• 한국항공우주학회지
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• 제47권9호
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• pp.607-616
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• 2019

항공우주비행체 정적구조시험을 위한 과하중 방지를 위해 사용되는 하중제한밸브(LLV)의 파일럿 스테이지의 주요 구성품들에 대한 자유물체도 분석을 수행하였다. 이 분석을 통하여 유압작동기의 동일한 힘에서 일관성있게 포펫 개방되도록 하기 위해서는 파일럿스테이지에 있는 두 포펫의 직경비($(D_2)^{ten}/D_2)^{comp}$)가 작동기의 피스톤 면적비($A_{comp}/A_{ten}$)와 동일해야만 한다는 것을 보였다. 실험실에서 외산으로 수입하여 사용하고 있는 4개의 서로 다른 하중제한밸브의 포펫들 형상을 측정하고 대응되는 4개의 다른 용량을 갖는 유압작동기들의 피스톤 면적비들로부터 위의 분석결과가 타당함을 확인하였다. 두 개의 다른 파일럿스테이지로 수행한 "조절자 분해능시험들"의 결과들로부터 조절자 각 회전에서 얻은 Fi(포펫개방 순간의 작동기 힘)의 최대 표준편차는 각 평균값으로부터 0.3KN이고 표준편차를 각 평균값으로 나눈 무차원값으로 분석하면 최대편차는 3.7%이다. 이 결과로 부터 동일 포펫 직경비를 갖는 두 개의 파일럿스테이지들의 포펫은 각 조절자 회전에 대해 Fi/(평균 Fi) 값이 +/- 3.7% 범위에서 일관성 있게 개방되고 있음을 확인하였다. 위의 편차는 포펫 O-링의 마찰력으로부터 유발되는 것임을 보였다. 부가적으로 파일럿스테이지의 다른 주요부품인 포펫 스프링과 조절자의 주요설계인자들도 식별하였고 이들의 결정과정도 본 연구에서 보였다.

• 드라이브 ㆍ 컨트롤
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• 제17권2호
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• pp.55-62
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• 2020

There are two types of IMV for MCV, the spool type and the poppet type. The spool type is used in the existing excavator MCV and easily meets large-capacity flow conditions, but has a flow force problem which affects the spool control. The poppet type stably blocks the flow and has excellent rapid response. However, the larger the capacity, the larger the diameter of the poppet needed, requiring a strong spring to withstand the oil pressure. In this study, a bi-directional three-stage IMV for MCV that can be used in medium and large hydraulic excavators was proposed. This is a poppet type, enabling bi-directional flow control and resolves the problem of proportional solenoid suction force limitation. To investigate the validity of the proposed valve, the system was mathematically modeled and the static and dynamic characteristics were investigated through the simulation using commercial software. It has been concluded that the reverse flow is possible in a regeneration circuit and that the proposed IMV can be used to perform various excavation modes.

• 한국자동차공학회논문집
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• 제19권2호
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• pp.57-65
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• 2011

In this paper, a hydropneumatic modeling and dynamic analysis of a heavy truck semi-active cabin air suspension system is presented. Semi-active cabin air suspension system improves driver's ride comfort by controlling the damping characteristics in accordance with driving situation. So it can reduce vibration between truck frame and cabin. Semi-active cabin air suspension system is consist of air spring, leveling valve and CDC shock absorber, and full cabin system are mathematically modelled using AMESim software. Simulation results of components and full cabin system are compared with experimental data of components and test results of a cabin using 6 axis simulation table. It is found that the simulation results are in good agreements with test results, and the hydropneumatic model can be used well to predict dynamic characterics of heavy truck semi-active cabin air suspension system.

• 한국자동차공학회논문집
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• 제16권4호
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• pp.128-134
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• 2008

In this paper, a hydropneumatic modeling and analysis of a heavy truck cabin air suspension system is presented. Cabin air suspension system is a system which improves ride comfort of a heavy truck and it can reduce vibration between truck frame and cabin. The components of the system, air spring, shock absorber, leveling valve and full cabin system are mathematically modelled using AMESim software. Simulation results of components and full cabin system are compared with experimental data of components and test results of a cabin using 6 axis simulation table. It is found that the simulation results are in good agreements with test results, and the hydropneumatic model can be used well to predict dynamic characteric of heavy truck cabin air suspension system.

• Journal of international Conference on Electrical Machines and Systems
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• 제2권1호
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• pp.97-103
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• 2013

This paper describes the characteristics of Electronic Throttle Controller (ETC) module in BLDC motor without the hall sensor for detecting a rotor position. The proposed ETC control system, which is mainly consisted of a BLDC motor, a throttle plate, a return spring and reduction gear, has a position sensor with an analogue voltage output on the throttle valve instead of BLDC motor for detecting the rotor position. So the additional commutation information is necessarily needed to control the ETC module. For this, the estimation method is applied. In order to improve and obtain the high resolution for the position control, it is generally needed to change the gear ratio of the module or the electrical switching method etc. In this paper, the 3-phase switching between successive commutations is adapted instead of the 2-phase switching that is conventionally used. In addition, the position control with a variable PI gain is applied to improve a dynamic response during a transient period and reduce vibration at a stop in case of matching position reference. The mentioned method can be used to estimate the commutation state and operate the high-precision position control for the ETC module and the high response characteristics. The validity of the proposed method is examined through the experimental results.

• 한국자동차공학회논문집
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• 제16권5호
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• pp.92-99
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• 2008

This paper describes an signal processing method for the hall sensorless position control of ETC control system using a BLDC motor. The proposed ETC control system, which is mainly consisted of a BLDC motor, a throttle plate, a return spring and reduction gear, has a position sensor with an analog voltage output on the throttle valve instead of BLDC motor for detecting rotor position of motor. So the additional commutation information is necessarily needed to control the mentioned ETC module. In order to estimate and determine the commutation state, it is proposed to properly manipulate the resolution of A/D converter considering the mechanical parameter, that is, the number of motor slot and the ratio of reduction gear. Through this method, the estimation of commutation state for operating the system is possible and the discrete signal for commutation is stably obtained. The validity of the method is examined through the experimental results.

• 전력전자학회논문지
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• 제2권1호
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• pp.26-32
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• 1997

본 논문에서는 자동차나 항공기에서 많이 사용되고 있는 고속 솔레노이드 밸브의 플런저형 솔레노이드에 대한 설계기술을 확보하기 위하여, 수치해석을 통해 플런저의 이동시간에 대해 설계 파라메타들이 미치는 영향 및 솔레노이드의 동작특성을 검토하였다. 솔레노이드의 형상이 원통형이므로 축대칭원통좌표계를 이용하였고, 특히 전자기적 부분의 이론 해석시 와전류에 의한 영향을 고려하였으며, 가정자로법에 의해 퍼미언스를 계산하여 해석에 활용하였다. 구해진 파라메타의 해석 결과를 참고로 하여, 파라메타 값을 약간씩 변화시켜서 시간에 따른 플런저의 변위, 전류, 흡인력과의 관계등 동특성을 재해석하는 과정을 반복하여 최적치를 도출하였다. 도출된 최적치를 사용한 모의실험결과 플런저 이동시간은 1.8[ms] 정도의 고속이 됨을 알 수 있었다.

• 드라이브 ㆍ 컨트롤
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• 제17권4호
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• pp.113-124
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• 2020

Most of the work of construction equipment and agricultural machinery is done in off-road conditions. Autonomous driving required in these conditions uses GPS sensors, and PID controllers to control their speed and position. The hydrostatic steering, which is composed of a PSU, hydraulic hoses, and cylinders, rather than a mechanical coupling is used in these equipments. The PSU plays a key role in hydrostatic steering. Precise control of the position under various conditions requires detailed behavioral analysis of the basic components and operation. Two Gerotor PSU is now a commonly used safer option. The components of the PSU can be divided into mechanical and hydraulic actuating elements by its behavior. Since the system is combined by mechanical and hydraulic elements, the modelings are performed using Amesim, which is one of the most effective for the multi-domain dynamic system analysis. To confirm the validity of the model, input torque and pressures are checked with varying steering speed. The opening and the steering speed of normal and newly designed control valve set is investigated with the effect of centering spring force and friction. Finally, simulation results with fully detailed model with two gerotors are analyzed and compared with simple model.

• 한국항공우주학회지
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• 제43권9호
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• pp.822-829
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• 2015

본 논문에서는 압전재료를 이용하여 중소형 무인기 브레이크 시스템에 적용 가능한 압전유압펌프를 설계 및 제작하고, 제작된 압전유압펌프의 성능검증 실험을 수행하였다. 중소형 무인기급 목표 항공기를 선정하여 브레이크 시스템의 요구조건을 분석하였으며, 이를 바탕으로 압전유압펌프의 성능 요구조건을 선정하였다. 요구조건을 만족하는 압전유압펌프의 형상설계를 수행하였으며, 고속 동작 조건에서도 유체의 역류를 효과적으로 차단시킬 수 있는 체크밸브를 비롯한 모든 구성품을 제작하였다. 제작된 압전유압펌프의 성능검증을 위해 실험장치를 구성하여 무부하 토출특성, 부하 시 압력형성 특성실험을 수행하였다. 실험결과, 무부하 최대 토출유량은 80 Hz에서 120.04 cc/min이고, 부하 시 최대 토출압력은 140 Hz에서 783.17 psi이고, 압력형성 반응속도는 약 30 ms 이내임을 확인하였다. 이는 설계 제작된 압전유압펌프가 펌프성능 요구조건을 충족하고 있다고 판단된다.