• Title/Summary/Keyword: 공진 회피설계

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The Natural Frequency Sensitivities of the Lower Modes of Ship Hull Vibrations (선체 저차고유진동수의 감도)

  • Y.C. Huh;T.Y. Chung;K.C. Kim
    • Journal of the Society of Naval Architects of Korea
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    • v.28 no.1
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    • pp.99-107
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    • 1991
  • In the course of ship basic design, the redesign works to avoid resonance can be carried out efficiently provided that the frequency sensitivities of the baseline system is available. In this paper, for lower modes of ship's hull vibrations, a practical method to predict the natural frequency sensitivities to major design variables subject to considerations at the preliminary design stage is presented. The method is of derivation based on frequency sensitivities of uniform Timoshenko beams eguivalent to actual ships.

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Dynamic Characteristics of Simply Supported Single Span Bridges for KTX and HEMU using Design Diagram (설계다이어그램을 이용한 KTX와 HEMU 차량 주행시 단경간 단순지지 교량의 동특성 분석)

  • Cho, Jeong-Rae;Cho, Keunhee;Kwark, Jong-Won;Kim, Young Jin
    • Journal of the Korean Society for Railway
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    • v.15 no.5
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    • pp.498-507
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    • 2012
  • This paper presents the ERRI design diagrams of KTX and HEMU applicable to simply supported single span bridges, and analyzes the dynamic characteristics and design considerations of the bridges under KTX and HEMU using the diagrams. The design diagrams of KTX and HEMU are calculated for the bridges with 25m, 30m, 35m and 40m span lengths, which are widely used for simple bridge in Korea. From the design diagrams, the dynamic characteristics of the bridges with the selected span lengths are analyzed. In addition, the design consideration is discussed to satisfy the design requirement of acceleration. It is desirable for the bridge with 25m span length to avoid resonance both for KTX and HEMU. Since larger responses are expected for HEMU in the bridge with 30m span length, and for KTX in the bridge with 35m and 40m span length, the bridges should be planned to have enough mass satifying acceleration requirement at resonance, or to avoid the resonance.

Systematic Design Approach Based on Cavity-Mode Resonance Analysis for Radiated Susceptibility of Cables in Air Vehicles (캐비티 공진 해석 기반 비행체 내부배선 복사내성 대책 설계 방안)

  • Minseong Kang;Yangwon Kim;Donggyu Roh;Myunghoi Kim
    • Journal of Advanced Navigation Technology
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    • v.27 no.5
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    • pp.587-593
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    • 2023
  • In this paper, we propose a systematic design approach based on cavity-mode resonance analysis to improve the radiated susceptibility of cables in air vehicles. As electronic devices equipped in air vehicles substantially increase, enhancing the radiated susceptibility of internal cables becomes more challenging and significant. The proposed design approach provides an efficient method to avoid and suppress cavity-mode resonances using analytical methods to estimate the resonance frequencies and the current ratio induced by the cavity-mode resonances. It is demonstrated in simulated results that the proposed method offers a design solution for improving the radiated susceptibility and reduces the computation time by up to 99.6% compared to the previous design method.

Design Enhancement to Avoid Radar Mast Resonance in Large Ship using Design of Experiments (실험계획법을 이용한 대형 선박용 레이더 마스트의 공진회피 설계)

  • Park, Jun Hyeong;Lee, Daeyong;Yang, Jung-Wook;Song, Chang Yong
    • Journal of Ocean Engineering and Technology
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    • v.33 no.1
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    • pp.50-60
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    • 2019
  • Recently, problems with excessive vibration of the radar masts of large bulk carriers and crude oil tankers have frequently been reported. This paper explores a design method to avoid the resonance of a radar mast installed on a large ship using various design of experiment (DOE) methods. A local vibration test was performed during an actual sea trial to determine the excitation sources of the vibration related to the resonant frequency of the radar mast. DOE methods such as the orthogonal array (OA) and Latin hypercube design (LHD) methods were used to analyze the Pareto effects on the radar mast vibration. In these DOE methods, the main vibration performances such as the natural frequency and weight of the radar mast were set as responses, while the shape and thickness of the main structural members of the radar mast were set as design factors. From the DOE-based Pareto effect results, we selected the significant structural members with the greatest influence on the vibration characteristics of the radar mast. Full factorial design (FFD) was applied to verify the Pareto effect results of the OA and LHD methods. The design of the main structural members of the radar mast to avoid resonance was reviewed, and a normal mode analysis was performed for each design using the finite element method. Based on the results of this normal mode analysis, we selected a design case that could avoid the resonance from the major excitation sources. In addition, a modal test was performed on the determined design to verify the normal mode analysis results.

Design for Resonance Avoidance of Mount Through the Modal Analysis (모드해석을 통한 마운트 공진회피 설계)

  • Lee, Jong-Myeong;Yu, Hyeon-Tak;Park, Gyu-Jin;Choi, Hyeon-Cheol;Choi, Byeong-Keun
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.25 no.7
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    • pp.481-486
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    • 2015
  • This paper provides how to solve the problems analytically and experimentally that occur for testing the water injection pump under development. First of all, water injection pump, based on shaft system dynamic analysis, is verified by measuring the behavior of the shaft system. After the water injection pump is measured, the structural resonances which can cause excessive noise, degradation the equipment life and malfunction are found. Therefore, by changing the structural design, the reso- nance should be avoided. Application of the design variables to the experimentally resonance avoid- ance is difficult. So analytically, with application of the design variables, the design will be changed with mode analysis using FEM.

Evaluation of Structural Safety of Linear Actuator for Flap Control of Aircraft (항공기 플랩 제어를 위한 선형 구동기의 구조 안전성 평가)

  • Kim, Dong-Hyeop;Kim, Sang-Woo
    • Journal of Aerospace System Engineering
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    • v.13 no.4
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    • pp.66-73
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    • 2019
  • The objective of this study was to evaluate the structural safety of the basic design for the linear actuator for the flap control of aircrafts. The kinetic behavior of the linear actuator was determined using the multi-body dynamics (MBD) analysis, and the contact force was calculated to be used as input data for the structural analysis based on the finite element analysis. In the structural analysis, the thermal and static behaviors of the linear actuator satisfying the designed velocity were examined, and the structural safety of the linear actuator evaluated. Moreover, the dynamic behaviors of the key components of the linear actuator were investigated by the modal analysis. The actuation rod linearly moved with about 5 mm/s when the motor operated at 225 rpm and the maximum contact force of 32.83 N occurred between two driving gears. Meanwhile, the structural analysis revealed that the maximum thermal and static stresses were 1.57% and 78% of the yield strength of steel, respectively, and they were in a safe range of the structure. In addition, the linear actuator for the basic design is stable to the resonance by avoiding the natural frequencies of the components.

Study on the Structural Reinforcements for the Transverse Vibration of Ship's Main Engine (선박 주기관 횡진동 구조보강 검토)

  • Im, Hong-Il;Shin, Sang-Hoon
    • Special Issue of the Society of Naval Architects of Korea
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    • 2013.12a
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    • pp.55-59
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    • 2013
  • Transverse vibrations of ship's aft end and deckhouse among the various modes of hull structures are induced mainly by transverse exciting forces and moments of main engine such as ${\times}$ and h-moment. Avoidance of resonance should be made in a intial design stage in case there is a prediction for resonance between main engine and transverse modes of deckhouse. This study shows a case of change in type of main engine from 12 cylinders to 10 without modification of hull structures in engine room requested by a shipowner of 8,600 TEU class container carrier and proposes a guide to the effective ways of structural arrangement for avoiding resonance between transverse exciting force and surrounding structures of main engine in engine room through case studies.

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A study on the design optimization of baseframe to avoid resonance of diesel generator set (발전기세트 공진 회피를 위한 베이스프레임 최적설계에 관한 연구)

  • Jeong, S.H.;Kwak, Y.S.;Kim, W.H.
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2012.04a
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    • pp.157-162
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    • 2012
  • A structural modification of baseframe is an effective method to avoid resonance in marine diesel generator (D/G) set which consists of diesel engine, generator and baseframe. However the reinforcement with thick plates or additional parts to increase the natural frequency can be less effective because of increased weight. Especially fine control of target mode based on the experience is difficult because the weight and interference of system have to be considered. In this paper, the design optimization of baseframe was performed to reduce the resonant vibration using a gradient descent method. The design parameters such as thickness, shape and location of baseframe parts are optimized to increase the torsional natural frequency of D/G set. From the actual test, the new designed baseframe reduced the vibration level in resonance by 55% without any increase of weight and interference. interference.

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Ground Vibration Test for Korean Utility Helicopter (한국형 기동헬기 전기체 지상진동시험)

  • Kim, Se-Hee;Kwak, Dong-Il;Jung, Se-Un;Choi, Jong-Ho;Kim, Joung-Hun
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.41 no.6
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    • pp.495-501
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    • 2013
  • Korean Utility Helicopter (KUH) has been designed to avoid the blade passing frequency and any instability due to a coupling of dynamic characteristics between the main rotor and the airframe in ground operation. For these design objectives, the vibration analysis and the ground resonance analysis were performed to analyze the dynamic characteristics of the airframe and the main rotor. Then, the whirl-tower test was conducted to identify the dynamic characteristics of the main rotor and the ground vibration test (GVT) was conducted to identify the dynamic characteristics of the airframe. The GVT for KUH was conducted with the test conditions and test articles established in consideration of each flight and ground condition. This paper shows the method and technique for performing the GVT for KUH and presents the correlation technique and the results for the correlated analysis model.

A Study on the Design Process of Steering System considering Frequency and Sensitivity (주파수와 감도를 고려한 스티어링 시스템 설계 프로세스 연구)

  • Kim, Ki-Chang;Kim, Chan-Mook
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2005.11b
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    • pp.208-211
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    • 2005
  • This paper describes the development process of steering system for reduce idle vibration through the data level of frequency and sensitivity. High stiffness and light weight vehicle is a major target in the refinement of passenger cars to meet customers' contradictable requirements between NVH performance and fuel economy. The target frequency of the steering system is set by benchmarking of a competitive vehicle and the vibration mode map is used to separate steering column modes from resonance of body structure and engine idle rpm. This paper descirbes the analysis approach process for high stiffness of steering system and the design guideline is suggested about steering column and support system by using mother car at initial design stage. We used a patent map in order to analyze accurately a technical trend and suggested the design process using dynamic damper of steering system considering sensitivity. And we established techniques of analysis on steering system and evaluated the level of accuracy of analysis through correlating the test and analysis results. It makes possible to design the good NVH performance vehicle at initial design stage and save vehicles to be used in tests. These improvements can lead to shortening the time needed to develop better vehicles.

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