• 제목/요약/키워드: Speed-power-rpm

검색결과 379건 처리시간 0.029초

견인 및 등판 성능을 통한 고소작업기계의 모터 주행장치 설계 (Design of Motor-driven Traveling System for High Clearance Working Machinery based on Tractive Performance and Hill Climbing Ability)

  • 이상식;장세윤;김태수;남규철;박원엽
    • 한국정보전자통신기술학회논문지
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    • 제9권3호
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    • pp.257-265
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    • 2016
  • 이 연구는 과수원에 높은 통관 작업 기계에 적용되는 전동식 트럭 주행 시스템을 적용한 최적 설계가 제안되어 있습니다. 견인 성능과 언덕 등반 능력은 예측 및 기계 작업이 높은 틈새를 이용하여 과수원의 토양 특성을 고려하여 최적의 모터 주행 시스템을 평가 하였다. 견인 성능을 위한 설계 기준은 운동 저항을 뺀 견인력으로부터 산출 된 견인능력에 기초를 두었다. 등판 능력은 20%의 경사면을 3km/h의 속도로 수행되도록 하는 설계기준을 가지고 있다. 견인 및 등판 능력의 평가 결과에 따라 두 개의 DV48V, 4500rpm, 16kW AC 모터는 좌우 양쪽에서 독립적인 괘도를 갖는 것으로 적용된다. 각각의 모터는 50:1 감속기어 비율을 통하여 트랙형 주행 시스템의 구동 스프로켓에 동력을 전달하도록 설계되었다. 본 연구의 전동 트랙형 주행 시스템은 충분한 견인성능 및 등판 능력을 충분히 입증하고 20%의 경사지면을 갖는 과수원의 토양에서의 등반저항보다 12.5%가 더 높은 396kgf의 견인능력을 가지고 있는 것으로 밝혀졌습니다.

반궤도식 산림작업차 개발(I) - 설계 및 제작 - (Development of the Semi-Crawler Type Mini-Forwarder - Design and Manufacture -)

  • 김재환;박상준
    • 한국산림과학회지
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    • 제100권2호
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    • pp.154-164
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    • 2011
  • 본 연구는 우리나라 험준한 급경사 지형의 단목중심의 목재생산시스템 등에 적합하고 사방사업, 임도사업 등의 다양한 산림작업에 유용하게 활용할 수 있는 다목적의 반궤도식 산림작업차 개발을 목적으로 실시하였다. 산림작업차량의 기본 차체는 최소회전반경 설계기준과 작업도 폭을 고려하여 차체프레임부의 총길이는 5,750 mm, 차체의 폭은 1,900 mm, 적재부의 적재용량은 약 $2.5m^{3}$으로 설계 제작하였다. 동력원은 3,400 rpm의 최대 96마력 출력의 엔진을 선정하였으며, 유압펌프는 2개의 주펌프와 2개의 보조펌프로 나누어 선정하고, 주펌프는 전후좌우 4개의 주행용 유압모터에 사용하고, 보조펌프는 각종 작업기에 사용하도록 설계 제작하였다. 동력전달방식은 HST(Hydro-Static Transmission) 시스템을 적용하였고, 주행부는 조향가능한 전방 고무바퀴와 무한 궤도형으로 회전하는 후방 크롤러로 설계 제작하고, 조향방식은 애커만 조향방식을 채택하였다. 주행조작부는 일반 자동차의 운전 및 운전석 형태로 설계 제작하였으며, 보조장치로 윈치와 로그그래플 및 아웃트리거를 장착하였다. 시작기의 공차시 임도의 주행속도는 저속 5.3 km/hr, 고속 7.7 km/hr로 나타났다.

선박 에너지 절감을 위한 기관실 팬 제어 시스템 구축 및 알고리즘에 관한 연구 (A Study on the Development of the Engine Room Fan Control System and ERFCS Algorithm for Ships Energy Saving)

  • 강영민;오진석
    • Journal of Advanced Marine Engineering and Technology
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    • 제39권6호
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    • pp.642-648
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    • 2015
  • 최근 선박에서 에너지 절감에 대한 많은 연구가 수행되고 있다. 그러한 연구의 일환으로 선박의 고정적인 부하를 제외한 변동 부하를 파악하고 제어함으로써 선박의 에너지를 절감할 수 있다. 기관실 팬 시스템은 대표적인 변동부하 중 하나이다. 기존 선박에서는 기관실 팬을 특별한 지침 없이 실 경험에 의해 정격운전으로 운용하고 있다. 이에 본 논문에서는 기관실 팬의 특성을 파악하고, 에너지 관리 시스템 중 하나로 ERFCS(Engine Room Fan Control System) 및 ERFCS 알고리즘을 제안하였다. ERFCS는 온도 및 압력에 따라 팬의 속도를 제어하며 부하 변화에 따라 팬의 운전 대수를 1대에서 4대 사이로 조절한다. 또한 기관실 팬의 최소 회전속도를 50%로 제한하여 낮은 RPM(Revolution Per Minute)에서 기계적 마찰, 발열 등의 이유로 팬이 손상을 입거나 낮은 압력으로 팬에 서징(surging) 현상이 발생하지 않도록 한다. 제안된 알고리즘과 ISO 8861을 바탕으로 LabVIEW를 사용한 팬 제어 시스템 시뮬레이션을 개발하였다. 결론적으로, 구현된 시뮬레이션을 통해 제안된 팬 제어 시스템이 기존 사용 방식에 비해 46.4%만의 동력만으로도 운전이 가능함을 확인하였다.

로우터리 맥류파종기 경운날의 개량시험 (Improvement of Rotary Tine for Barley Seeder Attached to Rotary Tiller)

  • 김성래;김문규;김기대;허윤근
    • Journal of Biosystems Engineering
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    • 제4권1호
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    • pp.1-23
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    • 1979
  • The use of barley seeder attached to rotary tiller in the rural area has a significant meaning not only for the solution of labor peak season, but also for the increase of land utilization efficiency. The facts that presently being used barley seeders are all based on the mechanical principles of the reverse rotation, center drive and are all using forward rotating tine, which is used to be easily and heavily worn out when it rotates reversely, raise problem of recommending them to rural area in Korea. Therefore, the main objective of the study was to develop new type of rotary tine attachable to barley seeders. To attain the objective the following approaches were applied. (1) The kinematic analysis of reverse rotating barley seeders. (2) The studies on the soil bin and artificial soil. (3) The comparative experiment on the power requirement of prototype tine. The results obtained from the studies are summarized as follow: 1. The kinematic analysis of barley seeder attached to rotary tiller: The following results were obtained from the kinematic analysis for deriving general formulae of the motion and velocity characterizing the rotary tine of barley seeders presently being used by farmers. a) The position vector (P) of edge point (P) in the rotary tine of reverse rotating, center drive was obtained by the following formula. $$P=(vt+Rcos wt)i+Rsin wt j+ \{ Rcos \theta r sin \alpha cos (wt- \beta +\theta r) +Rsin \theta r sin \alpha sin (wt-\beta + \theta r) \} lk $$ b) The velocity of edge point $(P^')$ of reverse rotating, center drive rotary tine was obtained by the following formula. $$(P^')=(V-wR sin wt)i+(w\cdot Rcoswt)j + \{ -w\cdot Rcos \theta r\cdot sin \alpha \cdot sin (wt-\beta +\theta r) + w\cdot Rsin \theta r\cdot sin \alpha \cdot cos (wt- \beta + \theta r \} k $$ c) In order to reduce the power requirement of rotary tine, the angle between holder and edge point was desired to be reduced. d) In order to reduce the power requirement, the edge point of rotary tine should be moved from the angle at the begining of cutting to center line of machine, and the additional cutting width should be also reduced. 2. The studies on the soil bin and artificial soil: In order to measure the power requirement of various cutting tines under the same physical condition of soil, the indoor experiments Viere conducted by filling soil bin with artificially made soil similar to the common paddy soil and the results were as follows: a) When the rolling frequencies$(x)$ of the artificial soil were increased, the densIty$(Y)$ was also increased as follows: $$y=1.073200 +0.070780x - 0.002263x^2 (g/cm^3)$$ b) The absolute hardness $(Y)$ of soil had following relationship with the rolling frequencies$(x)$ and were increased as the rolling frequencies were increased. $$Y=37.74 - \frac {0.64 + 0.17x-0. 0054x^2} {(3.36-0.17x + 0.0054x^2)^3} (kg/cm^3)$$ c) The density of soil had significant effect on the cohesion and angle of internal friction of soil. For instance, the soil with density of 1.6 to 1.75 had equivalent density of sandy loam soil with 29.5% of natural soil moisture content. d) The coefficient of kinetiic friction of iron plate on artificial soil was 0.31 to 0.41 and was comparable with that of the natural soil. e) When the pulling speed of soil bin was the 2nd forward speed of power tiller, the rpm of driving shaft of rotary was similar to that of power tiller, soil bin apparatus is indicating the good indoor tester. 3. The comparative experiment on the power requirement of prototype tine of reverse rotating rotary: According to the preliminary test of rotary tine developed with various degrees of angle between holder and edge pcint due to the kinematic analysis, comparative test between prototype rotary tine with $30 ^\circ $ and $10 ^\circ$ of it and presently being used rotary tine was carried out 2nd the results were as follows: a) The total cutting torque was low when the angle between holder and edge point was reduced. b) $\theta r$ (angle between holder and edge point) of rotary tine seemed to be one: of the factors maximizing the increase of torque. c) As the angle between holder and edge point ($\theta r$) of rotary tine was $30 ^\circ $ rather than $45 ^\circ $, the angle of rotation during cutting soil was reduced and the total cutting torque was accordingly reduced about 10%, and the reduction efficiency of total cutting torque was low when the angle between holder and edge point ($\theta r$) of rotary tine was $10 ^\circ $, which indicates that the proper angle between holder and edge point of rotary tine should be larger than $10 ^\circ $ and smaller than $30 ^\circ $ . From above results, it could be concluded that the use of the prototype rotary tine which reduced the angle between holder and edge point to $30 ^\circ $, insted of $45 ^\circ $, is disirable not only decreasing the power requirements, but also increasing the durabie hour of it. Also forward researches are needed, WIlich determine the optimum tilted angle of rotary brocket, and rearrangement of the rotary tine on the rotary boss.

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50KW 터보제너레이터용 가스터빈 엔진의 설계점/ 탈설계/과도성능해석 (On/Off-Design/Transient Analysis of a 50KW Turbogenerator Gas Turbine Engine)

  • 김수용;박무룡;조수용
    • 연구논문집
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    • 통권27호
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    • pp.87-99
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    • 1997
  • Present paper describes on/off design performance of a 50KW turbogenerator gas turbine engine for hybrid vehicle application. For optimum design point selection, relevant parameter study is carried out. The turbogenerator gas turbine engine for a hybrid vehicle is expected to be designed for maximum fuel economy, ultra low emissions, and very low cost. Compressor, combustor, turbine, and permanent-magnet generator will be mounted on a single high speed (82,000 rpm) shaft that will be supported on air bearings. As the generator is built into the shaft, gearbox and other moving parts become unnecessary and thus will increase the system's reliability and reduce the manufacturing cost. The engine has a radial compressor and turbine with design point pressure ratio of 4.0. This pressure ratio was set based on calculation of specific fuel consumption and specific power variation with pressure ratio. For the given turbine inlet temperature, a rather conservative value of $1100^\circK$ was selected. Designed mass flow rate was 0.5 kg/sec. Parametric study of the cycle indicates that specific work and efficiency increase at a given pressure ratio and turbine inlet temperature. Off design analysis shows that the gas turbine system reaches self operating condition at N/$N_{DP}$ = 0.53. Bleeding air for turbine stator cooling is omitted considering low TIT and for a simple geometric structure. Various engine performance simulations including, ambient temperature influence, surging at part load condition. Transient analysis were performed to secure the optimum engine operating characteristics. Surge margin throughout the performance analysis were maintained to be over 80% approximately. Validation of present results are yet to be seen as the performance tests are scheduled by the end of 1998 for comparison.

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파이어링 상태의 일정 축 각속도에서 엔진 베어링의 마모 해석 - Part I: 베어링 마모발생 부위 파악 (Wear Analysis of Engine Bearings at Constant Shaft Angular Speed on a Firing State - Part I: Understanding of Bearing Wear Region)

  • 전상명
    • Tribology and Lubricants
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    • 제34권3호
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    • pp.93-107
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    • 2018
  • The purpose of Part I of this study is to find the potential region of wear scarring on engine journal bearings operating at a constant angular crank shaft velocity under firing conditions. To do this, we calculate the applied loads and eccentricities of a big-end journal bearing installed on a four-stroke and four-cylinder engine at every crank angle. Then, we find potential wear regions, such as a minimum oil film thickness, at every crank angle below most oil film thickness scarring wear (MOFTSW) obtained based on the concept of the centerline average surface roughness. Thus, the wear region is defined as a set of each film thickness below the MOFTSW at every crank angle. In this region, the wear volume changes according to the wear depth and wear angle, depending on the minimum oil film thickness at every crank angle. The total wear volume is the summation during one cycle. Graphical views of the region in the two-dimensional coordinates show the crank angle and bearing angle along the journal center path, indicating the position of the minimum oil film thickness. The results of wear analysis show that the possible wear region is located at a few tens of angles behind the upper center of a big-end bearing at maximum power rpm.

백미와 발아현미의 혼합비율이 압출성형 멥쌀가루의 이화학적 특성에 미치는 효과 (Effect of Mixing Ratio of White and Germinated Brown Rice on the Physicochemical Properties of Extruded Rice Flours)

  • 김지명;우맹영;신말식
    • 한국식품조리과학회지
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    • 제28권6호
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    • pp.813-820
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    • 2012
  • To develop the high quality gluten-free rice products with health functionality and desirable texture with moistness, the physicochemical properties of extruded rice flours prepared from the mixture of germinated brown and white rices were investigated. The domestic organic Samgwangbyeo was used to make white and germinated brown rices. White rice (WR) was dried after soaked for 6 h at $15{\pm}3^{\circ}C$ and mixed with germinated brown rice (GBR) with different mixing ratios (100:0, 75:25, 50:50, 25:75, 0:100). The operating conditions of twin screw extruder were 250 rpm of screw speed, $120^{\circ}C$ of barrel temperature, and 25% moisture content of rice flour. The ash, crude protein and crude lipid contents were significantly different (p<0.05) and those of extruded GBR were the highest values, but those of extruded WR were the lowest. The color difference of extruded WR based on white plate showed the lowest among them. The water binding capacity (334.16%), swelling power (8.83 g/g), solubility (33.13%), and total starch (79.50%) were the lowest in extruded GBR. The viscosities of all extruded rice flours by RVA were maintained during heating. The peak and total setback viscosities of extruded rice flours ranged 127-352 and 58.0-85.5 cP, respectively. The novel food biomaterial from germinated brown rice as well as white rice was developed by twin screw extruder. The extruded rice flours control the moistness to improve the texture and also have functional materials, dietary fiber, GABA, and ferulic acid, etc to increase quality of gluten free rice products.

EGR 밸브 평가 장치 개발을 위한 EGR 장착 엔진 성능 및 배출 가스 특성 연구 (A Study on Exhaust Gas Characteristics and Engine Performance of EGR Valve Installed Engine for Development of EGR Valve Test System)

  • 나동하;고춘식;서형준;이창언
    • 드라이브 ㆍ 컨트롤
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    • 제9권4호
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    • pp.52-57
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    • 2012
  • In this study, in order to understand contents and ranges of design for the EGR Valve test system for improving quality and performance of EGR Valve, engine performance and exhaust gas characteristic of 3L-class diesel engine was analyzed. Experimental operation of engine performance test was performed with 50% engine load and 20% and 100% opening ratio of EGR Valve. From test of performance and exhaust gas characteristic of engine, torque output of engine and temperature and pressure of inlet and outlet of EGR Valve were measured. As a result, for design of EGR Valve test system, input fluid flow of EGR Valve must be set the same amount with exhaust gas flow that was below of engine speed of 2,500 rpm, and temperature of inlet of EGR Valve must be set under about $510^{\circ}C$. And the difference of temperature between inlet and outlet of EGR Valve must be over than about $200^{\circ}C$. Exhaust gas of inlet and outlet of EGR Valve were under 1 bar that was not considerable, and the difference of pressure between inlet and outlet of EGR Valve were under 1 bar that could not effect on mechanical operation of EGR Valve.

전자장비 구조기인소음 저감방안의 실험적 검토 (An Experimental Analysis of the Structure-Borne Noise Reduction on Electrical Equipment)

  • 이성현;서윤호;김원형;최영철
    • 한국음향학회지
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    • 제33권2호
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    • pp.111-117
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    • 2014
  • 본 논문은 전자장비의 구조기인소음 (structure-borne noise)의 실험적 저감방안 검토에 대한 내용을 다루었다. 수냉식 전자장비의 유일한 소음원인 냉각장치를 목업(mock-up)으로 제작하여 소음 특성을 파악하였으며, 전원에 의한 영향, 구조체 강성에 의한 영향, 팬 고정부위의 절연에 의한 효과, 마운트의 공진주파수가 미치는 영향 등에 대한 검토를 수행하였다. 이를 반영하여 제작된 전자장비 프로토타입의 소음 특성을 파악하였으며, 구조기인소음을 저감시키기 위하여 작동회전수(rpm) 조합, 마운트 종류 및 설치방법 등에 대하여 검토하였다. 냉각팬 작동 주파수의 1차, 4차 성분에 의하여 소음이 크게 발생하며, 구조체 강성증가, 팬 고정부위 절연, 마운트 공진주파수 저하, 작동회전수조합, 마운트 선정방법 등에 의하여 전자장비의 구조소음을 저감시킬 수 있음을 확인하였다.

"Inclined Keel" 컨테이너선의 조파저항 최소화를 위한 선형최적화 (Minimization of Wave-making Resistance for "Inclined Keel" Containership)

  • 서광철;;김희정;전호환
    • 대한조선학회논문집
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    • 제46권2호
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    • pp.97-104
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    • 2009
  • Ever increasing fuel prices, almost doubled in the last three years, and global pressure to reduce their environmental impact have been enforcing commercial vessel operators and designers to re-assess current vessel designs with emphasis on their propulsion systems and operational practices. In this paper the "Inclined Keel Hull (IKH)" concept, which facilitates to use larger propeller diameter in combination with lower shaft speed rates and hence better transport efficiency, is explored for a modern 3600 TEU container vessel with the aim of fitting an 13 % larger diameter propeller (and hence resulting 20% lower rpm) to gain further power saving over the similar size basis container ship with conventional "level keel" configuration. It appears that successful application of the "inclined keel Hull" concept is a fine balance amongst the maximum gain in propulsive efficiency, minimum increase in hull resistance and satisfaction of other naval architectural and operational requirements. In order to make the concept economically more viable, this paper concentrates on the fore body design with the possible combination of increase of volume in its fore body to recover the expected volume loss in the aft body due to the space for larger propeller and its low wave-making resistance to minimize the efficiency loss using a well-established optimization software.