• 한국기계가공학회지
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• 제21권8호
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• pp.53-59
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• 2022

In this study, an experimental device was fabricated to evaluate the hovering flight performance of a single rotor on a hexacopter used for river surveillance, and a thrust performance test was conducted. In addition, the 3D profile of the propeller was extracted by 3D scanning and CFD analysis was performed using ANSYS CFD 14.5 based on the extracted 3D model of the propeller. The aerodynamic characteristics were compared with the results of the performance tests and CFD analysis, and the vortex structure corresponding to each motor rotational speed in revolutions per minute (rpm) was identified. In the future, we plan to provide valuable data for multicopter propeller design and performance verification.

• 대한기계학회논문집B
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• 제39권8호
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• pp.669-675
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• 2015

자동차용 터보차저 원심압축기의 재순환케이싱처리(RCT)부의 높이변화가 압축기의 성능에 미치는 영향이 조사되었다. 연구대상 RCT 부의 높이는 1.2mm, 1.5mm, 1.8mm 의 세가지이며, 회전수 범위는 90,000 - 150,000 rpm, 유량 범위는 0.015 kg/s - 0.08 kg/s 이다. 전압력비와 등엔트로피 효율 비교 결과, 본 수치계산은 실제압축기의 성능 제원과 최대오차 0.7%의 범위 내에서 잘 일치하였다. 해석결과, RCT 부 높이 1.2mm, 1.8mm, 1.5mm 순서로 균일 압력분포, 높은 압력비, 넓은 작동범위를 얻었다. 이들 세가지 경우 모두, 회전수가 증가할수록 이들의 압력비는 높아지나 운전범위는 좁아지는 전형적인 압축기 맵의 특성을 보여주었다.

• 한국건설순환자원학회논문집
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• 제7권4호
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• pp.375-382
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• 2019

본 연구에서는 개발된 프린팅 재료 및 장비를 사용하여 대상 구조물의 시공성을 파악하기 위하여 기초 성능평가 프린팅 실험을 수행하였다. 3D 프린팅 콘크리트 구조물의 시공성은 콘크리트 필라멘트 재료 특성, 시공 프로세스 및 구조물의 기하특성에 영향을 받는다. 따라서, 콘크리트 구조물의 적층하는 동안의 시공성을 파악하기 위한 실험변수로서 노즐 이동속도(=80 및 100mm/s), 토출 버킷의 스크류 분당회전속도 (RPM) 및 구조물 벽체 길이의 변장비(1.67 및 5.00)를 고려하였다. 실험변수에 따른 3D 콘크리트 구조물의 최대 적층 수 및 파괴 패턴을 토대로 시공성을 분석하였다. 본 연구에서, 80mm/s의 노즐 이동속도 및 1.67의 변장비가 3D 프린팅 시공성에 유리함을 나타낸다. 또한, 적층 시 구조물 하단부의 상대변위측정을 통해 구조물의 전도 파괴 과정을 분석하였다.

• Restorative Dentistry and Endodontics
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• 제42권3호
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• pp.224-231
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• 2017

Objectives: To determine the actual revolutions per minute (rpm) values and compare the cyclic fatigue life of Reciproc (RPC, VDW GmbH), WaveOne (WO, Dentsply Maillefer), and TF Adaptive (TFA, Axis/SybronEndo) nickel-titanium (NiTi) file systems using high-speed camera. Materials and Methods: Twenty RPC R25 (25/0.08), 20 WO Primary (25/0.08), and 20 TFA ML 1 (25/0.08) files were employed in the present study. The cyclic fatigue tests were performed using a dynamic cyclic fatigue testing device, which has an artificial stainless steel canal with a $60^{\circ}$ angle of curvature and a 5-mm radius of curvature. The files were divided into 3 groups (group 1, RPC R25 [RPC]; group 2, WO Primary [WO]; group 3, TF Adaptive ML 1 [TFA]). All the instruments were rotated until fracture during the cyclic fatigue test and slow-motion videos were captured using high-speed camera. The number of cycles to failure (NCF) was calculated. The data were analyzed statistically using one-way analysis of variance (ANOVA, p < 0.05). Results: The slow-motion videos were indicated that rpm values of the RPC, WO, and TFA groups were 180, 210, and 425, respectively. RPC ($3,464.45{\pm}487.58$) and WO ($3,257.63{\pm}556.39$) groups had significantly longer cyclic fatigue life compared with TFA ($1,634.46{\pm}300.03$) group (p < 0.05). There was no significant difference in the mean length of the fractured fragments. Conclusions: Within the limitation of the present study, RPC and WO NiTi files showed significantly longer cyclic fatigue life than TFA NiTi file.

• Journal of Biosystems Engineering
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• 제40권1호
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• pp.10-18
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• 2015

Purpose: The study was conducted to investigate the proper working conditions like the mesh size of the concave and the chaffer angle of the oscillating sieve, and the fan speed of the head-feeding rice combine for foxtail millet harvesting. Methods: The study aimed to determine the harvesting conditions for the rice combine harvester at a 0.5 m/s working speed and at $40^{\circ}$ and $55^{\circ}$ sieve chaffer angles. The harvesting loss of the foxtail millet based on the speed of the fan and the oscillating speed of the sieve was measured at three levels of fan speed and oscillating sieve speed. Results: The threshing rates of different foxtail millet varieties were 64.1~83.5% at a mesh size of 7 mm of the concave. In experimental foxtail millet harvesting, the optimal operating condition of the rice combine harvester included a $40^{\circ}$ sieve chaffer angle and a 4.8 Hz oscillating sieve (cleaning shoe) frequency. The grain loss was found to be lower at a $40^{\circ}$ than at a $55^{\circ}$ sieve chaffer angle. In field harvesting using the combine harvester, the lowest harvesting grain loss rate of the foxtail millet varieties ranged between 0.2~0.5% at a 7 mm mesh concave, $40^{\circ}$ chaffer angle, 4.8 Hz sieve frequency, and a 20 m/s fan speed at an engine speed of 2,000 revolutions per minute (RPM). Conclusions: Findings showed that foxtail millet could be harvested using the combine harvester.

• Nuclear Engineering and Technology
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• 제53권8호
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• pp.2582-2590
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• 2021

The high-energy milling is one of the most extended techniques to produce Oxide dispersion strengthened (ODS) powder steels for nuclear applications. The consequences of the high energy mill process on the final powders can be measured by means of deformation level, size, morphology and alloying degree. In this work, an ODS ferritic steel, Fe-14Cr-5Al-3W-0.4Ti-0.25Y₂O₃-0.6Zr, was fabricated using two different mechanical alloying (MA) conditions (M_std and M_act) and subsequently consolidated by Spark Plasma Sintering (SPS). Milling conditions were set to evidence the effectivity of milling by changing the revolutions per minute (rpm) and dwell milling time. Differences on the particle size distribution as well as on the stored plastic deformation were observed, determining the consolidation ability of the material and the achieved microstructure. Since recrystallization depends on the plastic deformation degree, the composition of each particle and the promoted oxide dispersion, a dual grain size distribution was attained after SPS consolidation. M_act showed the highest areas of ultrafine regions when the material is consolidated at 1100 ℃. Microhardness and small punch tests were used to evaluate the material under room temperature and up to 500 ℃. The produced materials have attained remarkable mechanical properties under high temperature conditions.

• 농업과학연구
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• 제12권1호
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• pp.108-117
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• 1985

파종기(播種機)의 복토장치(覆土裝置) open auger의 토양이송과정(土壤移送過程)을 이론적(理論的)으로 분석(分析)하여 이송효율(移送效率)을 산출(算出)할 수 있는 이론적(理論的)인 동력효율식(動力效率式)을 유도(誘導)하고, open auger의 회전속도(回轉速度)의 적정범위(適定範圍), 그러고 auger 내(內)에서 토양(土壤)의 축방향(軸方向) 토립자(土粒子) 이송속도(移送速度)를 구명(究明)하였다. Open auger의 특성(特性)의 이론적(理論的)인 분석(分析)과 분석응용(分析應用)의 결과(結果)는 다음과 같다. 1. 동력효율(動力效率)의 예측식(豫測式)은 다음과 같다. ${\eta}_p={\frac{P_n}{P_g}}=({\frac{{\omega}_s}{{\omega}_a}}){\cdot}tan{\gamma}{\cdot}{\frac{mg}{F_mcos{\alpha}+F_scos{\gamma}}}$ 2. 보다 적은 동력(動力)으로 소정(所定)의 폭(幅)까지 토양이송(土壤移送)이 원활(圓滑)히 이루어질 수 있는 open auger의 회전속도(回轉速度)의 적정범위(適定範圍)는 다음과 같다. $$\frac{4d(L_a-L_i){\cdot}V_w}{{\pi}(D_o^2-D_s^2)r{\cdot}{\frac{{\omega}_s}{{\omega}_a}}{\cdot}tan{\gamma}}{{\leq_-}}{\omega}_a{{\leq_-}}({\frac{{\omega}_a}{{\omega}_s}}){\sqrt{\frac{g}{r}}}$$ 3. Auger 내(內)에서 토양(土壤)의 축방향(軸方向) 이송속도(移送速度)는 다음식(式)으로 구할 수 있다. $V_h=({\frac{{\omega}_s}{{\omega}_s}})V_a{\cdot}tan{\gamma}$ 4. Auger의 회전속도(回轉速度)는 다른 여러 인자(因子)들보다 동력효율(動力效率)에 가장 크게 영향(影響)을 미치는 것으로 나타났다.