• 한국유체기계학회 논문집
• /
• 제19권1호
• /
• pp.24-30
• /
• 2016

In this study, a 2W micro-gas turbine engine was designed using micro-electro-mechanical systems (MEMS) technology, and experimental investigations of its potential under actual combustion conditions were performed. A micro-gas turbine (MGT) contains a turbo-charger, combustor, and generator. Compressor and turbine blades, and generator coil were manufactured using MEMS technology. The shaft was supported by a precision computer numerical control (CNC) machined static air bearing, and a permanent magnet was attached to the end of the shaft for generation. A heat transfer analysis found that the cooling effect of the air bearing and compressor was sufficient to cover the combustor's high temperature, which was verified in an actual experiment. The generator performance test showed that it can generate 2W at design rotational speed. Prototype micro-gas turbine generated maximum 1 mW electric power and lasted up to 15 minutes.

• 대한기계학회:학술대회논문집
• /
• 대한기계학회 2005년도 창립60주년 기념 추계 학술대회
• /
• pp.199.1-199.1
• /
• 2005

• 한국정밀공학회:학술대회논문집
• /
• 한국정밀공학회 2010년도 춘계학술대회 논문집
• /
• pp.777-778
• /
• 2010

• Steel and Composite Structures
• /
• 제43권6호
• /
• pp.773-784
• /
• 2022

This paper aims to investigate the axial compressive behavior of reinforced concrete (RC) columns strengthened with self-compacting and micro-expanding (SM) concrete-filled steel tubes (SM-CFSTs). Nine specimens were tested in total under the local axial compression. The test parameters included steel tube thickness, filling concrete strength, filling concrete type and initial axial preloading. The test results demonstrated that the initial stiffness, ultimate bearing capacity and ductility of original RC columns were improved after being strengthened by SM-CFSTs. The ultimate bearing capacity of the SM-CFST strengthened RC columns was significantly enhanced with the increase of steel tube thickness. The initial stiffness and ultimate bearing capacity of the SM-CFST strengthened RC columns were slightly enhanced with the increase of filling concrete strength. However, the effect of filling concrete type and initial axial preloading of the SM-CFST strengthened RC columns were negligible. Three equations for predicting the ultimate bearing capacity of the SM-CFST strengthened RC columns were compared, and the modified equation based on Chinese code (GB 50936-2014) was more precise.

• 한국정밀공학회:학술대회논문집
• /
• 한국정밀공학회 2008년도 추계학술대회 논문집
• /
• pp.547-548
• /
• 2008

• 한국유체기계학회 논문집
• /
• 제18권5호
• /
• pp.42-48
• /
• 2015

To improve the core technology of the micro gas turbine, the performance test facility was developed. This paper is focusing on the explanation of the characteristics of micro gas turbine and its assist devices. Major part of micro gas turbine were radial type of compressor, annular type of combustor, radial type of turbine, thrust foil bearing, radial foil bearing and generator. The assist devices were consist of exhaust duct, inverter, data acquisition system, load bank and test cell. Before building up the test facility, the component test was previously conducted to confirm the component performance. After the test facility was prepared, the motoring test was conducted to investigate the rotor dynamic characteristics of the micro gas turbine. Also, the part load performance test was performed. With a developed micro gas turbine test facility, the improved core technology about the micro gas turbine can be suggested to the related industries.

• 대한기계학회논문집A
• /
• 제37권4호
• /
• pp.437-442
• /
• 2013

마찰을 크게 줄임과 동시에 신뢰성을 향상시키기 위하여 평행 스러스트 베어링, 메카니컬 시일과 피스톤링 등과 같은 기계부품에 표면가공방법이 최근에 적용되고 있다. 본 논문에서는 상용 전산유체역학 S/W인 FLUENT를 사용하여 반구형 미세딤플이 등간격으로 배치되어 있는 슬라이더 베어링의 윤활특성을 조사하였다. 미세딤플의 직경과 수에 따라서 압력분포, 지지하중, 누설유량과 마찰력은 아주 크게 변화하였다. 특히, 딤플의 밀도증가에 따라서 지지하중과 마찰력은 거의 선형적으로 감소하는 반면에 누설유량은 급격하게 증가하였다. 본 논문의 결과는 각종 미끄럼 베어링의 윤활성능을 향상시키기 위한 최적 딤플설계에 사용할 수 있으며, 추가적인 연구가 요구된다.

• 한국지반신소재학회논문집
• /
• 제13권4호
• /
• pp.161-167
• /
• 2014

본 연구에서는 교대에 인접하여 시공된 보강토옹벽에서 발생한 구조물 변형에 대한 원인을 분석하였으며, 이를 바탕으로 시공된 보강토옹벽의 단면을 유지함과 동시에 구조물의 안정성을 확보할 수 있도록 마이크로 파일을 이용한 보강방안에 대하여 안정성을 평가하였다. 연구대상 구조물의 지속적인 변형은 구조물의 주변환경 조건에 큰 영향을 받은 것으로 나타났으며, 이는 기초지반의 지지력을 감소시켜 중요구조물로서의 안정성 저해요인으로 작용하였다. 이에 보강토옹벽의 지지력 및 전체사면에 대한 안정성을 확보할 수 있도록 보강방안으로 마이크로 파일을 적용하였으며, 이에 대한 안정성 평가 결과, 구조물의 변형 및 구조물을 포함하는 전체사면에 대한 안정성을 확보할 수 있는 것으로 확인되었다. 즉, 시공여건 및 주변환경 조건에 의해 보강토옹벽의 재시공이 불가능한 경우에는 마이크로 파일을 이용한 보강이 충분히 가능한 것으로 판단되었다.

• 소성∙가공
• /
• 제11권7호
• /
• pp.620-627
• /
• 2002

The purpose of this paper is the development of an automated measurement system for micro spring based on the digital image processing technique. This micro spring can be used in various engineering applications such as filament, load bearing springs, hard disk suspension and many others. Main functionality of the micro spring inspection system is to measure the representative pitch of the micro spring. The derivative operators are used for edge detection in gray level image. Measurement system developed in this paper consisted of new auto feeding mechanism to take advantage of air pressure. In the process of development of the micro spring inspection system based on the image processing and analysis, strong background technology and know-how have been accumulated to measure micro mechanical parts.

• 동력기계공학회지
• /
• 제17권4호
• /
• pp.139-146
• /
• 2013

Because the magnetic bearing supports levitating body without contact, wear, noise and vibration, it is very useful to high revolution machinery. In this paper we selected ATmega 128, a less expensive and widely used micro controller, for control the magnetic bearing system. And we selected the sampling time and the control gain of PID controller through trial-and-error. The control program of the one board controller utilized lookup table to reduce calculation time, and bit shifting for the integer calculation in instead of floating point calculation. As the results, the controller carried out relatively high speed PID control on sampling time 0.25 ms. At last the rotation test for the magnetic bearing system was carried out by 3 phase induction motor and air turbine.