• Title/Summary/Keyword: Operating Pressure

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Optimum Operating Conditions of a Vacuum Nozzle Seeder (진공노즐식 파종기의 최적 작동조건)

  • 민영봉;김성태;정태상
    • Journal of Biosystems Engineering
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    • v.25 no.6
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    • pp.463-470
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    • 2000
  • For maximum seeding efficiency of a nozzle type seeder, the performance of the nozzle should be considered sufficiently. This study was carried out to investigate the optimum operating conditions of a seeder attached the vacuum nozzle which was modified syringe needle acting on the plug seedling tray and the seed plate. Such operating factors as the hole diameter of the nozzle (d), the distance from the nozzle tip to the bottom plate of seed hopper(D) the absorbing air pressure of the nozzle tip(P) the bounding height of seed from the vibrated bottom plate of seed hopper and the seeding speed were selected based on the weight of a grain of seed(W). The treated materials were pepper seed as the flat type, cucumber seed as the oval type and radish seed as the spherical type. The optimum operating conditions of the experimental seeder were revealed as follows: 1. The height of the seed bounding from the bottom plate of seed hopper and the distance from nozzle tip to bounded seed were 5 mm and 0.5 mm at all seeds. The hole diameter of the nozzle and the absorbing pressure for pepper seed, cucumber seed and radish seed was 0.45 mm, 0.65 mm. 0.65mm and 39.2 kPa, 88.3 kPa, 58.8 kPa, respectively. 2. The absorbing pressure P was represented as P=η.4W/$\pi$d$^2$ where η was 100. The seeding speed using a 128 cell tray was 2.4 cm/s which was same transfer as 2.5 trays per minute. 3. The maximum seeding rate in case of the pepper seed was 97% the cucumber seed was 95% and the radish seed was 100% under the optimum operating conditions of the seeder.

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Finite Element Analyses of Stamping Tact Spring and Operation of Tact Switch (택트 스프링 타발과 택트 스위치 작동의 유한요소해석)

  • 엄경근;이세형;오규환;이동녕
    • Transactions of Materials Processing
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    • v.4 no.1
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    • pp.17-27
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    • 1995
  • The tact switch is widely used in electric and electronic products. The dome type tact spring is produced by stamping. Stamping of the tact spring and operation of the tact switch have been simulated by the elasto-plastic finite element method. The operating characteristics of the switch may be given by the relation between the operating force and stroke. For a given material, this is affected by two main factors. One is the geometry of dome spring which is determined by the geometry of stamping dies and the stamping pressure, and another one is the dimension of switch. From the calculation, it was possible to obtain the stamping conditions and switch dimension for a predetermined force-stroki relation And, the hoop stresses and effective strains distributions due to the stamping and during the operation of the switch indicate a possibility of cracking in the center and rim of dome spring.

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Performance Analysis of SOFC/MGT Hybrid System

  • Kim, Jae-Hwan;Suzuki, Kenjiro
    • Proceedings of the KSME Conference
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    • 2001.06d
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    • pp.703-707
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    • 2001
  • A performance analysis of a SOFC/MGT hybrid system has been carried out for concept design. Thermo-dynamic models for each component being able to describe electrochemical characteristics and heat and mate-rial balance are proposed. Estimated is the power capacity of a SOFC suitable for the hybrid operation with a 5kW class MGT. Effects of current density and operating pressure are also investigated. Electric efficiency showed weak dependence on operating pressure and current density. It is desirable that the SOFC operates at high current density in manufacturing cost's point of view though operating with high current density slightly decreases the electric efficiency find specific power.

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Characteristics of Performance Parameters of Dual Mode(Ramjet-Scramjet Combined) Engine Based on the Analysis of The Operating limitations (작동한계 관점에서의 이중모드(램제트-스크램제트 연합 작동)엔진의 성능 인자 특성)

  • Sung, Hong-Gye;Byun, Jong-Ryul
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2006.11a
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    • pp.393-396
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    • 2006
  • This paper presents the characteristics of the performance parameters of dual mode(ramjet-scramjet combined) engine, inlet and combustor for wide range of flight Mach number, resulted from the analysis of its operating limitations. The transitional-critical flight Mach number from ramjet to scramjet and the performance of two types of combustors, such as constant pressure- and constant area- combustor, are conceptually evaluated.

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Effects of regenerator and cooler on the cooling performance of a vuilleumier cycle heat pump (재생기 및 냉각기가 VM열펌프의 냉방성능에 미치는 영향)

  • Lee, G.T.;Kang, B.H.;Yoo, H.;Lee, J.H.
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.9 no.3
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    • pp.333-342
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    • 1997
  • An experimental study has been carried out to investigate the effects of the combination of the different wire mesh number in a regenerator and the tube number in a cooler on the cooling performance of a Vuilleumier cycle heat pump. Effects of operating conditions, such as charging pressure, operating speed, and heat input, on the cooling performance are also studied. The experimental results obtained indicate that the cooling performance could be improved with the proper combination of different wire meshes in a regenerator. More tubes in a cooler are desirable for better cooling performance. It is also found that the cooling capacity is enhanced, whereas COP is reduced with an increase in the heater tube temperature and the revolution speed. Both the cooling capacity and COP are incereased with a higher charging pressure.

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Large Eddy Simulation on the Vorticity Characteristics of Three-Dimensional Small-Size Axial Fan with Different Operating Points (운전점에 따른 3차원 소형축류홴의 와도 특성에 대한 대규모 와 모사)

  • Kim, Jang-Kweon;Oh, Seok-Hyung
    • Journal of Power System Engineering
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    • v.20 no.6
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    • pp.64-70
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    • 2016
  • The unsteady-state, incompressible and three-dimensional large-eddy simulation(LES) was carried out to evaluate the vorticity distribution of a small-size axial fan(SSAF). The X-component vorticity profiles developed around blade tips turn from axial to radial, and diminish the density of distribution according to the increase of static pressure. Otherwise, the Z-component vorticity profiles evenly develop at the region larger than the half radial distance of blade at the operating points of A and B, partly at the trailing-edge region of blade and radially over bellmouth according to the increase of static pressure.

Simulator Development of 1000MW Class Ultra Super Critical Coal-Fired Power Plant with Advanced Process Control Algorithm (고급공정제어 알고리즘을 이용한 1000MW급 차세대화력발전소 시뮬레이터 개발)

  • Oh, Ki-Yong;Lim, Geon-Pyo;Kim, Ho-Yol
    • Proceedings of the KIEE Conference
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    • 2008.07a
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    • pp.1817-1818
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    • 2008
  • Even though efficiency of coal-fired power plant is proportional to operating temperature, increasement of operating temperature is limited by a technological level of each power plant components. It is an alternative plan to increase operating pressure up to ultra super critical point for efficiency enhancement. It is difficult to control in that pressure within safety guideline that many unexpected phenomena are happen because that region is highly nonlinear region. In this paper, Advanced process control algorithm, ARX and Fuzzifier, is introduced. Then power plant control logics applied Unit Step Optimizer, which is combination of ARX and Fuzzifier are proposed. Its performance is tested and analyzed with design guide line.

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evaluation of Performance Characteristic on Triple Effect Absorption Cycle (삼중효용 흡수사이클의 성능특성 평가)

  • 권오경
    • Journal of Advanced Marine Engineering and Technology
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    • v.22 no.6
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    • pp.782-791
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    • 1998
  • This paper presents a computer simulation of five types of triple effect absorption cycles employ-ing the refrigerant absorbent combinations of NH3/LiNO3 low-pressure type NH3/LiNO3+H2O/LiBr binary two-stage type series flow cycle and two types of parallel flow cycle for H2O/LiBr. The absorption systems is investigated through cycle simulation to obtain the system characteristics with the cooling water inlet temperature approach temperature of absorber loss temperature of absorber and chilled water outlet temperature. The most important characteristic temperature of absorber and chilled water outlet temperature. The most important characteristic of NH3/LiNO3 low-pressure type and a NH3/LINO3+H2O/LiBr binary two-stage type is that it obtains a coefficient of performance higher than the sum of the performance coefficients of its part operating independently. As a result of this analysis the optimum designs and operating conditions were determined based on the operating conditions and the coefficient of performance.

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Numerical Analysis of Performance of Linear Compressor for the Stilting Cryocooler (스터링 냉동기의 선헝압축기 운전특성에 관한 수치해석적 연구)

  • 홍용주;박성제;김효봉;염한길;최영돈
    • Progress in Superconductivity and Cryogenics
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    • v.4 no.2
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    • pp.58-62
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    • 2002
  • The purpose of this study is to analyze the charging gas effect on the resonance and performance characteristics of the linear compressor for small scale FPFD Stirling refrigerator. To ensure high performance of FPFD type Stirling refrigerator, the operating frequency of the refrigerator should be around the natural frequency of compressor. The gas spring effect which is induced from Pressure change in cylinder due to motion of pistons has significant effect on the natural frequency of the compressor. The numerical results show the linear compressor has high natural frequency when the charging pressure of working fluid is high and the stroke of compressor, current, input power and efficiency of compressor were shown with different operating conditions.

Study on Design- and Operating- Parameters of Supersonic Exhaust Diffusers Simulating high Altitude (고고도 모사용 초음속 디퓨져의 설계인자 및 작동인자에 대한 연구)

  • Yoon, Sang-Kyu;Kim, Jin-Kon;Sung, Hong-Gye;Kim, Yong-Wook;Oh, Seung-Hyup
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2007.04a
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    • pp.303-306
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    • 2007
  • A engineering analysis has been conducted to study operating characteristics of a supersonic exhaust diffuser simulating high altitude atmosphere from a flow-developing point of view. Emphasis is placed in the detail flow structure resulting from several design- and operating- parameters of the diffuser such as the area ratios of a exhaust nozzle to the diffuser, the vacuum chamber size, and jet pressure.

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