• 한국철도학회:학술대회논문집
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• 한국철도학회 2010년도 춘계학술대회 논문집
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• pp.1389-1394
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• 2010

This paper describes the evaluation of structural integrity and dynamic characteristic of inertial load test equipments for performance test of railway vehicle propulsion control system. The propulsion control system of railway vehicle has to be confirmed of safety and reliability prior to it's application. Therefore, inertial load test equipments were designed through theoretical equation for performance test of propulsion control system. The structural analysis of inertial load test equipments was conducted using Ansys v11.0 and it's dynamic characteristic was evaluated the designed using Adams. The results showed that the structural integrity of inertial load test equipment was satisfied with a safety factor of 10.2. Also, the structural stability was proved by maximum dynamic displacement of 0.82mm.

• 한국철도학회논문집
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• 제13권4호
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• pp.363-370
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• 2010

본 논문은 철도차량용 추진제어장치의 성능평가를 위한 관성부하 시험설비의 구조안전성 및 동특성 평가를 연구하였다. 추진제어장치는 철도차량의 핵심 부품으로서 차량에 적용하기 전에 안정성 및 신뢰성 검증이 충분히 이루어 져야 한다. 따라서 추진제어장치의 성능시험을 위한 관성부하 시험설비를 이론식을 바탕으로 하여 설계하였다. 설계된 관성부하 시험설비에 대해 Ansys v11.0을 이용하여 구조해석을 수행하였으며, ADAMS를 통해 동특성을 평가하였다. 관성부하 시험설비의 구조안전성은 조합하중하의 베어링에서 안전계수가 10.2로 만족하였다. 또한, 동적 시뮬레이션에 따른 플라이휠은 0.83mm이내의 최대진폭변위로 구조적 안정성이 확보되었다.

• 대한기계학회논문집
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• 제8권2호
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• pp.119-126
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• 1984

본 논문에서는 자유단에 부착된 질량의 관성모우멘트가 Beck's column의 안정 성에 미치는 영향을 연구하였다.

• 한국군사과학기술학회지
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• 제25권1호
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• pp.9-22
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• 2022

A fighter performing a reconnaissance mission is equipped with a pod that drives optical/infrared sensors for acquiring and identifying target information on the lower part of the fuselage. Due to the nature of the reconnaissance mission, the fighter performs high speed evasive maneuvers, and the resulting load should be considered importantly for the development of the pod. This paper concerns a numerical investigation into the inertial and aerodynamic loads of the airborne pod of high performance aircrafts. For the aerodynamic load analysis, the pylon and pod shapes are added to the fighter 3D model, and the commercial software was used for static and dynamic analysis. Considering the practical mission conditions, the common/extreme conditions were established respectively in the static and dynamic situations of pods and the driving torque could be tripled under dynamic conditions. In the analysis of inertia load, a 3-DOF model considering roll and turning maneuvers was derived by the Lagrangian method, and then the numerical integration method was applied to the analysis. As a results, it was conformed that the inertia load was generally induced at a low level compared to the aerodynamic load, but depending on the unbalance mass condition of the pod, the inertia load cannot be negligible.

• 대한기계학회논문집A
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• 제38권12호
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• pp.1395-1401
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• 2014

중력이 거의 작용하지 않는 마이크로중력환경에서 소동물의 질량이 측정 가능한 고성능 관성저울을 개발하기 위해, 약 100g의 측정시료를 이용하여 관성저울의 핵심 디자인 파라미터인 로드셀의 응답특성을 평가하였다. 정확한 성능평가를 위해서 1.5초의 마이크로중력환경을 제공할 수 있는 15m 자유 낙하탑을 활용하였으며, 살아 있는 동물의 질량을 측정해야 하는 점을 고려하여 측정시료의 감속 크기 변화에 따른 로드셀의 응답특성를 파악하였다. 동일한 가속도로 가 감속되는 표준시료와 측정시료의 관성력 비의 분석결과 로드셀이 장착된 가속판이 평균 이동속도 0.5 m/s 이상으로 운동하는 경우에 한하여 설계 기준에 부합하는 것을 알 수 있었다.

• 대한조선학회논문집
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• 제53권6호
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• pp.529-535
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• 2016

This study focuses on the comparison of measured data from 6-DOF motion sensor and strain gauge installed in the IBRV ARAON during 2015 summer voyage in the Arctic. Procedures to calculate the global ice load from MotionPak II inertial measurement system and the local load from stain gauge system are discussed. The ship's speed and peak load are determined in the concept of an ice collision "event". It is found that the peak values in the global ice calculated form whole ship motion analysis fall in the range of 1.5~3 times of the local ice load based in strain gauge measurement.

• International Journal of Precision Engineering and Manufacturing
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• 제9권3호
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• pp.46-50
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• 2008

The present status and future prospects of the levitation mass method (LMM), a technique for precision mass and force measurement, are reviewed. In the LMM, the inertial force of a mass levitated using a pneumatic linear bearing is used as the reference force applied to the objects being tested, such as force transducers, materials, or structures. The inertial force of the levitated mass is measured using an optical interferometer. We have modified this technique for dynamic force calibration of impact, oscillation, and step loads. We have also applied the LMM to material testing, providing methods for evaluating material viscoelasticity under an oscillating or impact load, evaluating material friction, evaluating the biomechanics of a human hand, and generating and measuring micro-Newton-level forces.

• 대한조선학회 특별논문집
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• 대한조선학회 2015년도 특별논문집
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• pp.63-68
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• 2015

This paper presents fatigue analysis of helideck structures located in FPSO. After FPSO is moved to the target position where production of resource is performed, FPSO stays at the target position and performs production of resource, storage and off-loading during the design life. Helideck structure is located in FPSO essentially for the movement of personnel and life rescue at emergency situations by using helicopters. Because inertial load induced by FPSO motion and landing and taking-off load of helicopter occur at helideck structures cyclically, helideck structures should be designed to withstand fatigue loads. Therefore, The fatigue assessment of helideck structures should be performed with fatigue loads. Effect of stress concentration due to misalignment between welded plates is considered in fatigue assessment additionally.

• Structural Engineering and Mechanics
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• 제82권3호
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• pp.283-294
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• 2022

An inerter is a passive mechanical element whose inertance can be thousands of times its own physical mass. This paper discusses the application of an inerter-based passive control system, termed rotational inertial double-tuned mass damper (RIDTMD), to mitigate human-induced floor vibrations. First, the acceleration frequency response function of the floor with an RIDTMD is first derived. It is then employed to determine the optimal design parameters of the RIDTMD using the extended fixed-points technique. Based on a theoretical analysis, design-oriented empirical functions are proposed for the RIDTMD optimal parameters, whose performance for floor vibration control is evaluated by numerical examples, in which three typical human-induced load types are considered: walking, jumping, and bouncing. The results indicate that the applicability and effectiveness of the RIDTMD for human-induced floor vibration control are robust for various load types, load frequencies, and floor natural frequencies. For the same mass ratio, the RIDTMD is better than the TMD in reducing the floor vibration amplitude and improving the effective frequency suppression bandwidth, and for the same vibration suppression effect, the mass of the RIDTMD is much lighter than that of the TMD.

• 한국추진공학회지
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• 제8권3호
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• pp.17-26
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• 2004

본 연구에서 동력 전달 시스템은 분리 축 방식의 가스 터빈 엔진의 축 동력을 발전기 전력으로 변환하여, 이것을 프로펠러를 구동하는 추력 모터에 공급하는 방식으로 구성되어있다. 여기에 사용된 가스 터빈 엔진은 엔진 축 마력 317shp(236kw)을 약110kw (147shp)으로 플랫 레이팅(flat rating) 하여 운용한다. 본 시험 장치의 엔진은 가스 터빈엔진 출력축과 발전기 사이에 부하 변화 시 댐핑(damping)역할을 할 수 있도록 플라이 휠(flywheel)을 장착하였다. 이 때 플라이휠의 적절한 관성 모멘트가 고려되지 않으면, 발전기와 모터는 부하 상승에 의한 엔진으로부터 요구되는 출력을 얻을 수 없으며, 또한 엔진이 정상적으로 작동하지 않음을 확인할 수 있다. 따라서 제공된 엔진 데이터와 엔진 시험 데이터로부터 동역학적인 천이 효과에 의한 성능 분석을 함으로써 관성 모멘트의 요구 범위를 결정하였다. 재설계한 플라이휠을 장착 시험한 결과, 본 시스템에서 요구한 출력을 얻을 수 있었다.