• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.41 no.12
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• pp.987-993
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• 2013

Korean Utility Helicopter(KUH) is the first korean-developed helicopter. Its first flight was performed in March 2010 and then its development was completed successfully by June 2012. During flight test phase, KUH faced various vibration problems and appropriate vibration-reduction devices were designed and applied to solve the problems. The vibration-reduction devices were applied to main rotor blades, main gear box(MGB) supporting structure, cockpit, cabin and pilot seats to reduce rotor-induced 4/rev vibration. Also, dome-fairing was introduced in order to reduce the tail-shake vibration. This paper shows design technique and flight test results for vibration-reduction devices that have been incorporated into KUH.

• Journal of KSNVE
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• v.4 no.3
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• pp.264-272
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• 1994

동력을 발생하거나 이를 이용하는 대부분의 기계장치는 회전하는 축계 장치 를 갖고 있는데 이들은 중량을 갖는 회전체와 이것을 지지하거나 연결하는 강성축과 베어링으로 구성되므로 진동형태에 따른 고유진동수를 나타낸다. 그 결과 축계 장치 가 운전되는 동안 발생하는 기진력이 축계 강도를 초과하거나 진동수가 시스템의 공진점에 일치하던지 가까우면 이들 진동에 의해 축계 장치에 부착되어 있는 카프링, 감속기어, 지지베어링, 밀봉씰, 공정볼트 등이 이상마모 또는 피로파괴의 원인이 되므로 설계시나 운전중에 이에 대한 진동원인들을 PC를 이용하여 현장운전자들이 쉽게 규명할 수 있도록 개발하고 발생되는 진동문제를 효과적으로 해결할 수 있는 진동 저감장치를 몇 가지 소걔하였다. 국내에서 제작되는 선박, 자동차, 발전프랜트 또는 여기에 설치되는 엔진의 진동저감울 위해 이들 소프트웨어와 하드웨어들은 국내 관련기업의 현장기술 지도를 위해 여러차례 활용된 바 있으며 이를 이용하므로 써 축계진동 저감기술 자립은 물론 국산화 제품의 성능향상에도 크게 기여할 수 있다고 본다.

• Journal of the Korean Society for Railway
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• v.9 no.1 s.32
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• pp.125-130
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• 2006

고속철도 교량구간에 차량(KTS)이 주행할 경우 교량 바닥판에서는 큰 가속도 응답이 계측된다. 이러한 가속도의 원인으로는 큰 단면의 국부 진동, 일정한 간격의 침목의 충격 그리고 차량 자체의 진동 등 여러 가지 원인이 있다. BRDM(Bridge Design manual)에서는 이러한 동적 특성치들에 대한 제한치를 규정하고 있는데, 가속도인 경우는 0.35G이하고 규정하고 있다. 실교량 실험에 의해 계측된 가속도 응답은 규정한 제한치인 0.35G 보다는 작지만, 이러한 가속도 응답치들은 차량이 고속으로 주행할 경우 안전성에 문제를 일으킬 수 있다. 본 논문에서는 큰 단면에서 과도한 국부 진동을 지배하는 가속도 응답을 줄이기 위해서 진동저감 방법을 연구하였다. 비록 휨이나 비틀림 같은 전체 진동모드에는 효과가 작지만 일반적으로 매우 큰 단면을 가진 고속철도 프리스트레스트 상자형 교량의 국부진동인 날개짓 모드를 감소시키는데 진동저감 장치는 효과적이라고 판단된다. 실교량에서 진동저감장치의 실험은 추후 연구를 수행할 예정이다.

• Journal of the Earthquake Engineering Society of Korea
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• v.11 no.3 s.55
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• pp.33-42
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• 2007

In this study, for research on an improvement of the seismic safety of an EDG system, a small scale EDG system was manufactured. For the isolation system, the Coil Spring-Viscous Damper systems were selected. For the shaking table test, 3 kinds of seismic motions were selected which had different frequency contents. In this study, the isolation effects were different and they depended on the input seismic motion. In the case of an NRC earthquake which had low fiequency contents, the isolation effects of the horizontal direction were 20%. But for the seismic motions which had high fiequency contents, the isolation effects were $50{\sim}70%$. In the case of the vertical direction, poor isolation effects were observed. It was because the design properties and the real properties of the isolation system were a little different.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.36 no.3
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• pp.285-290
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• 2008

Pyrotechnic shock or pyroshock is characterized as a transient vibration phenomena which shows large acceleration and high frequency range up to 10kHz during the operation of separation devices where explosives are used. During the flight of a launch vehicle, pyro-shock is mainly generated at several events such as satellite separation, fairing separation and stage separation. In this paper, characteristics of pyroshock are introduced briefly, and PEEK washer shock absorber is applied for the reduction of pyroshock in the high frequency range. With some electronic devices, reduction characteristic of pyroshock using washer type shock absorber are studied. Random vibration tests are also performed for the verification of vibrational characteristics.

• Journal of Space Technology and Applications
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• v.2 no.3
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• pp.187-194
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• 2022

Although the magnitude of the disturbance caused by the driving of the motor operated to secure the high-speed and precise directivity of the antenna is small, it acts as a major cause of impairing the image quality of the observation satellite, which requires precision directing performance. In order to acquire high-resolution image information through the improvement of the high-resolution observation satellite, proper vibration isolation and reduction design are required so that jitter generated when the directional antenna motor is driven is not transmitted to the main mission equipment. In this paper, the development process of the directional antenna vibration reduction device applied to real satellites and the effect of micro vibration reduction before and after application will be examined. This device was designed as a way to significantly improve the jitter problem by replacing only one gear in the directional antenna driving unit with a spring damper gear without any additional interface equipment. It was first applied and launched to a high-resolution earth observation satellite, and has been successfully operated so far.

• Transactions of the Korean Society for Noise and Vibration Engineering
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• v.22 no.9
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• pp.817-824
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• 2012

Transmission of unwanted vibration to sensitive systems can cause various problems including performance degradation and system malfunction. The most common approach to limit the transmission of harmful vibration disturbances to the sensitive system is adapting passive vibration isolator. The classical passive vibration isolator comprising a viscous damper and spring element in parallel, however, exhibits conflicting performance characteristics in that low amplification at the resonance, which is desirable, can only be achieved at the sacrifice of vibration isolation performance in high frequency region, which is undesirable. In this paper, vibration isolation characteristics of various passive isolator schemes in literature to circumvent this conflict are introduced and compared.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2012.04a
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• pp.232-237
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• 2012

Transmission of unwanted vibration to sensitive systems can cause various problems including performance degradation and system malfunction. The most common approach to limit the transmission of harmful vibration disturbances to the sensitive system is adapting passive vibration isolator. The classical passive vibration isolator comprising a viscous damper and spring element in parallel, however, exhibits conflicting performance characteristics in that low amplification at the resonance, which is desirable, can only be achieved at the sacrifice of vibration isolation performance in high frequency region, which is undesirable. In this paper, vibration isolation characteristics of various passive isolator schemes in literature to circumvent this conflict are introduced and compared.

• Bulletin of the Korean Space Science Society
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• 2011.04a
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• pp.32.3-32.3
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• 2011

통신위성은 지향성에 대한 요구조건이 상대적으로 느슨하지만 광학 카메라나 영상 레이다를 이용하여 지구를 관측하는 관측위성의 경우 고품질의 영상을 위해 정밀한 지향성 및 지향 안정성이 요구되나 극심한 열 하중에 의한 열변형 및 임무궤도 상에서 발생하는 미소진동 등은 지향 안정성을 영향을 주며 영상의 품질을 저하시킨다. 특히 자세제어를 위해 쓰이는 반작용휠이나 지상과의 송수신을 위한 안테나들은 그 기능을 수행하기 위해 작동하는 과정에서 미소진동을 발생시키고 이는 카메라나 레이다에 외란으로 작용하기 때문에 이를 최소화할 필요가 있다. 이 논문은 미소진동을 저감시키기 위한 진동저감 장치의 성능과 효율성 분석을 그 목적으로 한다.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2004.05a
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• pp.505-508
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• 2004

단열완충재 제품간의 경량충원 저감성능 평가를 객관적이고 신속하게 판별하기 위하여 실험실용 시험장치를 개발하였다. EVA계열 및 EPPㆍEPS계열의 단열완충재들에 대한 경량충격원 시험에서 제품간의 성능비교가 가능하였으며, 동탄성계수 및 손실계수 측정과 병행함으로써 제품들간의 우열성을 보다 정밀하게 평가할 수 있었다.