• 제목/요약/키워드: Lift plate

검색결과 108건 처리시간 0.026초

충전전압에 따른 겔형 VRLA전지 양극판의 파손방식 (Failure Mode of the Positive Plate on Charging Voltage in Gel Type Valve Regulated Lead Acid Batteries)

  • 오상협;김명수;이흥락
    • 전기화학회지
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    • 제3권2호
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    • pp.90-95
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    • 2000
  • 겔형 VRLA전지의 파손방식을 조사하기 위하여 $100\%$ 방전심도에서 5시간율 전류로 충방전 수명시험을 하였다. 정전압 충전방식을 사용하여 충전전압을 2.40V와 2.50V로 하였을 때 1,000회 이상의 수명을 나타내었으며, 전지의 무게변화를 측정한 결과 각각 426.4g과 391.2g의 전해액이 감소하였다 2.50V로 충전한 전지가 우수한 수명특성을 나타내었으며, 전해액 손실량이 충전계수와 비례하는 것을 알 수 있었다 1,000회의 충방전 수명시험을 한 전지의 양극기판에는 약 $50{\mu}m$의 부식층이 관찰되었고, 활성물질의 미세구조는 크게 변하였다. 양극판의 파손방식은 활물질 탈락이며, 전해액 손실이 방전용량 감소의 원인인 것을 알 수 있었다.

노즈 페어링 구조용 복합재 평판의 음향 하중 저감 특성 (Acoustic Loads Reduction of Composite Plates for Nose Fairing Structure)

  • 박순홍;공철원;장영순;이영무
    • Composites Research
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    • 제17권3호
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    • pp.15-22
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    • 2004
  • 위성 발사체의 추진 기관에 의한 음향 하중은 이륙 시 작용하는 주요한 동적 하중 중 하나로서, 이에 의한 위성이나 탑재물의 파손이 보고되고 있다. 위성이나 탑재물에 작용하는 음향 하중의 강토를 저감하기 위해서는 노즈 페어링의 구조 설계 시 차음 성능을 고려한 설계가 필요하다. 특히 복합재 구조의 경우 금속재 구조에 비해 비강성이 커서 음향 하중의 차음 측면에서는 불리하다. 본 논문에서는 위성 발사체의 노즈 페어링용 복합재 평판의 차음 특성을 살펴보았다. 노즈 페어링 구조로 사용 가능한 4종의 복합재 구조에 대하여 무한판 이론 및 통계적 에너지 해석법(SEA)을 이용하여 차음 성능을 평가하였다. 해석 결과를 토대로 두 종류의 복합재 평판을 제작하여 이에 대한 차음 성능을 측정하고 예측치와 비교를 수행하였다. 이를 바탕으로 무게 대비 차음 성능이 우수한 노즈 페어링용 복합재 구조를 선정할 수 있었다.

해수열원 히트펌프 시스템의 운전특성 (The Operation Characteristics of a Sea Water Source Heat Pump System)

  • 장기창;백영진;나호상;김지영;이재훈
    • 대한설비공학회:학술대회논문집
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    • 대한설비공학회 2008년도 하계학술발표대회 논문집
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    • pp.1353-1357
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    • 2008
  • A sea water source cascade heat pump was designed and tested in this study. The system was designed to perform a single stage operation in summer, as well as a cascade operation in winter to ensure the high temperature lift. A steady-state simulation model was developed to analyze and optimize its performance. The simulation results show that the R717 exhibits best performance among combinations considered in this study. A R410A also exhibits the highest performance among HFCs with the smallest compressor displacement. A 15-RT R410A-R134a pilot system was installed in the 5-story commercial building at Samcheok City by the East Sea. A scroll type R410A compressor, a reciprocating type R134a compressor, plate type condenser/ evaporator/ cascade heat exchanger and two electronic expansion valves were used to build a pilot. A titanium plate type heat exchanger is also used for the heat exchanging with a sea water. The heat source/sink water is supplied from the well below the seashore in the depth of 5 m. In the initial test of the system, supply water temperature was rising up to $67^{\circ}C$ using a sea water heat source of $9^{\circ}C$, while an ambient temperature was $4.5^{\circ}C$.

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해수열원 히트펌프 시스템의 설계 및 운전 (A Design and Test of a Sea Water Source Heat Pump System)

  • 이재훈;김지영;백영진;장기창;나호상;신광호
    • 대한설비공학회:학술대회논문집
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    • 대한설비공학회 2008년도 하계학술발표대회 논문집
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    • pp.1273-1278
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    • 2008
  • A sea water source cascade heat pump was designed and tested in this study. The system was designed to perform a single stage operation in summer, as well as a cascade operation in winter to ensure the high temperature lift. A steady-state simulation model was developed to analyze and optimize its performance. The simulation results show that the R717 exhibits best performance among combinations considered in this study. A R410A also exhibits the highest performance among HFCs with the smallest compressor displacement. A 15-RT R410A-R134a pilot system was installed in the 5-story commercial building at Samcheok City by the East Sea. A scroll type R410A compressor, a reciprocating type R134a compressor, plate type condenser/ evaporator/ cascade heat exchanger and two electronic expansion valves were used to build a pilot. A titanium plate type heat exchanger is also used for the heat exchanging with a sea water. The heat source/sink water is supplied from the well below the seashore in the depth of 5 m. In the initial test of the system, supply water temperature was rising up to $67^{\circ}C$ using a sea water heat source of $9^{\circ}C$, while an ambient temperature was $4.5^{\circ}C$.

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HEMU-400X 팬터그래프 시스템의 공력성능 개선을 위한 실험적 연구 (Experimental Studies on Improvement of Aerodynamic Performance of Pantograph System for HEMU-400X)

  • 이영빈;곽민호;김규홍;이동호;정형석;장영일;권혁빈
    • 한국철도학회:학술대회논문집
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    • 한국철도학회 2011년도 춘계학술대회 논문집
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    • pp.1-6
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    • 2011
  • In this study, wind tunnel test were conducted to improve an aerodynamic performance of HEMU400X pantograph system with 4 types of pantograph housing models. Experimental models were 1/4 scaled pantograph system, 1/4 scaled ground plate which is scaled down to real roof shape of HEMU-400x, and 4 types of pantograph housing models. The free stream of wind tunnel were 20, 40, 60, 70m/s. The lift and drag forces were measured with 2-axis load cell. And, Total pressure were measured with rake in the wake region of panhead. In addition, Surface flow visualization by tufts were performed to know flow characteristics around pantograph housing. According to the results of force tests and surface visualizations, pantograph housing shape is important part because the shape affects to pantograph system. Therefore, it is considered that adaption of pantograph housing is more advantageous to decrease drag and acoustic noise.

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마늘파종기용 배종장치 개발 (Development of a Metering Device for the Garlic Planter)

  • 최덕규;조성찬;이채식;박석호;김학진;강태경;김충길;곽태용
    • Journal of Biosystems Engineering
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    • 제26권6호
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    • pp.525-534
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    • 2001
  • Garlic clove planting is one of the most laborious operations in Korean farming. The garlic planting has been done manually; therefore, it requires tremendous amounts of human labor resulting in the increase of production cost. This problem necessitated the development of a garlic clove metering device fur the planter. The device was fabricated to meter a single garlic clove with a scooping bucket(29mm in diameter and 8mm in depth) designed after the image of clove's bottom shape. The lift angle of the metering plate and the magnitude of vibration were also affected the metering performance. The angle clove metering rates ranged 95.4~96.7% with the missing rate of 0.0~1.3% at the 80~85 degrees of the tilt angle and vibration level 2(1.985 m/s$^2$).

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공압용 더블챔버 로터에서 베인개수에 따른 성능특성에 관한 실험적연구 (An Experimental Study of Performance Characteristics on a Double Chamber Rotor Operated by High Pressure Air with Various Vanes)

  • 조종현;최상규;조수용
    • 한국유체기계학회 논문집
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    • 제9권6호
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    • pp.54-62
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    • 2006
  • An experiment about performance characteristics is conducted on a double chamber vane-type rotor. Three different rotors, which have 6, 8 and 9 vanes, are applied to the driver and various lift holes at the rear plate are used to increase the effective vane height. The inner diameter of a double chamber cylinder is ${\phi}27mm$, and the length of the cylinder is 65 mm. The maximum offset length between the rotor outer surface and the cylinder inner surface is 4.5 mm. In this study, specific output torques and powers are measured, and also noise and vibration are measured at the real operating situation. The operating torque on the double chamber is increased to 17% compared to the operating torque obtained at the single chamber which has the same size. The experimental results of noise and vibration show that the operating sound and vibration are directly related to the operating power generated by the double chamber rotor.

정밀이송을 위한 캠-슬라이더 메커니즘 구조의 테이프 피더에 관한 연구 (A Study on the High Precision Tape Feeding Device with Cam-slider Mechanism)

  • 전병철;조명우;강성민;이수진;최진화
    • 한국정밀공학회지
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    • 제23권4호
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    • pp.132-138
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    • 2006
  • A tape feeder is an important part to supply a micro chip such as 1005 and 0603 components in SMT process. Traditional sprocket wheel type feeder has several problems such as backlash and indexing errors, low compatibility and confidence. However, it is very difficult to solve such problems due to the inevitable fraction defectives of sprocket wheel. Thus, the object of this works is to develop a linear type high precision tape feeding system using cam-slider mechanism. The proposed cam-slider mechanism is composed of several links and a plate, pneumatic actuator is used to generate linear motion. The proposed mechanism has distinct advantages over the conventional mechanism. It has reduced feeding errors, long lift-cycle, and slim width. As a result, the developed tape feeder using cam-slider mechanism shows special characteristics far high precision feeding for chip-mounters.

EDISON_전산열유체를 활용한 풍력발전기 타워의 후류 불안정성 억제에 관한 수치연구 (NUMERICAL ANALYSIS FOR SUPPRESSING UNSTEADY WAKE FLOW ON WIND TURBINE TOWER USING EDISON_CFD)

  • 김수용;진도현;이근배;김종암
    • 한국전산유체공학회지
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    • 제18권1호
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    • pp.36-42
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    • 2013
  • The performance of the wind turbine is determined by wind speed and unsteady flow characteristics. Unsteady wake flow causes not only the decline in performance but also structural problems of the wind turbine. In this paper, conceptual designs for the wind turbine tower are conducted to minimize unsteady wake flow. Numerical simulations are performed to inspect the shape effect of the tower. Through the installation of additional structures at the rear of the tower, the creation of Karman vortex is delayed properly and vortex interactions are reduced extremely, which enhance the stability of the wind turbine. From the comparative analysis of lift and drag coefficients for each structure, it is concluded that two streamwise tips with a splitter plate have the most improved aerodynamic characteristics in stabilizing wake flow.

난류 혼합층에서 확산화염에 대한 flame hole dynamics 모델 (Flame Hole Dynamics Model of a Diffusion Flame in Turbulent Mixing Layer)

  • 김준홍;정석호;안국영;김종수
    • 한국연소학회지
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    • 제8권3호
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    • pp.15-23
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    • 2003
  • Partial quenching structure of turbulent diffusion flames in a turbulent mixing layer is investigated by the method of flame hole dynamics in order to develop a prediction model for turbulent flame lift off. The essence of flame hole dynamics is derivation of the random walk mapping, from the flame-edge theory, which governs expansion or contraction of flame holes initially created by local quenching events. The numerical simulation for flame hole dynamics is carried out in two stages. First, a direct numerical simulation is performed for constant-density fuel-air channel mixing layer to obtain the turbulent flow and mixing fields, from which a time series of two dimensional scalar dissipation rate array is extracted at a fixed virtual flame surface horizontally extending from the end of split plate to the downstream. Then, the Lagrangian simulation of the flame hole random walk mapping projected to the scalar dissipation rate array yields temporally evolving turbulent extinction process and its statistics on partial quenching characteristics. The statistical results exhibit that the chance of partial quenching is strongly influenced by the crossover scalar dissipation rate while almost unaffected by the iteration number of the mapping that can be regarded as a flame-edge speed.

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