• Proceedings of the Korean Society of Precision Engineering Conference
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• 2001.10a
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• pp.101-105
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• 2001

고속절삭을 통해서 생산성과 가공정밀도의 향상을 도모할 수 있기 때문에, 최근 머시닝센터를 중심으로 한 공작기계 주축계의 고속화는 눈부시게 발전하고 있다. 그러나 주축계가 고속화될 수록 증가하는 베어링에서의 발열은 베어링의 수명단축, 주축계의 열변형 증대 등을 초래하고, 궁극적으로 공작기계의 성능을 저하시키게 된다. 따라서 고속으로 회전하는 베어링에서의 발열을 효과적으로 억제할 수 있는 윤활방법에 대한 연구들이 활발히 진행되고 있다. 따라서 본 연구에서는 공작기계용 고속주축계의 냉각특성을 규명하기 위한 노력의 하나로 압축공기를 이용한 고속주축 계의 냉각실험을 수행하였다. 고속주축계의 실험모델은 오일에어윤활방법, 앵귤러콘택트 볼베어링, 이중분사노즐, 냉각 자켓등을 사용해서 제작하였으며, 특히 고속주축계의 공기냉각방법에 대한 유용성은 실험결과로 부터 입증하였다.

• Journal of Space Technology and Applications
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• v.1 no.1
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• pp.7-22
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• 2021

In this paper, we describe the results of the docking phase test in the ground environment of the rendezvous/docking technology verification satellite under development for the first time in Korea. rendezvous/docking technology is a high-level technology in space technology, which is also very important for accessing and performing tasks on relative objects in space orbit. In this paper, we describe the ground test results that the chaser finally docks the fixed target using an air bearing device. Based on the thrust control algorithm in the docking phase and the relative object recognition and relative distance estimation algorithm using visual-based sensors validated in this paper, we intend to use them for later expansion to rendezvous/docking algorithms in three-dimensional space for testing in space.

• Journal of the Korean Society of Manufacturing Technology Engineers
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• v.19 no.4
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• pp.576-581
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• 2010

As a super high speed small-sized centrifugal separator which is operated by the center inputting method has solved two difficulty problems, it can be made use of developing the new composition through the making of Nano particle (50~100nm) by high speed revolution and alleviation of unbalanced shapes inside the disk continuously throwing slurry in the central part. Uses the air spindle and the centrifugal machine production will be able to manufacture the Roh class fine particle under boil.

• Proceedings of the Korean Society of Precision Engineering Conference
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• 2008.11a
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• pp.463-464
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• 2008

• Proceedings of the Korean Society of Precision Engineering Conference
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• 2009.06a
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• pp.485-486
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• 2009

• Proceedings of the Korean Society of Precision Engineering Conference
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• 2009.10a
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• pp.23-24
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• 2009

• Journal of the Korean Society for Precision Engineering
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• v.18 no.2
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• pp.96-101
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• 2001

This paper shows the temperature characteristics of a high speed angular contact ball gearing which is 7004C type with ISO P2 tolerance class. A built-in motor type high speed spindle which adopts an oil-air lubrication system was used to measure the temperature rise up to 60,000rpm. The gearing temperature was measured using thermocouples that were attached to the outside surfaces of the outer rings. The result showed that the continuous test method which was suggested in this paper is more effective than on and off method and the lubrication oil supply rate should be reduced in high speed rolling bearings as long as the seizure does not occur. And the result were confirmed that the bearings packed with ceramic balls are superior to those with steel balls in temperature characteristics.

• Tribology and Lubricants
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• v.16 no.4
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• pp.247-252
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• 2000

As the demand for higher areal recording densities requires a lower flying height of the slider, the variation of the flying height of the slider during drive operation becomes of great concern. The variation of the flying height is closely related with the slider design parameters such as air bearing shape, cavity depth, shallow step depth, crown, camber, pitch offset, roll offset, gram load, and so on. The objective of this work is to optimize the cavity depth and the shallow step depth, which are the control factors in air bearing design, using Robust Design method. It was found that the shallow step depth was statistically significant in affecting the variation of flying height, therefore the level of the shallow step depth should be chosen to minimize the variation of flying height.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2003.05a
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• pp.1107-1114
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• 2003

In this thesis, the dynamic characteristic analysis of carriage structure supported by air bearings were peformed. Toward this end, the characteristics of air bearing were numerically analyzed to estimate the stiffness of the air bearing and the clearance between air bearing and guide surface. The modal analysis of the carriage structure was peformed by using finite element method, and the experimental modal analysis was also performed to validate the finite element model, where rigid body modes were compared to validate the stiffness of the air bearings. From the results, the air spring stiffness can be estimated within the range of acceptable accuracy under any pressure and clearance condition.

• The Bulletin of The Korean Astronomical Society
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• v.37 no.2
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• pp.202-202
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• 2012

항공우주연구원에 설치되어있는 태양전지판 무중력 전개시험장치는 지상 전개시험 시 지구 자중으로 인해 발생하는 하중과 마찰력을 상쇄하여 우주 궤도상에서 전개되는 것과 동일하게 태양전지판이 전개되도록 구성되어 있다. 이를 위해 에어베어링을 사용하여 전개 시 발생할 수 있는 전개방향으로의 마찰력을 상쇄하고, 지구 중력으로 인한 영향이 없도록 하기 위해 중력축에 대해 각 레일이 수평이 되도록 정밀하게 정렬되어야 한다. 본 연구에서는 천리안위성의 정밀조립 및 전개시험에 사용되었던 태양전지판 무중력 전개시험장치를 차기 정지궤도위성의 대형 태양전지판에 적용하였을 때에도 전개시험이 가능한 지를 카티아 디지털 목업 시뮬레이션을 사용해 모사하고 검토되어야 할 주요 사항들에 대해 분석하였다.