• 제목/요약/키워드: Micro-gear

검색결과 73건 처리시간 0.025초

정밀소형회전기구의 마모해석모델에 관한 연구 (Development of Wear Analysis Model of Precision Small Rotating Device)

  • 여은구;조선형;이용신
    • 한국소성가공학회:학술대회논문집
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    • 한국소성가공학회 2003년도 춘계학술대회논문집
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    • pp.355-358
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    • 2003
  • Recently, micro forming process technology have been developed since the size of machine parts become the crucial factor for minimizing of products in general electronic products. Most small machine parts consist of gear and rotation axis and the wear by mechanical contact is known as the primary factor for life reduction of high precision machine part. Lots of studies for mechanical wear and friction have been reported and many researches of MEMS technology have been studied recently. But just few studies for wear of micro or milli sized machine part have teen implemented. In this research, the wear equation is suggested according to the contact shape of axial part in micro or milli sized machine part. And wear analysis model which can predict the magnitude of wear through this suggested equation with numerical analysis program.

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Tribology Characteristics of Hexagonal Shape Surface Textured Reduction Gear in Electric Agricultural Vehicle

  • Choi, Wonsik;Pratama, Pandu Sandi;Byun, Jaeyoung;Kwon, Soonhong;Kwon, Soongu;Park, Jongmin;Kim, Jongsoon;Chung, Songwon
    • 한국산업융합학회 논문집
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    • 제22권1호
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    • pp.47-54
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    • 2019
  • An experimental study was conducted on the wear and friction responses in sliding tests of a micro-textured surface on laser pattern (LP) steel as reduction gear material in electric guided vehicle. In this research, the friction characteristics of laser pattern steel under different micro texture density conditions were investigated. The friction tests were carried out at sliding speeds of 0.06 m/s to 0.34 m/s and at normal loads of 2 to 10 N. Photolithography method was used to create the dimples for surface texturing purpose. Four different specimens having different dimple densities of 10%, 12.5%, 15%, and 20% were observed respectively. In this research, friction conditions as shown in Stribeck curve were investigated. Furthermore, the microscopic surface was observed using scanning electron microscope. It was found that the dimple density had a significant role on the friction characteristics of laser pattern steel conditioned as reduction gear material in an agricultural vehicle. The duty number showed that the friction condition was hydrodynamic regime. The best performance was obtained from 12.5% dimple density with lowest friction coefficient achieved at 0.018771 under the velocity of 0.34 m/s and 10N load.

하이브리드 쾌속 조형을 이용한 나노 복합재의 조형 (Fabrication of Nano Composites Using Hybrid Rapid Prototyping)

  • 추원식;김성근;안성훈
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2005년도 춘계학술대회 논문집
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    • pp.757-760
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    • 2005
  • The technology of rapid prototyping (RP) is used for design verification, function test and fabrication of prototype. The current issues in RP are improvement in accuracy and application of various materials. In this paper, a hybrid rapid prototyping system is introduced which can fabricate nano composites using various materials. This hybrid system adopts RP and machining process, so material deposition and removal is performed at the same time in a single station. As examples, micro gears and a composite scaffold were fabricated using photo cured polymer with nano powders such as carbon black and hydroxyapatite. From the micro gear samples the hybrid RP technology showed higher precision than those made by casting or deposition process.

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피팅 파손면적분석기법을 이용한 기어재의 피팅 수명 실험 (Pitting Life Experiments of Gear Material using a Damaged Area Analysis Method)

  • 주진욱;이병욱;문석만;김태완;조용주
    • 한국정밀공학회지
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    • 제27권11호
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    • pp.92-97
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    • 2010
  • The object of this study is to investigate the definite method for pitting damaged surfaces. Pitting is a sort of fatigue damages and it is made by a repetitive load. For a judgment between damages or not, sensing vibrations of test equipment is simple. However, it is not only difficult to observe a growth of pitting but also impossible to detect the juncture of initial pitting. Therefore, a method for the pitting damaged area measuring technique was effectively implemented by Two Roller Machine. The change of surface damaged area was measured by an optical microscope in regular time and calculated by the use of dark and bright ratio of test specimens' pictures taken by optical microscope. In conclusion, S - N Curves gained by Failure rate - Cycle graph was led and the curves are able to be chosen as occasion demands for a failure area percentage.

초소형 날갯짓 비행체의 최적 날갯짓 속도 분포 연구 (Velocity Profile Optimization of Flapping Wing Micro Air Vehicle)

  • 조선규;이준희;김종암
    • 한국항공우주학회지
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    • 제48권11호
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    • pp.837-847
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    • 2020
  • 본 논문에서는 20g급 날갯짓 초소형 비행체의 정지 비행 시의 날갯짓 효율을 증가시키기 위한 날갯짓 속도 분포 최적화를 진행하였다. 비원형 기어를 이용하여 다양한 날갯짓 속도 분포를 나타내는 메커니즘을 설계하였으며, 실증 기체를 이용하여 실험적으로 날갯짓 속도 분포 최적화를 진행하였다. 최적화 모델은 노이즈를 포함한 Kriging을 사용하였으며 불확실성에 의한 오차를 반영하였다. 날갯짓 속도 분포를 네 개의 파라미터로 나타내어 각 파라미터에 대한 최적화를 진행하였고. 최적화 결과 추력-파워비가 11.3% 증가하였다. 추력-파워비가 증가한 이유에 대해 탄성력에 의해 이전 스트로크에서의 각운동에너지가 일부 보존되어 다음 스트로크에서 사용되어 효율이 높아진 것으로 분석하였다.

지향성을 가지고 동작하는 위성 안테나 진동저감 장치 (Vibration Reduction Device for Directional Moving Satellite Antenna)

  • 최석원;용상순
    • 우주기술과 응용
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    • 제2권3호
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    • pp.187-194
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    • 2022
  • 안테나의 고속 정밀 지향성 확보를 위해 동작되는 모터의 구동에 의한 외란의 크기는 극히 미소함에도 불구하고, 정밀 지향 성능이 요구되는 관측 위성의 영상 품질을 저해하는 주요 원인으로 작용하게 된다. 고해상도 관측위성의 지향 성능 향상을 통한 고해상도 영상정보 획득을 위해서는 지향성 안테나의 모터 구동시 발생하는 미소진동(Jitter)이 주요 임무 장비에 전달되지 않도록 적절한 진동절연 및 저감 설계가 요구된다. 본 논문에서는 실제 위성에 적용된 지향성 안테나 진동저감 장치에 대해 개발과정과 적용 전후의 미소 진동 저감 효과에 대해 살펴보고자 한다. 이 장치는 별다른 인터페이스 추가 장비 없이, 지향성 안테나 구동부 내에 있는 기어 하나만을 스프링 댐퍼 기어 형태로 교체함으로서, 발생되는 지터문제를 획기적으로 개선할 수 있는 방법으로 고안되었으며, 이 방식은 2015년에 발사된 서브미터급 고해상도 지구관측 위성에 처음으로 적용되어 발사되었으며, 현재까지 성공적으로 운용 중에 있다.

식각장비의 RF 정합모듈 성능 개선 (Matching Improvement of RF Matcher for Plasma Etcher)

  • 설용태;이의용;권혁민
    • 한국산학기술학회논문지
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    • 제9권2호
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    • pp.327-332
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    • 2008
  • 본 논문에서는 반도체 소자와 디스플레이 패널의 제조공정에 사용되는 플라즈마 식각장비의 RF 정합특성을 개선하기 위한 모듈을 제안하였다. 구동부의 기구 중 베벨기어를 웜기어로 새롭게 설계 제작하고 제어부도 원칩 마이크로 프로세서를 이용하여 재구성하였다. 개발된 모듈은 기존의 정합장치보다 다양한 공정변수에 대한 능동적인 대처가 가능하고, 모터의 흐름현상 등을 개선함으로서 RF 정합특성이 개선되어, 플라즈마 식각공정의 생산성을 향상시킬 수 있음을 보였다.

Structural Analysis of a Composite Target-drone

  • Park, Yong-Bin;Nguyen, Khanh-Hung;Kweon, Jin-Hwe;Choi, Jin-Ho;Han, Jong-Su
    • International Journal of Aeronautical and Space Sciences
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    • 제12권1호
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    • pp.84-91
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    • 2011
  • A finite element analysis for the wing and landing gear of a composite target-drone air vehicle was performed. For the wing analysis, two load cases were considered: a 5g symmetric pull-up and a -1.5g symmetric push-over. For the landing gear analysis, a sinking velocity of 1.4 m/s at a 2g level landing condition was taken into account. MSC/NASTRAN and LS-DYNA were utilized for the static and dynamic analyses, respectively. Finite element results were verified by the static test of a prototype wing under a 6g symmetric pull-up condition. The test showed a 17% larger wing tip deflection than the finite element analysis. This difference is believed to come from the material and geometrical imperfections incurred during the manufacturing process.