• 제목/요약/키워드: Equivalent Mass Moment of Inertia

검색결과 7건 처리시간 0.021초

배골형단면(背骨型斷面) 주상체(柱狀體)의 자유수면(自由水面)하에서의 비틂진동(振動)에 대(對)한 이차원적(二次元的) 부가관성(附加慣性)모우먼트의 계산(計算) (A Note on the Two-Dimensional Added Mass Moment of Inertia in Torsional Vibration of Cylinders of Curvilinear-Element Sections with Chines.)

  • 이기표;양영순
    • 대한조선학회지
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    • 제11권2호
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    • pp.41-44
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    • 1974
  • A calculation of the two dimensional added mass moment of inertia for the Kim's chine form sections is made with a special consideration of a location of a axis of rotation. The results are compared with those of Lewis form section equivalent to the above chine form sections calculated by Kumai.

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자율비행 개인항공기용 주익 조립체 등가모델 동특성 해석 (Equivalent Model Dynamic Analysis of Main Wing Assembly for Optionally Piloted Personal Air Vehicle)

  • 김현기;김성준
    • 항공우주시스템공학회지
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    • 제15권1호
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    • pp.72-79
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    • 2021
  • 본 연구에서는 신개념 항공교통수단으로 활용될 자율비행 개인항공기 개발의 일환으로 자율비행 개인항공기 주익조립체의 등가모델을 생성한 후 고유모드 해석을 통해 생성된 등가모델의 신뢰성을 검증하였다. 주익조립체는 주익, 안쪽파드, 바깥쪽 파드로 구성되어 있다. 먼저, 각 부품의 등가모델을 생성하기 위해서 해당 부품을 몇 개의 구역으로 분할하고, 각 구역의 양 끝단에 등가모델 축상에 놓이는 절점들을 생성하였다. 그리고, 단위하중과 단위모멘트을 부과한 정적해석을 통해 변형량 또는 회전량을 계산하고, 빔 이론식을 적용하여 각 부품들의 등가 축강성, 굽힘강성, 비틀림강성을 계산하였다. 그리고, 각 구역 중앙에 집중질량을 생성하여 질량과 관성모멘트 정보를 입력하고, 빔 요소를 사용하여 등가모델을 생성하였다. 최종적으로 상세모델의 모드해석 결과와의 비교를 통해 생성된 등가모델의 신뢰성을 확인하였다.

자동차용 워터펌프의 스퀼소음 저감을 위한 영향도분석 (Parametric Study for the Squeal Noise Reduction of an Automobile Water Pump)

  • 김보형;정원영;백홍길;강동진;정진태
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2013년도 춘계학술대회 논문집
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    • pp.492-497
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    • 2013
  • In this study, a parametric study is performed to investigate the squeal noise of an automobile water pump. The squeal noise studied in this paper is generated by the self-excited torsional resonance of the rotating shaft, and this noise is related to the stick-slip phenomenon of the mechanical seal in the water pump. The mechanical seal friction has the characteristics of the negative velocity-gradient. The equations of motion of multiple-degree-of-freedom torsional vibration model is constructed by the Holzer's method and then the equation is transformed to an equivalent single-degree-of-freedom torsional resonance simulation model. A squeal noise criteria is determined by the simulation model to perform the parametric study. The design parameters(the mass moment of inertia of the pulley, the mass moment of inertia of the impeller, the length of the shafts, the radius of the shafts, spinning speed of the shafts, the position of the mechanical seal, radius of the mechanical seal, and normal load of the mechanical seal) are investigated to confirm the stability for the squeal noise.

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자동차용 워터펌프의 스퀼소음 저감을 위한 영향도 분석 (Parametric Study for the Squeal Noise Reduction of an Automobile Water Pump)

  • 김보형;정원영;백홍길;강동진;정진태
    • 한국소음진동공학회논문집
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    • 제23권7호
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    • pp.624-630
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    • 2013
  • In this study, a parametric study is performed to investigate the squeal noise of an automobile water pump. The squeal noise studied in this paper is generated by the self-excited torsional resonance of the rotating shaft, and this noise is related to the stick-slip phenomenon of the mechanical seal in the water pump. The mechanical seal friction has the characteristics of the negative velocity-gradient. The equations of motion of multiple-degree-of-freedom torsional vibration model is constructed by the Holzer's method and then the equation is transformed to an equivalent single-degree-of-freedom torsional resonance simulation model. A squeal noise criteria is determined by the simulation model to perform the parametric study. The design parameters(the mass moment of inertia of the pulley, the mass moment of inertia of the impeller, the length of the shafts, the radius of the shafts, spinning speed of the shafts, the position of the mechanical seal, radius of the mechanical seal, and normal load of the mechanical seal) are investigated to confirm the stability for the squeal noise.

플라이휠의 새로운 설계 해석 (A New Design Analysis of Flywheel)

  • 김재호;신영재
    • 대한기계학회논문집
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    • 제15권3호
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    • pp.1063-1066
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    • 1991
  • 본 연구에서는 기계 기구의 각속도 변동을 줄이는데 사용되는 플라이휠을 운동에너지의 법칙을 이용하여 해석하고, 주어진 허용 각속도 변동률을 정확히 만족하 는 플라이휠의 크기를 결정하는 새로운 방법을 제시하였다. 또한 수치 해석을 통하 여 본 해석방법에 의해 설계된 플라이휠과 종래 방법에 의한 플라이휠의 성능을 비교 하였다.

헬리컬 기어계의 동적 전달오차의 예측 (The Prediction of the Dynamic Transmission Error for the Helical Gear System)

  • 박찬일;조도현
    • 대한기계학회논문집A
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    • 제28권9호
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    • pp.1359-1367
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    • 2004
  • The purpose of this study is to predict the dynamic transmission error of the helical gear system. To do so, the equations of motion in the helical gear system which consists of motor, coupling, gear, torque sensor, and brake are derived. As the input parameters, the mass moment of inertia by a 3D CAD software and the equivalent stiffness of the bearings and shaft are calculated and the coupling stiffness is measured. The static transmission error as an excitation is calculated by in-house program. Dynamic transmission error is predicted by solving the equations of motion. Mode shape, the dynamic mesh force and the bearing force are also calculated. In this analysis, the relationship between the dynamic mesh force and the bearing force and mode shape behavior in gear mesh are checked. As a result, the magnitude of mesh force is highly related with the gear mesh behavior in mode shape. The finite element analysis is conducted to find out the natural frequency of gear system. The natural frequencies by finite element analysis have a good agreement with the results by equation of motion. Finally, dynamic transmission error is measured by the specially designed experiment and the results by equation of motion are validated.

OTM 단말기 안테나 시선 안정화 제어 (Stabilization Control of line of sight of OTM(On-The-Move) Antenna)

  • 강민식;조용완
    • 전기학회논문지
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    • 제59권11호
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    • pp.2073-2082
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    • 2010
  • The 4-th generation of mobile communication aims to realize global, fast and mobile communication service. The satellite communication charges a key role in this field. In this study, an OTM(On-The-Move) antenna which is mounted on ground vehicles and is used for mobile communication between vehicle and satellite was addressed. Since vehicles move during communication, active antenna line-of-sight stabilization is a core technology to guarantee high satellite communication quality. Stabilization of a satellite tracking antenna which consists of 2-DOF gimbals, an elevation gimbal over an azimuth gimbal, was considered in this study. Various disturbance torques such as static and dynamic mass imbalance torques, variation of moment of inertia according to elevation angle, friction torque related to vehicle motion, equivalent disturbance torque due to antenna roll motion, etc. were analyzed. As a robust stabilization control, rate feedback with sliding mode control and position feedback with proportional+integral control was suggested. To compensate antenna roll motion, a supplementary roll rate feed forward control was included beside of the feedback control loop. The feasibility of the analysis and the proposed control design were verified along with some simulation results.