• 항공우주시스템공학회지
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• 제4권4호
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• pp.44-48
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• 2010

This paper is used the commercial magneto-rheological(MR) damper for landing gear. The damping characteristics of Commercial MR damper by changing the intensity of the magnetic field are investigated and the dynamic responses of the landing gear. it is set up tset equipment, the landing gear drop test system. The landing gear involved drop testing the gear. The landing gear is tested by implementing sky-hook control algorithm and its performance is evaluated comparing to the result.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2003년도 춘계학술대회논문집
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• pp.1048-1053
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• 2003

This paper proposed a MR(Magneto-rheological) seat damper for a commercial vehicle. After formulating the governing equation of motion, an appropriate size of damper is designed and manufactured. Following the equation of fie d-dependent damping force characteristics, a semi-active seat suspension installed with the proposed MR-damper is constructed and its dynamic model id established, Subsequently, vibration isolation performance of the semi-active suspension system is demonstrated by incorporating with a MRAC(Model referenced adaptive control) fer the MR Seat Damper

• 한국항공우주학회지
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• 제36권4호
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• pp.346-351
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• 2008

본 논문에서는 MR 댐퍼를 헬기 착륙장치 완충기에 적용하여 반능동형 헬기 착륙장치 시스템을 설계하고, 헬기 착륙장치의 반능동제어를 수행하였다. MR 유체는 자기장 내에서는 유체의 물성치가 바뀌게 되는 빙햄거동을 시뮬레이션 하여 MR 댐퍼의 성능을 평가하였다. MR 댐퍼 내에서 자기장을 설계하고, 자기장의 변화에 대해 내부감쇠력의 변화를 고찰하고 자기장에 따른 착륙장치의 거동을 평가하였다. 또한 반능동형 헬기 착륙장치에 제어 알고리즘을 적용하여 착륙특성 성능을 해석하였고, 수동계의 착륙특성과 반능동형의 착륙특성을 비교하였다.

• 한국소음진동공학회논문집
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• 제23권5호
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• pp.463-471
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• 2013

This paper presents design and control of electronic control suspension(ECS) equipped with controllable magnetorheological(MR) damper for passenger vehicle. In order to achieve this goal, a cylindrical type MR fluid damper that satisfies design specification of a middle-sized commercial passenger vehicle is proposed. After manufacturing the MR damper with design parameters, their field-dependent damping forces are experimentally evaluated and compared with those of a conventional damper. A quarter-vehicle MR ECS system consisting of sprung mass, spring, tire, controller and the MR damper is established in order to investigate the ride comfort performances. On the basis of the governing equation of motion of the suspension system, five control strategies(soft, hard, comfort, sport and optimal mode) are formulated. The proposed control strategies are then experimentally realized with the quarter-vehicle MR ECS system. Control performances such as vertical acceleration of the car body and tire deflection are evaluated in frequency domains on random road condition. In addition, performance comparison of WRMS(weighted root mean square) of the quarter-vehicle MR ECS system on random road are undertaken in order to investigate ride comfort characteristics.

• 한국소음진동공학회논문집
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• 제20권3호
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• pp.249-256
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• 2010

This paper presents performance analysis of a quarter-vehicle magneto-rheological(MR) suspension system with respect to different tire pressure. As a first step, MR damper is designed and manufactured based on the optimized damping force levels and mechanical dimensions required for a commercial mid-sized passenger vehicle. After experimentally evaluating dynamic characteristics of the manufactured MR damper, the quarter-vehicle MR suspension system consisting of sprung mass, spring, tire and the MR damper is constructed in order to investigate the ride comfort. After deriving the equations of the motion for the proposed quarter-vehicle MR suspension system, vertical tire stiffness with respect to different tire pressure is experimentally identified. The skyhook controller is then implemented for the realization of quarter-vehicle MR suspension system. Ride comfort characteristics such as vertical acceleration RMS and weighted RMS of sprung mass are evaluated under various road conditions.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2009년도 추계학술대회 논문집
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• pp.834-835
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• 2009

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2011년도 추계학술대회 논문집
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• pp.343-348
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• 2011

This paper presents ride comfort characteristics of a quarter-vehicle magneto-rheological (MR) suspension system with respect to different tire pressure. As a first step, controllable MR damper is designed and modeled based on both the optimized damping force levels and mechanical dimensions required for a commercial full-size passenger vehicle. Then, a quarter-vehicle suspension system consisting of sprung mass, spring, tire and the MR damper is constructed. After deriving the equations of the motion for the proposed quarter-vehicle MR suspension system, vertical tire stiffness with respect to different tire pressure is experimentally identified. The skyhook controller is then implemented for the realization of the quarter-vehicle MR suspension system. Finally, the ride comfort analysis with respect to different tire pressure is undertaken in time domain. In addition, a comparative result between controlled and uncontrolled is provided by presenting vertical RMS displacement.

• 한국항공우주학회지
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• 제37권4호
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• pp.344-349
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• 2009

본 논문은 헬기용 주륜 착륙장치의 성능을 향상시킬 목적으로 반능동형 착륙장치를 도입하였다. 상용 유한요소 코드를 이용하여 자기장해석을 한 MR 댐퍼를 완충기에 적용 하였다. 착륙 거동 시 내력으로 발생되는 공기력과 감쇠력의 합을 일정하게 유지시키는 개념의 하중제어기법을 적용하여 반능동형 착륙장치의 제어기를 구성하였다. 다른 형태의 수동형 및 스카이 훅 제어 반 능동형 착륙장치와 함께 ADAMS를 이용한 낙하 시뮬레이션을 수행하였고 착륙특성에 대한 성능평가를 위해 그 결과들을 비교하였다.

• 한국소음진동공학회논문집
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• 제21권12호
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• pp.1159-1165
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• 2011

This paper presents ride comfort characteristics of a quarter-vehicle magneto-rheological(MR) suspension system with respect to different tire pressure. As a first step, controllable MR damper is designed and modeled based on both the optimized damping force levels and mechanical dimensions required for a commercial full-size passenger vehicle. Then, a quarter-vehicle suspension system consisting of sprung mass, spring, tire and the MR damper is constructed. After deriving the equations of the motion for the proposed quarter-vehicle MR suspension system, vertical tire stiffness with respect to different tire pressure is experimentally identified. The skyhook controller is then implemented for the realization of the quarter-vehicle MR suspension system. Finally, the ride comfort analysis with respect to different tire pressure is undertaken in time domain. In addition, a comparative result between controlled and uncontrolled is provided by presenting vertical RMS displacement.

• 항공우주시스템공학회지
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• 제14권5호
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• pp.33-41
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• 2020

항공기의 착륙장치는 지상에서 동체로 전달되는 충격에너지를 흡수 및 소산시키는 장치이다. 착륙장치 중 반능동형 MR 댐퍼 착륙장치는 다양한 착륙조건에서 높은 충격흡수효율을 보여주며 제어 불능 시 안정성을 확보할 수 있는 장점이 있다. 오리피스가 아닌 환형 관유로를 이용하는 MR 댐퍼 착륙장치의 경우, 유로 압력강하로 인해 발생하는 감쇠력이 MR 댐퍼 내부 형상 구조에 따라 저압 챔버에서 캐비테이션을 유발할 수 있어 기존의 2 자유도계 모델링 기법보다 다중물리시스템 해석 프로그램인 Amesim이 더 유용하다. Amesim을 이용한 해석결과를 바탕으로 착륙장치 내부 유로 형상 배치를 수정하여 캐비테이션을 방지할 수 있는 유로 구조를 제안하였고 낙하 시험 시뮬레이션 결과를 통해 이를 검증하였다. 본 논문에서는 환형 관로 형태 유로 구조를 갖는 MR 댐퍼형 착륙장치의 캐비테이션 발생시 주요 특성을 파악하였고, 아울러 내부형상 배치 수정을 통해 이를 방지하는 방안을 제시하였다.