• 소음진동
• /
• 제8권1호
• /
• pp.99-111
• /
• 1998

An analytical method using the substructure synthesis and assumed modes method is developed to investigate the effect of flexibility of bladed disk assembly on vibrational modes of flexible rotor system. In modeling the system, Coriolis forces, gyroscopic moments, and centrifugal stiffening effects are taken into account. Then the coupled vibrations between the shaft and bladed disk are extensively investigated using simplistic models, as the shaft rotational speed and the pretwist and stagger angles of blade are varied.

• 대한기계학회논문집A
• /
• 제29권5호
• /
• pp.716-725
• /
• 2005

The method of substructure synthesis o. component mode synthesis(CMS) provides an effective means of dynamic analysis of very large and/or complex structures. In this study, residual dynamic flexibility attachment modes in hybrid component mode synthesis are considered for the purpose of exactly compensating the effect of higher order truncated modes. Following this way, the analysis accuracy of the synthesized structure can be improved effectively with less computational effort. In order to show the accuracy and effectiveness of the proposed hybrid component mode synthesis(HCMS), numerical experiments were carried out for the models of a clamped-clamped beam. The results verified the effectiveness of the proposed method.

• International Journal of Aeronautical and Space Sciences
• /
• 제15권2호
• /
• pp.113-122
• /
• 2014

The objective of the paper is to clarify a methodology based on the use of the existing component mode synthesis methods for the case of two damped substructures which are coupled through a linking viscoelastic flexible substructure and for which the structural modes with free geometrical interface are used for each main substructure. The proposed methodology corresponds to a convenient alternative to the direct use either of the Craig-Bampton method applied to the three substructures (using the fixed geometric interface modes) or of the flexibility residual approaches initiated by MacNeal (using the free geometric interface modes). In opposite to a geometrical interface which is a topological interface on which there is a direct linkage between the degrees of freedom of substructures, we consider a physical flexible interface which exists in certain present technologies and for which the general framework linear viscoelasticity is used and yields a frequency-dependent damping and stiffness matrices of the physical flexible interface.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2003년도 춘계학술대회논문집
• /
• pp.571-577
• /
• 2003

This research proposes a finite element method to determine the natural vibration characteristics of the spinning disk-spindle system in a HDD including the flexibility of supporting structure. Finite element equations of each substructure are derived with the introduction of consistent variables to satisfy the geometric compatibility at the internal boundaries. The natural frequencies and modes from the global asymmetric matrix equations of motion are determined by using the implicit restarted Arnoldi iteration method. The validity of the proposed method is verified by the experimental modal testing. It also shows that the flexibility of base plate plays an important role to determine the natural frequencies of the spinning disk-spindle system in a HDD.

• 대한토목학회논문집
• /
• 제7권2호
• /
• pp.45-57
• /
• 1987

지진하중(地震荷重)에 대한 구조물(構造物)의 동적(動的) 거동(擧動)은 지반(地盤)의 특성(特性)에 따라 현저한 차이(差異)를 나타내게 되는데 이러한 현상(現象)을 동적(動的) 지반(地盤)-구조물(構造物) 상호작용(相互作用)이라고 한다. 지반(地盤)-구조물(構造物) 상호작용(相互作用)의 해석방법(解析方法)은 크게 직접법(直接法)과 부분구조법(部分構造法)으로 구분되며, 이 중 부분구조법(部分構造法)은 직접법(直接法)에 비하여 해석방법(解析方法)은 간편하지만 매입구조물(埋入構造物)이나 층상지반상(層狀地盤上) 구조물(構造物)에 대한 해석 시 많은 제약(制約)을 받게 된다. 본 논문(論文)에서는 원친적으로 반무한탄성체지반상(半無限彈性體地盤上) 구조물(構造物)에만 효과적으로 적용(適用)할 수 있는 부분구조법(部分構造法)을 적절히 응용(應用)하여 매입구조물(埋入構造物) 혹은 층상지반상(層狀地盤上) 구조물(構造物)에도 적용할 수 있는 방법을 제시(提示)하였으며, 직접법(直接法)에 의한 해석프로그램인 FLUSH의 해석결과와 비교(比較) 검토(檢討)하여 그 타당성(妥當性)을 입증(立證)하였다.

• 소음진동
• /
• 제8권3호
• /
• pp.477-484
• /
• 1998

An analytical procedure on the base of the substructure synthesis and assumed modes method is developed to investigate the flexibility effect of bladed disk assembly on vibrational modes of flexible rotor system. In modeling the system, Coriolis forces, gyroscopic moments, and centrifugal stiffening effects are taken into account. The coupled vibrations between the shaft and bladed disk are then extensively investigated through the numerical simulation of simplified models, with varying the shaft rotational speed and the prewist and stagger angles of the blade. It is found that the Coriolis and inertia forces and the inertia torque, which are induced by the one nodal diameter modes of the bladed disk and vary depending upon the stagger and prewist angles, lead to the coupled motions of the shaft and the bladed disk.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 1997년도 추계학술대회논문집; 한국과학기술회관; 6 Nov. 1997
• /
• pp.101-109
• /
• 1997

An analytical procedure on the base of the substructure synthesis and assumed modes method is developed to investigate the flexibility effect of bladed disk assembly on vibrational modes of flexible rotor system. In modeling the system, Coriolis forces, gyroscopic moments, and centrifugal stiffening effects are taken into account. The coupled vibrations between the shaft and bladed disk are then extensively investigated through the numerical simulation of simplified models, with varying the shaft rotational speed and the pretwist and stagger angles of the blade. It is found that the Coriolis and inertia forces and the inertia torque, which are induced by the one nodal diameter modes of the bladed disk and vary depending upon the stagger and pretwist angles, lead to the coupled motions of the shaft and the bladed disk.

• 한국구조물진단유지관리공학회 논문집
• /
• 제15권5호
• /
• pp.124-135
• /
• 2011

연속교의 교대부와 교각부에 설치되는 받침 용량은 통상적으로 각 지점에 작용하는 최대수직반력의 크기에 따라 결정되며 교각부에 더 큰 용량의 받침이 위치한다. 본 연구에서는 지진격리장치가 적용된 세 가지 받침배치에 따른 사교의 지진거동 변화를 비교 분석하여 연속 사교의 지진성능 향상 가능성을 검토하였다. 기존 받침배치(Case A)를 기준으로 교각부에 설치되는 납고무받침(LRB)의 수평강성에 변화를 주어 세 가지 받침배치(Case A, Case B, Case C)를 선정하였다. 납고무받침 자체의 감쇠효과가 고려된 hybrid response spectrum을 이용한 응답스펙트럼 해석을 수행하여 총 36개의 연속 플레이트 거더 사교들의 지진거동을 조사하였다. 해석결과 교대부에 설치된 LRB와 유사한 수평강성 또는 작은 수평강성을 가진 LRB를 교각부에 설치할 때 훨씬 바람직한 사교의 지진거동이 유발되었다. 즉, 교각부에 설치되는 LRB의 수평강성 변화는 사교의 고유진동주기를 길게 하고 모드형상에 변화를 유발시켜 전체밑면전단력과 교각부에서의 최대밑면전단력 그리고 거더에 걸리는 응력을 크게 감소시킨다. 비록 하부구조의 유연성이 증가할수록 받침배치 변경에 따른 지진거동의 긍정적인 효과가 다소 감소되지만, 10m 미만의 교각 높이를 가지면서 지진격리받침(LRB)이 설치된 연속 플레이트 거더 사교의 경우 제안된 받침배치는 지진성능 향상을 가져온다.

• 한국도로학회논문집
• /
• 제13권2호
• /
• pp.9-20
• /
• 2011

국내 대부분을 차지하고 있는 노출형 신축이음장치는 주행 시 소음과 충격을 발생시켜 주행성을 떨어뜨리며, 많은 유지관리비가 소요되고 있다. 이에 미국과 유럽 등에서 적용되었던 매설형 신축이음장치인 Asphalt Plug Joint(APJ) 시스템을 기본으로 하부 구조를 개량한, 새로운 매설형 신축이음장치 Buried Folding Lattice Joint(BFLJ) 시스템이 제안되었다. 본 연구에서는 실험을 통해 매설형 신축이음장치의 상부포장 혼합물에 따른 내구성 및 신축 특성을 비교하였으며, 포장가속시험을 통해 실제 차량 하중에 대한 BFLJ 시스템의 내구성을 평가하였다. 실험결과 개발된 BFLJ 시스템은 기존 APJ 시스템에 비해 신축성능이 우수하며 접합부에서의 응력 집중을 완화시켰다. 또한 차량 하중에 의한 BFLJ 시스템의 표면 처짐이 크게 발생하지 않았으며, 신축이음장치 내의 하부 구조의 손상이 없었던 점에서 기존 APJ 시스템의 문제점을 극복하고 조기파손을 예방할 수 있을 것이라 판단되었다.

• 한국소음진동공학회:학술대회논문집
• /
• 한국소음진동공학회 2007년도 춘계학술대회논문집
• /
• pp.859-865
• /
• 2007

This paper presents a method to analyze the unbalance response of a high speed polygon mirror scanner motor supported by sintered bearing and flexible supporting structures by using the finite element method and the mode superposition method. The appropriate finite element equations for polygon mirror are described by rotating annular sector element using Kirchhoff plate theory and von Karman non-linear strain, and its rigid body motion is also considered. The rotating components except for the polygon mirror are modeled by Timoshenko beam element including the gyroscopic effect. The flexible supporting structures are modeled by using a 4-node tetrahedron element and 4-node shell element with rotational degrees of freedom. Finite element equations of each component of the polygon mirror scanner motor and the flexible supporting structures are consistently derived by satisfying the geometric compatibility in the internal boundary between each component. The rigid link constraints are also imposed at the interface area between sleeve and sintered bearing to describe the physical motion at this interface. A global matrix equation obtained by assembling the finite element equations of each substructure is transformed to a state-space matrix-vector equation, and both damped natural frequencies and modal damping ratios are calculated by solving the associated eigenvalue problem by using the restarted Arnoldi iteration method. Unbalance responses in time and frequency domain are performed by superposing the eigenvalues and eigenvectors from the free vibration analysis. The validity of the proposed method is verified by comparing the simulated unbalance response with the experimental results. This research also shows that the flexibility of supporting structures plays an important role in determining the unbalance response of the polygon mirror scanner motor.