• 제목/요약/키워드: Multibody dynamics simulation

검색결과 123건 처리시간 0.014초

Analysis of Dynamic Interaction Between Maglev Vehicle and Guideway (자기부상열차/가이드웨이 동적상호작용 해석)

  • Kim, Ki-Jung;Han, Hyung-Suk;Yang, Seok-Jo
    • Transactions of the Korean Society of Mechanical Engineers A
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    • 제37권12호
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    • pp.1559-1565
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    • 2013
  • This study aims to investigate the dynamic interaction characteristics between Maglev vehicles and an elevated guideway. A more detailed model for the dynamic interaction of the vehicle/guideway is proposed. The proposed model incorporates a 3D full vehicle model based on prototyping, flexible guideway by a modal superposition method, and levitation electromagnets including the feedback controller into an integrated model. The proposed model was applied to an urban transit Maglev developed for a commercial application to analyze the dynamic response of the vehicle and guideway, and the effect of the surface roughness of the rail, mid-span guideway deflections, and air gap variations are then investigated from the numerical simulation.

Helicopter Active Airframe Vibration Control Simulations Using an Exhaustive Test Method (Exhaustive 시험 기법을 이용한 헬리콥터 능동 기체 진동 제어 시뮬레이션)

  • Park, Byeong-Hyeon;Lee, Ye-Lin;Park, Jae-Sang
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • 제50권11호
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    • pp.791-800
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    • 2022
  • The number and locations of force generators and their force directions of Active Vibration Control System(AVCS) are important to maximize the airframe vibration reduction performance of helicopters. The present AVCS simulation using an exhaustive test method attempts to determine the best number and locations of force generators and their force directions for maximization of the airframe vibration reduction performance of UH-60A helicopter at 158 knots. The 4P hub vibratory loads of the UH-60A helicopter are calculated using DYMORE II, a nonlinear multibody dynamics analysis code, and MSC.NASTRAN is used to predict the vibration responses of the UH-60A airframe. The AVCS framework with an exhaustive test method is constructed using MATLAB Simulink. As a result, when applying AVCS with the optimal combination of the force generators, the 4P airframe vibration responses of UH-60A helicopter are reduced by from 19.35% to 98.07% compared to the baseline results without AVCS.

Optimization of a Cam Profile in a Circuit Breaker to Improve Latching Performance (캠 윤곽 최적설계를 통한 차단기 래칭 성능 향상)

  • Lee, Jae Ju;Jang, Jin Seok;Park, Hyun Gyu;Yoo, Wan Suk;Kim, Hyun Woo;Bae, Byung Tae
    • Transactions of the Korean Society of Mechanical Engineers A
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    • 제40권1호
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    • pp.73-79
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    • 2016
  • Higher circuit breaker safety standards can be obtained by increasing the sustaining time of the latching section. This time increase is achieved through velocity reduction after contacting when the closing mechanism operates. The potential for the re-closing phenomenon to occur is also reduced by obtaining time to return open latch. In this study, the sustaining time for the latching section was increased through cam profile optimization based on the displacement response of the moving parts. In addition, the existing performance velocity was also satisfied. A multibody dynamics model of the circuit breaker was developed using ADAMS. To validate the model, simulation results were compared to experiment results. Then, cam profile optimization was carried out using an optimal design program PIAnO. Design variables selected included the radial direction of the cam. Design sensitivity analysis was carried out by design section as well. As a result of optimization, the sustaining time for the latching section was increased.