• 제목/요약/키워드: Torsional Vibration Mode

검색결과 121건 처리시간 0.031초

공기부양선의 추진 및 부양축계 비틀림진동 해석 연구 (A Study on the Analysis of Torsional Vibration of Branched Shafting System for Propulsion and Lift in Air Cushion Vehicle)

  • 손선태;김정렬
    • Journal of Advanced Marine Engineering and Technology
    • /
    • 제31권4호
    • /
    • pp.335-342
    • /
    • 2007
  • A propulsion and lift shafting system in an air cushion vehicle is flexible multi-elements system which consists of two aeroderivative gas turbines with own bevel gears, four stage lift fan reduction gear, two stage propulsion reduction gear air propellers and high capacity of lifting fans. In addition, the system includes the multi-branched shafting with multi-gas turbine engines and thin walled shaft with flexible coupling. Such a branched shafting system has very intricate vibrating characteristics and especially, the thin walled shaft with flexible couplings can lower the torsional natural frequencies of shafting system to the extent that causes a resonance in the range of operating revolution. In this study, to evaluate vibrational characteristics some analytical methods for the propulsion and lift shafting system are studied. The analysis, including natural frequencies and mode shapes, for five operation cases of the system is conducted using ANSYS code with a equivalent mass-elastic model.

Prediction of elastic constants of Timoshenko rectangular beams using the first two bending modes

  • Chen, Hung-Liang (Roger);Leon, Guadalupe
    • Structural Engineering and Mechanics
    • /
    • 제80권6호
    • /
    • pp.657-668
    • /
    • 2021
  • In this study, a relationship between the resonance frequency ratio and Poisson's ratio was proposed that can be used to directly determine the elastic constants. Using this relationship, the frequency ratio between the 1st bending mode and 2nd bending mode for any rectangular Timoshenko beam can be directly estimated and used to determine the elastic constants efficiently. The exact solution of the Timoshenko beam vibration frequency equation under free-free boundary conditions was determined with an accurate shear shape factor. The highest percent difference for the frequency ratio between the theoretical values and the estimated values for all the beam dimensions studied was less than 0.02%. The proposed equations were used to obtain the elastic constants of beams with different material properties and dimensions using the first two measured transverse bending frequencies. Results show that using the equations proposed in this study, the Young's modulus and Poisson's ratio of rectangular Timoshenko beams can be determined more efficiently and accurately than those obtained from industry standards such as ASTM E1876-15 without the need to test the torsional vibration.

현수교(懸垂橋)의 비틀림진동(振動)에 관한 연구(硏究) (A Study of Torsional Vibrations of Suspended Bridges)

  • 민창식;김생빈;손승요
    • 대한토목학회논문집
    • /
    • 제3권3호
    • /
    • pp.27-37
    • /
    • 1983
  • 본(本) 연구(硏究)는 경기도(京畿道) 설계심의회(設計審議會)에서 천마산(天馬山) 청소년(靑少年) 심신수련장(心身修練場) 현수교(懸垂橋) 설계심의시(設計審議時) 현수교(懸垂橋)의 동적(動的) 거동(擧動)에 대한 설계미비(設計未備)의 원인(原因)이 아직도 체계화(體系化)되지 못한 우리 나라 현수교(懸垂橋)의 설계자료(設計資料)와 지침(指針)의 불비(不備)함에 그 동기(動機)를 얻어, 유한요소법(有限要素法)을 적용(適用)하여 현수교(懸垂橋)의 비틀림진동(振動)에 대한 고유진동수(固有振動數)와 이에 상응(相應)하는 고유진동형(固有振動形)을 구(求)하였다. 실제(實際)로 현수교(懸垂橋)의 일반적(一般的) 거동(擧動)은 수직(垂直) 수평면(水平面) 내(內)에서의 연성(連成)된 운동(運動)으로 표시(表示)되지만 사용목적(使用目的)에 부합(附合)하여 그 진폭(振幅)을 미소(微小)하도록 제한(制限)하면 수직(垂直) 비틀림 진동(振動)은 단독(單獨)으로 비연성화(非連成化)할 수 있으며, 이에 따라 해석하였다. 1973년 6월에 개통된 Streamlined Box-Girder Type인 남해대교(南海大橋)와 Lateral Bracing으로 이루어진 단경간의 천마산(天馬山)의 현수교(懸垂橋)의 설계자료(設計資料)를 이용하여 수치해(數値解)를 얻었으며, 천마산(天馬山) 현수교(懸垂橋)의 경우(境遇) 보조(補助) 보강(補强)케이블의 유무(有無)에 따른 고유진동수(固有振動數)와 진동형(振動形)을 구(求)하여 비교(比較) 검토(檢討)하였다. 보강(補强)케이블의 유무(有無)에 따라 초기의 진동수(振動數) 등에서는 그 영향이 매우 뚜렷하였으나, 진동형(振動形)이 복잡해짐에 따라 보강(補强)케이블의 영향은 미약했거나 또는 오히려 역효과를 가져왔다. 남해대교(南海大橋)에 있어서 유한요소기법(有限要素技法)과 전자계산기에 의해 본(本) 연구(硏究)에서 구한 고유진동수(固有振動數)와 남해대교(南海大橋) 건설지(建設誌)에 있는 Frequency Equation으로 구한 값 또는 풍동실험(風洞實驗)에 의한 결과(結果) 등과 비교(比較) 검토(檢討)하였으며, 비교(比較) 결과(結果) 좋은 일치(一致)를 보여주었다.

  • PDF

부품의 국부적 유연성이 차량의 동적 거동에 미치는 영향 (Flexibility Effects of Components on the Dynamic Behavior of Vehicle)

  • 이상범;임홍재
    • 한국공작기계학회논문집
    • /
    • 제12권4호
    • /
    • pp.57-62
    • /
    • 2003
  • A fundamental structural design consideration for a vehicle system is the overall vibration characteristics in bending and torsion. Vibration characteristics of such vehicle system are mainly influenced by the static and dynamic stiffness of the vehicle body structure and also by the material and physical properties of the components attached to the vehicle body structure. In this paper, modeling techniques for the vehicle components are presented and the flexibility and mass effects of the components for the vibration characteristics of the vehicle are investigated. The $1^{st}$ torsional frequency is increased by attaching windshields to the B.I.W. (body-in-white), but the $1^{st}$ bending frequency is decreased by the mass effect. And also, the natural frequencies of the vehicle are large decreased by attaching bumpers, seats, doors, trunk-lid etc. But, suspension system rarely affects the natural frequencies of the vehicle. The study shows thai the dynamic characteristics of the vehicle system can be effectively predicted in the initial design stage.

조합공진 영역에서 감쇠의 영향을 고려한 비선형 진동 응답 특성 (Nonlinear Oscillation Characteristics in Combination Resonance Region Considering Damping Effects)

  • 정태건
    • 한국소음진동공학회논문집
    • /
    • 제20권9호
    • /
    • pp.849-855
    • /
    • 2010
  • Damping may change the response characteristics of nonlinear oscillations due to the parametric excitation of a thin cantilever beam. When the natural frequencies of the first bending and torsional modes are of the same order of magnitude, we can observe the one-to-one combination resonance in the perturbation analysis depending on the characteristic parameters. The nonlinear behavior about the combination resonance reveals a chaotic motion depending on the natural frequencies and damping ratio. We can analyze the chaotic dynamics by using the eigenvalue analysis of the perturbed components. In this paper, we derived the equations for autonomous system and solved them to obtain the characteristic equation. The stability analysis was carried out by examining the eigenvalues. Numerical integration gave the physical behavior of each mode for given parameters.

차체의 탄성진동을 고려한 4기통 엔진 고무마운트의 최적설계 (Optimal Design of the 4-cylinder Engine Rubber Mounts with Elastic Vibrations of Vehicle Body)

  • 박철희;오진우
    • 한국자동차공학회논문집
    • /
    • 제6권1호
    • /
    • pp.163-181
    • /
    • 1998
  • In this study, the objective is determine the optimal design variable of engine mount system using the rubber mount of bush-type which is usually utilized in passive control to minimize vibrations of vehicle body or transmission from engine into body. The engine model adopted in this study is 4-cylinder, 4-stroke gasoline engine support- ed by 4-points. The system is modelled in 10 d.o.f.-rigid body motion of the engine & transmission in 6 d.o.f., elastic motion of vehicle body in 4 d.o.f.(1st torsional, 1st vertical and 1st & 2nd lateral bending vibration mode). To consider the elastic motion of vehicle body, find the eigenvalues and mode shapes of vehicle body by nodal testing and then determine the modal masses and stiffnesses of the body. The design variables of the engine mount system are locations, stiffness and damping coefficients of the rubber mounts(28 design variables). In case of considering the torque-roll axis for the engine, the design variables of the mount system are reduced to 22 design variables. The objective functions in optimal design process are considered by three cases, that is, 1) transmitted forces through engine mounts, 2) acceleration components of generalized coordinates for the vibration of vehicle body, 3) acceleration of specified location(where gear box) of body. three case are analyzed and compared with each other.

  • PDF

Investigating the effect of edge crack on the modal properties of composite wing using dynamic stiffness matrix

  • Torabi, Ali Reza;Shams, Shahrokh;Fatehi-Narab, Mahdi
    • Steel and Composite Structures
    • /
    • 제39권5호
    • /
    • pp.543-564
    • /
    • 2021
  • In this study free vibration analysis of a cracked Goland composite wing is investigated. The wing is modelled as a cantilevered beam based on Euler- Bernoulli equations. Also, composite material is modelled based on lamina fiber-reinforced. Edge crack is modelled by additional boundary conditions and local flexibility matrix in crack location, Castigliano's theorem and energy release rate formulation. Governing differential equations are extracted by Hamilton's principle. Using the separation of variables method, general solution in the normalized form for bending and torsion deflection is achieved then expressions for the cross-sectional rotation, the bending moment, the shear force and the torsional moment for the cantilevered beam are obtained. The cracked beam is modelled by separation of beam into two interconnected intact beams. Free vibration analysis of the beam is performed by applying boundary conditions at the fixed end, the free end, continuity conditions in the crack location of the beam and dynamic stiffness matrix determinant. Also, the effects of various parameters such as length and location of crack and fiber angle on natural frequencies and mode shapes are studied. Modal analysis results illustrate that natural frequencies and mode shapes are affected by depth and location of edge crack and coupling parameter.

포물선형 띠기초의 자유진동 해석 (Free Vibration Analysis of Parabolic Strip Foundations)

  • 이태은;이종국;강희종;이병구
    • 한국소음진동공학회:학술대회논문집
    • /
    • 한국소음진동공학회 2005년도 춘계학술대회논문집
    • /
    • pp.703-706
    • /
    • 2005
  • Since soil structure interactions are one of the most important subjects in the structural/foundation engineering, much study concerning the soil structure interactions had been carried out. One of typical structures related to the soil structure interactions is the strip foundation which is basically defined as the beam or strip rested on or supported by the soils. At the present time, lack of studies on dynamic problems related to the strip foundations is still found in the literature. From these viewpoint this paper aims to theoretically investigate dynamics of the parabolic strip foundations and also to present the practical engineering data for the design purpose. Differential equations governing the free, out o plane vibrations of such strip foundations are derived, in which effects of the rotatory and torsional inertias and also shear deformation are included although the warping of the cross-section is excluded. Governing differential equations subjected to the boundary conditions of free-free end constraints are numerically solved for obtaining the natural frequencies and mode shapes by using the numerical integration technique and the numerical method of nonlinear equation.

  • PDF

원호형 띠기초의 자유진동 해석 (Free Vibration Analysis of Circular Strip Foundations)

  • 이종국;강희종;이병구
    • 한국소음진동공학회:학술대회논문집
    • /
    • 한국소음진동공학회 2004년도 추계학술대회논문집
    • /
    • pp.898-901
    • /
    • 2004
  • Since soil-structure interactions are one of the most important subjects in the structural/foundation engineering, much study concerning the soil-structure interactions had been carried out. One of typical structures related to the soil-structure interactions is the strip foundation which is basically defined as the beam or strip rested on or supported by the soils. At the present time, lack of studies on dynamic problems related to the strip foundations is still found in the literature. From these viewpoint, this paper aims to theoretically investigate dynamics of the circular strip foundations and also to present the practical engineering data for the design purpose. Differential equations governing the free, out-of-plane vibrations of such strip foundations are derived, in which effects of the rotatory and torsional inertias and also shear deformation are included although the warping of the cross-section is excluded. Governing differential equations subjected to the boundary conditions of corresponding end constraints are numerically solved for obtaining the natural frequencies and mode shapes by using the numerical integration technique and the numerical method of non-linear equation.

  • PDF

System identification of the suspension tower of Runyang Bridge based on ambient vibration tests

  • Li, Zhijun;Feng, Dongming;Feng, Maria Q.;Xu, Xiuli
    • Smart Structures and Systems
    • /
    • 제19권5호
    • /
    • pp.523-538
    • /
    • 2017
  • A series of field vibration tests are conducted on the Runyang Suspension Bridge during both the construction and operational stages. The purpose of this study is devoted to the analysis of the dynamic characteristics of the suspension tower. After the tower was erected, an array of accelerometers was deployed to study the evolution of its modal parameters during the construction process. Dynamic tests were first performed under the freestanding tower condition and then under the tower-cable condition after the superstructure was installed. Based on the identified modal parameters, the effect of the pile-soil-structure interaction on dynamic characteristics of the suspension tower is investigated. Moreover, the stiffness of the pile foundation is successfully identified using a probabilistic finite model updating method. Furthermore, challenges of identifying the dynamic properties of the tower from the coupled responses of the tower-cable system are discussed in detail. It's found that compared with the identified results from the freestanding tower, the longitudinal and torsional natural frequencies of the tower in the tower-cable system have changed significantly, while the lateral mode frequencies change slightly. The identified modal results from measurements by the structural health monitoring system further confirmed that the vibrations of the bridge subsystems (i.e., the tower, the suspended deck and the main cable) are strongly coupled with one another.