• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2000년도 춘계학술대회논문집
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• pp.280-285
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• 2000

With recent development of technology of high stiffness material and the structural design, the construction of high rise structures such as tall building, tower has increased. The more flexible and slender structure is vulnerable to the internal and external dynamic loads induced by earthquake, wind and traffic load. There have been great effort and many researches to minimize the influence of dynamic loads on the structure. The traditional and stable method, the application of the passive damper, is not able to comply with various dynamic loads, while the mass damper which active control technology is integrated can effectively comply with load types. Therefore, the application of active control of huge structures with AMD(Active mass damper) or HMD(Hybrid Mass damper) is increasing. Up to now, most of actuators are servomotor and hydraulic actuator. But it is known that the electromagnetic actuator applies non contacting control force, which makes the control system easier with no characteristic change depending on time. In this paper, Hybrid mass damper with electromagnetic actuator was designed and applied to building scaled structure. The performance of designed HMD tested by shake table test is included.

• Earthquakes and Structures
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• 제1권4호
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• pp.411-425
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• 2010

The effect of dead loads on dynamic responses of uniform elastic beams is examined by means of a governing equation which takes into account initial bending stress due to dead loads. First, the governing equation of beams which includes the effect of dead loads is briefly presented from the author's paper (Takabatake 1990). In the formulation the effect of dead loads is considered by strain energy produced by conservative initial stresses produced by the dead loads. Second, the effect of dead loads on dynamical responses produced by live loads in simply supported beams and clamped beams is confirmed by the results of numerical computations with the Galerkin method and Wilson-${\theta}$ method. It is shown that the dynamical responses, like dynamic deflections and bending moments produced by dynamic live loads, are decreased in a heavyweight beam when the effect of dead loads is included. Third, an approximate solution for dynamic deflections including the effect of dead loads is presented in closed-form. The proposed solution shows good in agreement with results of numerical computations with the Galerkin method and Wilson-${\theta}$ method. Finally, a method reflecting the effect of dead loads for dynamic responses of beams on the magnitude of live loads is presented by an example.

• 한국가스학회지
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• 제12권1호
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• pp.13-18
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• 2008

지진 및 외부 진동에 의하여 구조물에 발생하게 되는 진동량은 진동 속도와 피해규모가 비례하는 관계에 있음을 고려하여 일반적으로 진동속도로 나타내어진다. 본 연구에서는 진동 속도 기반의 구조물 진동기준을 검토하고, 이를 고려하여 도로 하부 매설 가스 강관의 안정성 평가를 수행하였다. 가스공사 주사용 배관인 762 mm API 5L Gr. X65 강관을 해석 대상 배관으로 선정하였으며 도로설계기준에 의하여 지반 매설 조건 및 DB-24 하중을 다양한 속도에 대한 시간 함수로 고려하여 재하하였다. 진동속도는 차량 진행 속도 80 km/h까지 증가하다가 이후 감소하는 경향을 보였으며, 차량 진행 속도 80 km/h에서 0.034 cm/s의 진동 속도를 보임으로서 진동 기준 대비 매우 작은 값임을 확인하였다. 또한 감쇄법칙을 적용하여 진행파의 속도를 분석한 결과, 차량 진행 속도 80 km/h에서 가장 작은 속도를 나타내었다.

• 한국항공우주학회지
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• 제41권6호
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• pp.440-447
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• 2013

본 연구에서는 능동적인 블레이드 제어기법인 고조파제어(Higher Harmonic Control, HHC) 기법을 적용하여 로터의 허브 진동하중을 억제하기 위한 최적 제어입력을 탐색하였다. 통합 공탄성 해석 프로그램인 CAMRAD II를 이용하여 HART II 로터를 모델링하고 다양한 HHC 입력 조건에 대하여 파라미터 연구를 수행하여 최대의 진동하중을 감소시키기 위한 제어입력을 찾고, HART II 시험에서 정한 최소 진동 조건에서의 허브 진동하중과 비교하였다. 파라미터 연구를 통하여 HART II 시험에서의 최소 진동 조건에서는 진동하중이 증가하는 것을 확인하였다. 허브 진동하중을 감소시키기 위한 최적의 제어입력은 3/rev의 가진주파수에서 찾을 수 있었고 0.8도의 진폭과 350도의 위상각을 갖는 제어입력을 이용하는 경우에 기준조건대비 약 45%의 허브 진동하중 감소효과를 얻었다. HHC 기법을 이용하는 경우의 로터의 파워 감소는 5% 미만으로 나타나고, 성능이 향상되는 경우에는 대부분 진동이 증가하는 경향을 보였다.

• 한국가스학회지
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• 제15권1호
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• pp.22-29
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• 2011

도심지 내 공사 현장 및 주변 지반에 매설된 지중 배관은 시공하중에 의한 진동에 노출이 되어있는 실정이다. 주기적으로 진동이 발생하는 매설된 배관의 지중 동적 거동 특성을 분석하기 위하여 기존 문헌 분석과 실증 실험의 결과를 토대로 수치해석을 수행하고 그 사용성을 검증하였다. 본 논문은 건설 장비중 하나인 덤프 트럭 하중의 매설 심도에 따른 배관의 거동을 분석하여 향후 지중 배관 관리기준 수립을 위한 기초 연구로서 수행되었다. 매설 심도 0.6, 1.2, 1.8m 차량 이동 속도 10km/h에 대하여 해석을 실시하였으며, 그 결과 매설 심도가 깊어질수록 진동속도 및 발생 응력이 작아지는 것을 확인할 수 있다.

• 산업기술연구
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• 제17권
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• pp.199-204
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• 1997

In this paper, the result of application of vibration method to the orthotropic plates with free edges supported on elastic foundation and with a pair of opposite edges under axial forces is presented. Such plates represent the concrete highway slab and hybrid composite pavement of bridges. The reinforced concrete slab can be assumed as a special orthotropic plate, as a close approximation. The highway slab is supported on elastic foundation, with free boundaries. Sometimes, the pair of edges perpendicular to the traffic direction may be subject to the axial forces. The plate is subject to the concentrated load/loads, in the form of traffic loads, or the test equipments. Finite difference method is used to obtain the deflection influence surfaces needed for vibration analysis. The influence of the modulus of the foundation, the aspect ratio of the plate, and the magnitudes of the axial forces and the concentrated attached mass on the plate, under the natural frequency is thoroughly studied.

• Architectural research
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• 제15권1호
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• pp.35-42
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• 2013

A study on the free vibration and linear buckling analyses of thick plates is described in this article. In order to determine the natural frequencies and buckling loads of plates, a plate element is developed by using isogeometric approach. The Non-uniform B-spline surface (NURBS) is used to represent both plate geometry and the unknown displacement field of plate. All terms required in isogeometric formulation are consistently derived by NURBS definition. The capability of the present plate element is demonstrated by using several numerical examples. From numerical results, it is found to be that the present isogeometric element can predict accurate natural frequencies and buckling loads of plates.

• 한국기계가공학회지
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• 제11권5호
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• pp.68-75
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• 2012

This study aims at the structural analysis of vibration and fatigue according to the tie rod configuration. The maximum displacement amplitude is happened at 156Hz by harmonic vibration analysis, this tie rod model can be broken as the weakest state. Among the cases of nonuniform fatigue loads, 'SAE bracket history' with the severest change of load becomes most unstable but 'Sine wave' becomes most stable. In case of 'Sine wave' with the average stress of 0MPa and the amplitude stress of 570MPa, the possibility of maximum damage becomes 70%. This stress state can be shown with 140 times more than the damage possibility of 'SAE bracket history' or 'SAE transmission'. The structural result of this study can be effectively utilized with the design on tie rod by investigating prevention and durability against its damage.

• 한국기계가공학회지
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• 제10권5호
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• pp.65-71
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• 2011

This study analyzes about front axle through the analyses of stress, fatigue and vibration. Maximum equivalent stress is shown with the frequency of 60Hz in case of the harmonic vibration analysis applied with force. Among the cases of nonuniform fatigue loads, 'SAE bracket history' with the severest change of load becomes most unstable but 'Sample history' becomes most stable. In case of 'Sample history' with the average stress of 0 to $-2{\times}10^5MPa$ and the amplitude stress of 0 to $-2{\times}10^5MPa$, the possibility of maximum damage becomes 3%. This stress state can be shown with 6 times more than the damage possibility of 'SAE Bracket history' or 'SAE transmission'. The structural result of this study can be effectively utilized with the design of front axle by investigating prevention and durability against its damage.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2000년도 춘계학술대회논문집
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• pp.1252-1258
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• 2000

Koreasat-3 was successfully launched by an Ariane IV launch vehicle on September 5, 1999. Although the primary purpose of the satellite is to replace Koreasat-l, it also can extend its communication service coverage over the Asia-Pacific region. A spacecraft is subjected to severe dynamic loads during launch period. To verify the safety of spacecraft under the launch environment, dynamic tests should be performed such as sine sweep, acoustic and separation shock tests. This paper presents the launch environment test results of Koreasat-3. A total of 188 acceleration responses was measured and compared with the design requirements of components and spacecraft. Dynamic characteristic change was also investigated by comparing between low-level pre/post vibration results. From the review of test results, it is concluded that Koreasat-3 was designed and manufactured with the margin of safety enough to survive the launch loads of Ariane IV.