• Proceedings of the Korean Society of Precision Engineering Conference
• /
• 2002.10a
• /
• pp.181-184
• /
• 2002

In these day, fabrication technologies for micro parts become more important with the increase of interest on microsystem and developed through the various approaches in the whole world. Among these technologies; micro mechanical machining is one of the most effective methods for the fabrication of micro parts. In this study, we fabricated micro shafts using micro endmill and micromachining system and measured the cutting force at the process. Also, Based on the data, we simulated the deformation of micro shafts due to the cutting force. Through the simulation results, it was verified that the cutting force at the process is enough to cause dimensional error at the micro shafts.

• Journal of the Korean Society for Heat Treatment
• /
• v.14 no.6
• /
• pp.371-377
• /
• 2001

스테인리스강의 주요 특징은 우수한 내식성에 있다. 그럼에도 불구하고 스테인리스강은 질화시키면 스테인리스강의 주요 특징인 내식성의 저하가 불가피하다. 그러나 경우에 따라서는 내식성이 다소 희생되더라도 내모성 향상을 목적으로 SUS 304소재를 이용한 피스톤링이나 SUS 420 J2소재를 사용하는 마이크로 샤프트 등과 같은 많은 제품에 대하여 질화처리를 실시하고 있다. 스테인리스 제품에 얼룩이 없는 질화처리를 실시하기 위해서는 앞에서 소개한 방법 이외에 표면활성화를 위한 분말처리법 등이 많이 사용되고 있으며, 그 예로 일본의 마테크(주)에서 제조하여 (주)사마루에서 시판하고 있는 활성분체질화제(APN법, DCA)을 사용하여 질화시키는 방법등도 있다. 이와 같이 외국에서는 프라즈마법이 아닌 일반 가스질화에 의한 스테인리스강의 질화에 대한 많은 연구가 이루어지고 산업화 되어 있지만 현재 국내에서는 이에 대한 연구가 거의 이루어지고 있지 않은 실정이다. 따라서 앞으로는 국내에서도 이러한 분야에 대한 보다 많은 관심과 연구 및 기술보고 등이 활성화되어야 할 것으로 생각된다.

• 유체기계공업학회:학술대회논문집
• /
• 2001.11a
• /
• pp.361-366
• /
• 2001

A mim turbo-shaft engine of 50HP for UAV, which can be easily modified to turbo-prop and turbo-jet engine by sharing the core engine and has many applications to civilian demands and munitions, will be developed This kind of micro gas turbine engine has been developed mostly by the corporations which have special technology but are small in its scale. Especially, the gas turbine engine can be easily applied to other fields and developed by domestic technology, so that the sharing of technology is planed to realize through the cooperations with academies and research institutes. In this paper, the gas turbine engine, which has the compressor ratio of 3.8, the turbine inlet temperature of l180K and the engine speed higher than 100,000 rpm, is composed of centrifugal compressor, combustor, gas generator turbine, free power turbine and gear box. The competitiveness of the gas turbine engine can be obtained from minimizing its cost by the utilization of domestic infrastructure for the performance test and the decisive outsourcing.

• Transactions of the Korean Society of Mechanical Engineers
• /
• v.15 no.1
• /
• pp.90-97
• /
• 1991

A stepping motor can be driven with open-loop or closed-loop control. The major disadvantage of open-loop control is that it is subjected to resonance and instability in certain speed range, and that there is no way to check stalling or error in position. In this paper, a closed-loop control system consisting of a microcomputer, a hybrid stepping motor, a drive, a lead screw, and an encoder which is used as a position sensor is developed. A control program is programmed in assembly language for real time control and the versatile interface adapter(VIA) is used as the interface with the microcomputer. The experimental results of the stepping motor were eliminated on all kinds of inertia load, and maximum start stop pulse rate and maximum slewing pulse rate were also increased about twice respectively.