Intake Valve Closing) strategy turns out to be superior to LIVC(Late Intake Valve Closing) strategy in reducing fuel consumption. Deterioration of combustion quality can be overcome by introducing LIVO(Late Intake Valve Opening) strategy, which increases turbulent intensity in cylinders. Furthermore, LIVO can reduce HC emission by decreasing the required amount of fuel to be injected during cold start.

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Development of Evaluation and Prediction Model for Concrete High Speed Pumping (고강도콘크리트의 고속펌핑을 위한 압송성평가 및 예측모델에 관한 연구)

  • Kim, Hyung-Rae;Cho, Ho-kyoo;Jeong, Woong-Taek
    • Proceedings of the Korean Institute of Building Construction Conference
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    • 2012.05a
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    • pp.201-203
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    • 2012
  • The establishment of the technology for evaluating friction resistance and pipe pressure and the relation of the fluid characteristics and pumpability of concrete is essential for the evaluation of concrete pumping performance for high speed construction of super-tall building. So, this study focuses on quantitative evaluation of concrete fluid characteristics and surface friction resistance under the change of concrete mix proportion and pumping condition. In this study, we measured the rheology of concrete and pipe pressure and surface friction characteristics when pumping. And, relations between the rheology characteristics of concrete and pumping performance was investigated by experiment. As the result of the experiment, high regression between the surface friction and pressure gradient was confirmed. And, prediction model to evaluate the friction resistance coefficient and pipe pressure reduction coefficient was suggested.

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Optimal Design for the Rotor Overlap of a Supersonic Impulse Turbine to Improve the Performance (초음속 충동형 터빈 성능개선을 위한 동익 오버랩 최적설계)

  • Cho, Jongjae;Shin, Bong Gun;Kim, Kuisoon;Jeong, Eunhwan
    • Journal of the Korean Society of Propulsion Engineers
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    • v.18 no.1
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    • pp.33-41
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    • 2014
  • In a supersonic turbine, A rotor overlap technique reduced the chance of chocking in the rotor passage, and made the design pressure ratio satisfied. However, the technique also made additional losses, like a pumping loss, expansion loss, etc. Therefore, an approximate optimization technique was appled to find the optimal shape of overlap which maximizes the improvement of the turbine performance. The design variables were shape factors of a rotor overlap. An optimal design for rotor overlap reduces leakage mass flow rate at tip clearance by about 50% and increases about 4% of total-static efficiency compared with the base model. It was found that the most effective design variable is the tip overlap and that the hub overlap size is the lowest.

The Effects of Additional Factors on the Engine Friction Characteristics (엔진 마찰 특성에 미치는 부수적 인자의 영향)

  • Cho, Myung-Rae;Kim, Joong-Soo;Oh, Dae-Yoon;Han, Dong-Chul
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.26 no.10
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    • pp.2159-2164
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    • 2002
  • This paper reports on the effects of additional factors on the engine friction characteristics. The total friction loss of engine is composed of pumping and mechanical friction loss. The pumping loss was calculated from the cylinder pressure, and the mechanical friction loss was measured by strip-down method under the motoring condition. The various parameters were tested. The engine friction loss was much affected by oil and coolant temperature. The low viscosity oil was very effective to reduce the friction loss, and friction modifier was very useful to reduce the friction loss at lower engine speed. The engine friction loss was varied with engine running time because of surface roughness decreasing and oil degradation. To prevent oil-churning effect, it was very important to maintain the proper oil level. The presented results will be very useful to understand friction characteristics of engine.

Dynamical Behavior of Bidirectional Monolithic Nd:YAG Ring Laser (양방향으로 발진하는 일체형 Nd:YAG 고리레이저에서의 출력변조현상)

  • 홍정미;손승현;송홍주;길상근;이재철
    • Korean Journal of Optics and Photonics
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    • v.6 no.2
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    • pp.115-121
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    • 1995
  • 본 논문에서는 일체형, Nd:YAG 고리 레이저에서 서로 반대방향으로 진행하는 두 모드의 비선형적인 상호작용에 의한 출력 불안정 현상을 조사하였다. 실험을 통하여 두 모드가 각각 단일 종모드로 발진함을 확인하였고, 레이저가 발진하는 임계치 부근의 낮은 펌핑수준을 유지하여 다중모드간의 경쟁이나 단방향 발진에 의한 출력 불안정이 아님을 확인하였다. 또한 잘 알려진 시스템 고유의 감쇄진동과 구별되는 현상임을 보였다. 두 모드간의 손실차가 클수록 이 출력의 변조주파수는 증가하고 변조폭이 줄어 들어 안정화 되며 단방향 발진이 일어난다.

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Efficiency Analysis of Thermal Transpiration According to Knudsen Number for Application to Micro-propulsion System (마이크로 추진장치에 적용을 위한 누센수에 따른 열적발산원리의 효율분석)

  • Jung, Sung-Chul;Huh, Hwan-Il
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.36 no.5
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    • pp.483-490
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    • 2008
  • Minimization of nozzle induces many flow losses in micro-propulsion system. In this study, we studied about thermal transpiration based micro propulsion system to overcome these losses. Thermal transpiration device(Knudsen pump) having no moving parts can self-pump the gaseous propellant by temperature gradient only (cold to hot). We designed, fabricated the Knudsen pump and analyzed pressure gradient efficiency of membrane according to Knudsen number under vacuum condition. Experimental results showed that thick membranes are more effective than thin membranes in transition flow regime, and pressure gradient efficiency according to Knudsen number is increased to maximum 82% apart from membrane thickness in free molecular regime.