• Tribology and Lubricants
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• 제34권3호
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• pp.75-83
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• 2018

Microturbomachinery (< 250 kW) using gas foil bearings can function without oil lubricants, simplify rotor-bearing systems, and demonstrate excellent rotordynamic stability at high speeds. State-of-the-art technologies generally use bump foil bearings or leaf foil bearings due to the specific advantages of each of the two types. Although these two types of bearings have been studied extensively, there are very few studies on leaf-bump foil bearings, which are a combination of the two aforementioned bearings. In this work, we illustrate a simple mathematical model of the leaf-bump foil bearing with leaf foils supported on bumps, and predict its static and dynamic performances. The analysis uses the simple elastic model for bumps that was previously developed and verified using experimental data, adds a leaf foil model, and solves the Reynolds equation for isothermal, isoviscous, and ideal gas fluid flow. The model predicts that the drag torques of the leaf-bump foil bearings are not affected significantly by static load and bearing clearance. Due to the preload effect of the leaf foils, rotor spinning, even under null static load, generates significant hydrodynamic pressure with its peak near the trailing edge of each leaf foil. A parametric study reveals that, while the journal eccentricity and minimum film thickness decrease, the drag torque, direct stiffness, and direct damping increase with increasing bump stiffness. The journal attitude angle and cross-coupled stiffness remain nearly constant with increasing bump stiffness. Interestingly, they are significantly smaller compared to the corresponding values obtained for bump foil bearings, thus, implying favorable rotor stability performance.

• 한국항공우주학회지
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• 제44권5호
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• pp.381-390
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• 2016

본 연구에서는 이중구조팬의 소음특성을 알아보고 소음저감 방법으로 알려진 톱니형 뒷전(Serrated Trailing Egde)을 적용하여 이중구조팬의 소음을 저감시켰다. 해석에는 Lattice Boltzmann Method(LBM)를 이용한 비정상 전산해석을 수행하였으며 해석의 타당성을 평가하기 위하여 시험을 실시하였다. 이중구조팬은 일반적인 팬처럼 단일의 Blade Passing Frequency(BPF)를 갖는 것이 아니라 내부팬과 외부팬 각각의 BPF가 서로 다른 음역대에서 나타나는 것을 확인 하였다. 톱니형 뒷전을 내부팬에 적용하여 경계층에서의 구속와류와 뒷전에서의 와류흘림이 억제 또는 분산되고 광역소음뿐만 아니라 팬의 토크도 저감되었다.

• 대한기계학회논문집A
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• 제38권4호
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• pp.437-442
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• 2014

원자력 발전소의 터빈-발전기 시스템과 같이 일정한 토크와 함께 축 진동에 의한 가변 응력이 인가되는 부재의 경우 비틀림 응력에 의한 피로 파괴 거동을 보인다. 따라서 본 연구에서는 터빈-발전기의 터빈 축에 인가하는 비틀림 응력을 측정하고 응력에 의해 발생하는 피로 파괴 거동을 분석하는 것을 목적으로 하였다. 이를 위해 터빈-발전기 시스템과 같은 실험 장치를 제작하고 임의의 부하를 인가하여 다양한 비틀림 응력에 대한 피로 파괴 거동을 평가하였다. 특히 기존의 알려진 피로 거동 평가 방법인 응력-수명, 변형률-수명, 균열성장 평가 방법을 동시에 적용하여 평가를 진행하였다. 부하의 크기가 증가하면서 평가 방법과 무관하게 피로 수명이 감소하는 경향이 확인하였으며 5 kV 부하 인가 시 최대 10배의 피로 수명의 감소가 발생하였다.

• 한국측량학회지
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• 제27권2호
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• pp.187-194
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• 2009

지상용 3차원 레이저 스캐너를 설계하고 개발하는데 있어서 위치 측정 결과의 정확성을 향상하기 위한 서보 모터의 선정과 서보 모터 FOC(Field Oriented Control) 제어 방식의 적용에 대한 연구이다. 개발 중인 지상용 3차원 레이저 스캐너는 360$^\circ$방위각과 270$^\circ$고도각의 스캔 범위를 가지고 있다. 이의 구현은 서보 모터인 방위각 모터와 고도각 모터의 정밀한 서보 모터 제어를 통해 실현된다. 연구 결과 FOC(Field Oriented Control)제어를 통해서 모터의 일정한 토크를 유지하면서 모터의 동작 위치 정확도를 향상할 수 있음을 확인하였다. 이러한 모터 제어는 지상용 3차원 레이저 스캐너뿐만 아니라 로보틱 토털스테이션에도 적용이 가능 할 것으로 사료된다.

• 한국정밀공학회지
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• 제29권2호
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• pp.129-138
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• 2012

In this study, three types of large scale multi-tasking machine tools together with core technologies involved have been developed and introduced; a multi-tasking machine tool for large scale marine engine crankshafts, a multi-tasking vertical lathe for windmill parts, and a large scale 5-axis machine tool of gantry type. Several special purpose devices has been necessarily developed for the purpose of handling and machining big and heavy workpieces accurately, such as PTD (Pin Turning Device) with revolving ring spindle for machining eccentric crankshaft pins, hydrostatic rotary table and steady rest for supporting and resting heavy workpieces, and 2-axis automatic swiveling head for high-quality free surface machining. Core technologies have been also developed and adopted on their detail design stage; 1) structural design optimization with FEM structural analysis, 2) theoretical hydrostatic analysis for the PTD and rotary table bearings, 3) box-in-box type cross-rail and octagonal ram design to secure machine rigidity and accuracy, 4) constant spindle rpm control against gravitational torque due to unbalanced workpiece.

• 농업과학연구
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• 제49권4호
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• pp.845-855
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• 2022

The purpose of this study is to develop a self-propelled underground crop harvester and its performance was evaluated by measuring the load during actual potato harvesting operations. This study was conducted at a constant working speed of 1 km·h^-1. A load measurement system was installed to measure the actual load and the required working power was analyzed. A hydraulic pressure sensor was also installed to measure the hydraulic pressure. The required hydraulic power was calculated using the hydraulic pressure and flow rate. The results showed that the engine speed, torque, and power during harvesting operation were in the range of 845 - 1,423 rpm, 95 - 228 Nm, and 9 - 31 kW, respectively. Traction power, excluding the hydraulic pump of the tractor and power take-off (PTO) output, was in the range of 9 - 28 kW, and it was confirmed that it occupies a ratio of 16.2 to 50% of the engine rated output. The engine can supply the minimum required traction power to move the vehicle. This means that the engine used in this study could be down-sized to be suitable for an underground crop harvester. In this study, the gear stages of the tractor were not considered. This research thus shows the possibility of developing a self-propelled underground crop harvester.

• Smart Structures and Systems
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• 제29권5호
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• pp.661-675
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• 2022

In this paper, an electric vehicle drives with efficient control and low cost hardware using four quadrant DC converter with Permanent Magnet Direct Current (PMDC) motor fed by DC boost converter is presented. The main idea of this work is to improve the energy efficiency of the conversion chain of an electric vehicle by inserting a boost converter between the battery and the four quadrant-DC motor chopper assembly. Consequently, this method makes it possible to maintain the amplification gain of the 4 quadrant chopper constant regardless of the battery voltage drop and even in the presence of a fault in the battery. One of the most important control problems is control under heavy uncertainty conditions. The higher order sliding mode control technique is introduced for the adjustment of DC bus voltage and mechanical motor speed. To implement the proposed approach in the automotive field, experimental tests were carried out. The performances obtained show the usefulness of this system for a better energy management of an electric vehicle and an ideal control under different operating conditions and constraints, mostly at nominal operation, in the presence of a load torque, when reversing the direction of rotation of the motor speed and even in case of battery chamber failure. The whole system has been tested experimentally and its performance has been analyzed.

• 대한토목학회논문집
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• 제29권4A호
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• pp.291-297
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• 2009

실험을 통해 고장력 볼트의 릴렉세이션를 측정하였다. 종류와 표면 처리가 다른 볼트를 사용하여 체결길이가 서로 다른 블록형태와 겹침이음형태의 시험체를 조립하였다. 항온항습실에서 시간 경과에 따라 볼트에 도입된 축력을 변형률 게이지를 통하여 측정하였다. 볼트축력의 감소율은 모든 시험체에서 10% 미만으로 나타났다. 결합 형태, 볼트종류, 체결길이 그리고 볼트의 표면 처리가 서로 다른 여러 경우에 대해 실험결과를 이 연구에서 제안한 릴렉세이션 추정 모델을 이용하여 비교, 검토하였다. 제안한 모델은 여러 경우에 대한 실험 결과와 모두 합리적으로 잘 합치하고 있다. F13T와 F10T 볼트사이에 차이점을 발견할 수 없으나 다크로 볼트의 최종 체결력 감소율은 일반 볼트보다 30% 정도 높으며, 또한 전체적으로 볼트 체결길이가 짧아짐에 따라, 전단면의 수가 증가함에 따라 높아지는 경향을 보여주고 있다.

• Restorative Dentistry and Endodontics
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• 제31권6호
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• pp.477-484
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• 2006

학생들이 사용한 세 가지 NiTi file systems (ProFile$^{(R)}$, Hero Shaper$^{(R)}$, K3$^{TM}$)을 사용하여 성형한 모형 근관의 apical terminus width를 비교하여 flute angle 및 pitch 혹은 radial land가 screw-in effect에 미치는 효과를 알아보고자 하였다. NiTi file의 사용 경험이 없는 부산대학교 치과대학 4학년 학생 50명이 세 종류의 NiTi file systems- Pro File$^{(R)}$ (Dentsply Maillefer, Ballaigues, Switzerland), K3$^{TM}$ (SybronEndo, Glendora, France), Hero Shaper$^{\circledR}$(Micromega, Besancon, France)-을 사용하여 각 system으로 하나의 근관씩, 모두 150 개의 레진 블락 근관모형 (Endo Training Bloc; Dentsply Maillefer, Ballaigues, Switzerland)을 16 : 1 감속 handpiece를 장착한 electric motor (Tecnika ATR, Pistola, Italy)를 사용하여 300 rpm의 속도에서 torque는 30 (Tecnikamotor setting value)으로 성형하였다. 스캐너로 근관 성형 전 후 이미지를 채득하여 중첩한 후 근단부의 최종 폭경을 측정하였다. 통계분석은 one-way ANOVA와 95% 신뢰도의 Scheffe's multiple range test로 사후 검증하였다. ProFile$^{(R)}$의 근관 성형 후 근단부의 폭이 Hero Shaper$^{(R)}$ and K3$^{TM}$에 비해 통계학적으로 유의하게 작았다. 본 연구의 결과에서 근단부의 과도한 확대가 variable pitch와 helical angle를 가진active file에 비해 con-stant pitch와 helical angle을 가짐에도 불구하고 radial land를 가진passive file에서 적게 나타났다. 이 결과로 추정해 볼 때, variable pitch와 helical angle보다는 근본적으로 radial land가 screw-in effect의 예방에 더 큰 역할을 하는 것으로 추정될 수 있다 따라서 NiTi file의 사용 경험이 없는 초심자의 경우 근단부 폭경의 유지능력이 좋은 ProFile$^{(R)}$의 사용이 추천된다.

• Journal of Advanced Marine Engineering and Technology
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• 제8권1호
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• pp.17-36
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• 1984

Since 1973, the competition on the development of fuel saving type internal combustion engines has become severe by the two times oil shock, and new type engines are reported every several months. Whenever these new type engines are developed, new designs are required and they will be offered in the market after performing the endurance test for a long time. But the engine market is faced with a heavy burden of finance, as the developing of a new engine requires tremendous expenses. For this reason, the computer simulation method has been lately developed to cope with it. The computer simulation method can be available to perform the reasonable research works by the theoretical analysis before carrying out practical experiments. With these processes, the developing expenses are cut down and the period of development is curtailed. The object of this study is the development of simulation computer program for the small naturally aspirated four-stroke diesel engine which is intended to product by the original design of our country. The process of simulation is firstly investigated for the ideal engine cycle, and secondly for the real engine cycle. In the ideal engine cycle, each step of the cycle is simulated by the energy balance according to the first law of thermodynamics, and then the engine performance is calculated. In the real cycle imulation program, the injection rate, the preparation rate and the combustion rate of fuel and the heat transfer through the wall of combustion chamber are considered. In this case, the injection rate is supposed as constant through the crank angle interval of injection and the combustion rate is calculated by the Whitehouse-Way equation and the heat transfer is calculated by the Annand's equation. The simulated values are compared with measured values of the YANMAR NS90(C) engine and Mitsubishi 4D30 engine, and the following conclusions are drawn. 1. The heat loss by the exhaust gas is well agree with each other in the lower load, but the measured value is greater than the calculated value in the higher load. The maximum error rate is about 15% in the full load. 2. The calculated quantity of heat transfer to the cooling water is greater than the measured value. The maximum error rate is about 11.8%. 3. The mean effective pressure, the fuel consumption, the power and the torque are well agree with each other. The maximum error is occurred in the fuel consumption, and its error rate is about 7%. From the above remarks, it may be concluded that the prediction of the engine performance is possibly by using the developed program, although the program needs to reform by adding the simulation of intake and exhaust process and assumping more reliable mechanical efficiency, volumetric efficiency, preparation rate and combustion rate.