• 한국정밀공학회지
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• 제3권3호
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• pp.40-71
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• 1986

By developing a computer program for the systematic design of worm gears, the design formulae and tables of AGMA, JGMA, BS and DIN are analized and compared. The computer program can be used on micro-computers. According to the input data of the reduction ratio, the center distance. the driving torque and the material as design parameters, the program calculate the most efficient worm gear dimension. The variation of the design parameters and other empirical coefficients in case of resulting an inadequate design gear dimension can be easily modified throuth the way of interactive method between the user and the monitoring system of computer. A proposal of the standardization of worm gears was made in which a standard module according to the DIN 323 standard series number was applied. For the more exact and effective calculation of the stress concentration and the deformation of gear teeth, a computer program using the boundary element method is also developed. Even the strength of the special gear shape such as Niemann's "Cavex" gear can be calculated in a short CPU-time. The most effort of this study has been layed on the developing a computer program for the correction of a tooth profile and face width which is most important design factor for an exact and wide teeth contacts under loads, especially by great and wide gears. For this purpose were investigated the tooth stiffness, the mesh interferences and the kinematics and the dynamics of gear mesh. The deflection and the deformation of the gear shaft due to the loads acting on gear and shaft were aslo considered. Some examples have shown the sufficient good status of teeth contact in which the correction of the tooth profile and face width were accomplished due to the calculated results.d results.

• 한국기계가공학회지
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• 제13권5호
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• pp.15-20
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• 2014

The wind industry grew in the first decade of the 21st century at rates consistently above 20% a year. For wind turbine, gearbox failure can be extremely costly in terms of repair costs, replacement parts, and in lost power production due to downtime. In this paper, gear tooth micro-modification for the high speed stage was used to compensate for the deformation of the teeth due to load and to ensure a proper meshing to achieve an optimized tooth contact pattern. The gearbox was firstly modeled in a software, and then the various combined tooth modification were presented, and the prediction of transmission under the loaded torque for the helical gear pair was investigated, the normal load distribution and root stress were also obtained and compared before and after tooth modification under one torque. The simulation results showed that the transmission error and normal load distribution under the load can be minimized by the appropriate tooth modification. It is a good approach where the simulated result is used to improve the design before the prototype is available for the test.

• 한국소성가공학회:학술대회논문집
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• 한국소성가공학회 2009년도 추계학술대회 논문집
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• pp.387-390
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• 2009

This study was designed to fabricate the micro-electro-mechanical systems (MEMS) parts such as micro spur gears using hot extrusion of gas atomized Al-78Zn powders. For this purpose, it is important to develop new methods to fabricate micro-dies and choose suitable extrusion conditions for a micro-forming. Micro-dies with Ni were fabricated by LIGA technology. LIGA technology was capable to produce micro-extrusion dies with close tolerances, thick bearing length and adequate surface quality. Superplastic Al-78Zn powders have the great advantage in achieving deformation under low stresses and exhibiting good micro formability with average strain rates ranging from $10^{-3}$ to $10^{-2}\;s^{-1}$ and constant temperatures ranging from 503 to 563K. Al-78Zn powders were compacted into a cylindrical shape (${\Phi}3{\times}h10$) under compressive force of 10kN and, subsequently, the compacted powders were extruded at 563k in a hot furnace. Micro-extrusion has succeeded in forming micro-gear shafts.

• 한국기계가공학회지
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• 제4권4호
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• pp.7-13
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• 2005

In the case of fabricating micro pole structures such as column, square-pole and gear shaft by the micro end-milling process, it can be useful in the fields of industry, for example, micro parts, electrode for electrical discharge machining and micro mold for injection molding. In this study, machining factors and the process were analyzed. Machining experiments of various micro pole configurations were performed. Analysis of the change and effect of the cutting force according to the machining conditions was carried out. An analytical study of the deformation of the micro pole caused cutting conditions and cutting force through the finite element method and ANSYS program was carried out. As a result, this research presented a method of fabricating the column pole of below $100{\mu}m$ diameter with high aspect ratio by using micro end-milling process, and based on that, a method of fabricating a variety of applicable structures. Also the minimum size of the pole capable of fabricating through theory and experiment were demonstrated.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2003년도 춘계학술대회 논문집
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• pp.589-592
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• 2003

In the machining process of micros shape by using high-precision machining system and micro end-mill, it is important for machining characters of tools to be grasped in order to stably use tools of micro end-mill. In this study. we carried out an analytical experiment of basic machining features by using end-mill tools for the purpose of damage prevention and manufacture of high quality when the tools of micro end-mill are used. This experiment used a micro machining system with high precision and a variety of end-mill tools commercialized from tens to hundreds microns in diameter. To establish an optimal machining condition without tool damage, cutting force was analyzed according to the changes of tool diameter and cutting conditions such as cutting speed. feed rate, depth of cut. And an examination was performed for the shape and surface illumination of machining surface according to the changes of machining conditions. Based on these micro machining conditions, micro square pillar, cylinder shaft. thin wall with high aspect ratio, and micro 3-D structures such as micro gear and fan were manufactured.

• 항공우주시스템공학회지
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• 제12권2호
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• pp.46-58
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• 2018

고해상도 관측위성의 대용량 영상 데이터 송신용인 2축 짐벌식 X-밴드 안테나는 궤도 임무수행 중 안테나 구동에 따라 미소진동을 유발하며, 이는 관측위성의 영상 품질을 저하시키는 요인 중 하나이기 때문에 반드시 절연되어야 할 대상이다. 본 논문에서는 상기 X-밴드 안테나의 방위각 구동에 따른 미소진동절연과 동시에 기존에 제안된 티타늄 블레이드 기어가 소성변형에 취약한 문제점을 보완하기 위해 초탄성 형상기억합금 (SMA)을 활용한 메쉬 와셔 기어를 제안하였다. 상기 SMA 메쉬 와셔 기어의 기본 특성을 파악하기 위해 SMA 메쉬 와셔 두께방향 정하중 시험과 SMA 메쉬 와셔 기어 수준의 회전방향정하중 시험을 실시하였다. 아울러 안테나 조립체 수준의 미소진동 측정시험을 통해 제안된 SMA 메쉬와셔 기어의 진동절연이 효과적임을 입증하였다.

• 농업과학연구
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• 제47권2호
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• pp.327-335
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• 2020

The purpose of this study was to analyze the load distribution and contact safety factor for the power take off (PTO) gear of a 71 kW class agricultural tractor. In this study, a simulation model of the PTO gear-train was developed using Romax DESGINER. The face load factor and contact safety factor were calculated using ISO 6336:2006. The simulation time was set at 2,736 hours considering the lifetime of the tractor, and the simulation was performed for each PTO gear stage at the engine rated power conditions. As a result of the simulation, the face load factors for the driving gear at the PTO 1^st, 2^nd and 3^rd stages were 1.644, 1.632, and 1.341, respectively. The contact safety factors for the driving gear at the PTO 1^st, 2^nd and 3^rd stages were 1.185, 1.216, and 1.458, respectively. As the PTO gear stage was increased, the face load factor decreased, and the contact safety factor increased. The load distributions for all the PTO gears were concentrated to the right of the tooth width. This causes stress concentrations and shortens the lifespan of the gears. Therefore, it is necessary to improve the face load factor and the contact safety factor with macro-geometry and micro-geometry.

• 한국전기전자재료학회논문지
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• 제29권12호
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• pp.796-802
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• 2016

In order to develop an electrical insulation material for gas GIS (insulation switch gear) spacer, 4 types of epoxy/micro-alumina (40, 50, 60, 70 wt%) composites and 9 types of epoxy/nano-alumina (1, 3, 5 g)/micro-alumina (40, 50, 60, 70 wt%) composites were prepared and tensile test was carried out. In here, nano-alumina was previously surface-treated with GDE (glycerol diglycidyl ether). As micro-alumina and GDE-treated nano-alumina contents increased, tensile strength increased and the highest value was shown in the system with 3 g GDE-treated nano-alumina.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2010년도 춘계학술대회 논문집
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• pp.687-688
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• 2010

• 대한기계학회논문집B
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• 제39권4호
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• pp.371-378
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• 2015

전기자동차 레인지 익스텐더는 소형 엔진으로 구동되는 발전기 시스템(초소형 파워팩)으로서 자동차 운행 중 지속 충전을 통하여 운전 거리 및 시간을 연장한다. 기존 가솔린 엔진 파워팩은 복잡한 구조와 낮은 에너지 밀도로 인하여 고출력 소형 시스템 구현에 한계가 있다. 반면, 가스터빈 파워팩은 출력밀도가 매우 높고 고속화를 통해 시스템의 소형화가 가능하다. 본 연구에서는 전기자동차 레인지 익스텐더로 활용하기 위하여 초소형 가스터빈, 자동차용 알터네이터, 배터리를 사용한 초소형 가스터빈 파워팩 실험장치를 개발하고, 무부하 및 부하 조건에서 동력전달 기어비 및 알터네이터 전기부하에 따른 운전 특성 및 발전 성능을 측정하였다. 실험 결과, 부하 변화에 따른 발전 성능의 변화는 없었으며, 코어터빈 속도가 150 krpm 일 때 최대 전기적 출력은 0.8 kW 로 측정되었다. 또한, 동력축의 3:1 감속을 통해 전기적 출력은 1.5 kW 로 88% 증가하였다. 따라서, 본 연구의 초소형 가스터빈 파워팩은 배터리 부하변동에 대해 안정적인 전력생산이 가능하며, 전기자동차용 레인지 익스텐더로 적용가능함을 확인하였다.