• 제목/요약/키워드: inertia properties

검색결과 169건 처리시간 0.034초

건물 내장재의 화재위험성 평가 방법 (A Fire Hazard Assessment of Interior Finish Materials)

  • 김운형
    • 한국화재소방학회논문지
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    • 제12권2호
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    • pp.17-28
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    • 1998
  • 건물 화재시 예상되는 내장재의 실째 화재성농올 기준으로 한 위험성 명가방법올 제시하였다. 이률 위해 ISO Room Corner Test. (9705)를 기준으로 Qui ntie re의 화재확산 모델을 이용하여 내장재의 열 적 특성과 플래쉬 오버 도달시간과의 상관성을 유도하고 스쩨덴의 실제 시험결과와 비교 분석하였다. 이 결과, 내장재의 상대척인 화재위험성은 화재확산 변수 b륨 기준으로 명가될 수 있었다.

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지르코니아$(ZrO_2)$ 분말을 이용한 시계케이스의 세라믹 사출성형 (Ceramic injection molding of the watch case composed by zirconia$(ZrO_2)$ powder)

  • 곽태수;신호용;임종인
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2005년도 추계학술대회 논문집
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    • pp.275-278
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    • 2005
  • This study has focused on manufacturing technique of powder injection molding of watch case which made from zirconia powder. A series of computer simulation process was applied to prediction of the flow pattern in the inside of the mould and defects as weld line. The material properties of melted feedstock inclusive of the PVT graph and thermal viscosity flowage properties were measured for obtaining the input data in computer simulation. Also, molding experiment was conducted and the results of experiment showed that good agreement with simulation results far flow pattern and weld line location. On the other hand, gravity and inertia effect have an influence on velocity of melt front because of high density of ceramic powder particles in powder injection molding against the polymer injection molding process. In the experiment, the position of melt front was compared with upper gate and lower gate position. The gravity and inertia effect could be confirmed in the experimental results.

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여유자유도/여유구동 인체형 로봇의 임피던스 생성방식 (Impedance modulation of anthropomorphic robots with kinematic and force redundancies)

  • 이병주;김희국;이재훈
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1997년도 한국자동제어학술회의논문집; 한국전력공사 서울연수원; 17-18 Oct. 1997
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    • pp.1289-1292
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    • 1997
  • Typical biomechanical system such as human body and mammals possess abundant muscles which are more than required for motion generation of such systems. We have shown that the excess number of muscles play important roles in spring-like impedance modulation. redundant kinematic structure, which is another feature of biomechanical systems, allows modulations of inertia and damping properties of such systems. In this work, we propose a frequency modulation algorithm which combines the spring-like impedance with inertia impedance. also, a load distribution method for frequency modulation is also introduced. The frequency modulation represents a simulataneous control of force and kinematic redundancies, which has not been addressed in the literature.

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A gain scheduling method for the vibration suppression servo controller of articulated robots

  • Lee, Sang-Hun;Yim, Jong-Guk;Hur, Jong-Sung;Park, Jong-Hyeon
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2003년도 ICCAS
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    • pp.2725-2730
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    • 2003
  • In this study we present a vibration controller for articulated robots that has flexible joints modeled as a 2-mass system. Most of articulated robots have time varying load inertias for each axis according to its motion. Moreover, the inertias vary drastically; for the base axis of articulated robots it may vary about 10 times of its minimum value. But, for industrial robots and many mechatronic devices, it is desirable to maintain control performance in spite of load inertia variation. So we propose a control gain adjustment rule considering the time-varying nature of load inertia. In this gain-adjusting algorithm, the pole locations are in proportion to the anti-resonance frequency of the 2-mass system. The simulation and experimental results show uniform properties in overshoot in spite of the variation of load.

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고무와 압전작동기를 이용한 무인항공기 EO/IR 센서 마운트의 설계 및 능동 진동 제어 (Design and Active Vibration Control of UAV EO/IR Sensor Mount Using Rubber Element and Piezoelectric Actuator)

  • 박동현;최승복
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2008년도 추계학술대회논문집
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    • pp.743-748
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    • 2008
  • This paper presents an inertia type of piezostack based active mount for unmanned aero vehicle (UAV) camera system. After identifying the stiffness and damping properties of the rubber element and piezostack a mechanical model of the active mount system is established. The governing equation of mount is them derived and expressed in a state space farm. Subsequently, a sliding mode controller which is robust to uncertain parameters is designed in order to reduce the vibration imposed according to the military specification associated with UAV camera mount system operation. Control performances such as acceleration and transmitted force are evaluated through both computer simulation and experimental implementation.

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종이성형구조물의 구조적 강도에 대한 이론분석과 유한요소해석 (Theoretical and Finite Element Analysis for Structural Strength of Paperboard-stacked Structure)

  • 박종민;이명훈
    • 한국포장학회지
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    • 제5권1호
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    • pp.13-20
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    • 1999
  • Not only is it important that the physical properties of the paperboards be appropriate for the intended end use, but the proper arrangement of the component in the built-up board is essential for attaining the optimum moment of inertia and the maximum load-carrying ability in a box. It is known to be impossible to estimate the stress distribution and deflection pattern by experiments or theoretical analysis when the corrugated fiberboard get the bending force. This study was tried theoretical and finite element analysis to analyze structural strength characteristics of corrugated fiberboards. If the linerboard and corrugating medium of every corrugated fiberboards is made from the same material, the location of neutral axis comes close to inside liner in order of DMA, DM, DMB, SW and DW, and moment of inertia of area decreases in order of DMA, DMB, DW, DM and SW. With the finite element analysis, deflection of applied loads represented SW, DM, DMA, and TW in the order of their value.

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초고진공중의 Tribo-Coating 막의 윤활특성(II) (Lubricating Properties of Tribo-Coating Film in Ultra High Vacuum)

  • 김형자;전태옥
    • Tribology and Lubricants
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    • 제10권4호
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    • pp.69-74
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    • 1994
  • The space world under zero gravity and super vacuum where the space machine works has only friction and inertia. Inertia of acceleration and diceleration is accurately obtained by computing while friction is always in contact surface and unsteady. The sur soundings under super vacuum make surface friction more complicate. [1,2]. Therefore, method to lubricate stably the contact surface for long term in space machine is very important and friction for space machine proves to be true by several accident of space projects. In spite of that accident, method of lubrication and lubricants to keep stablity for long term in space machine have not been established so far. Lubrication for space machine is very important and under developings over the world. In this study we suggest a new lubricating technology, which improves powerful for space machine.

압전작동기를 이용한 무인항공기 EO/IR 센서 마운트의 능동 진동 제어 (Active Vibration Control of UAV EO/IR Sensor Mount Using Piezoelectric Actuator)

  • 박동현;최승복
    • 한국소음진동공학회논문집
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    • 제18권12호
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    • pp.1278-1285
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    • 2008
  • This paper presents an inertia type of piezostack based active mount fur unmanned aero vehicle (UAV) camera system. After identifying the stiffness and damping properties of the rubber element and piezostack a mechanical model of the active mount system is established. The governing equation of mount is then derived and expressed in a state space form. Subsequently, a sliding mode controller which is robust to uncertain parameters is designed in order to reduce the vibration imposed according to the military specification associated with UAV camera mount system operation. Control performances such as acceleration and transmitted force are evaluated through both computer simulation and experimental implementation.

선내 탑재 마운팅 장비의 동특성에 관한 실험적 연구 (An Experimental Study on the Dynamic Characteristics of Onboard Machinery with Resilient Mounts)

  • 김극수;최수현
    • 대한조선학회논문집
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    • 제40권2호
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    • pp.28-33
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    • 2003
  • This study is performed to evaluate and design the dynamic characteristics of the onboard machinery with resilient mounts. To avoid resonance with onboard machinery and external force, it is necessary to calculate natural frequencies of the resilient mounting system more accurately. Natural frequencies of on board machinery are determined by rigid body properties(mass, moment of inertia, center of mass) of machinery and stiffness of mounts. But it is very difficult to calculate rigid body properties theoretically. And stiffness properties of rubber mounts vary with dynamic displacement, pre load, frequency and temperature, and so on. In this study, we have identified rigid body properties using experimental modal analysis and estimated dynamic stiffness of rubber mount for onboard machinery using measured vibration response during seatrial. We measured displacement excitation through deck under mounts and evaluated relationship between modes of resilient mounting system and main excitation sources of a ship.

에너지 효율 향상을 위한 직렬형 머니퓰레이터의 관성 파라미터 설계 최적화 방법 (Design Optimization Method of Inertial Parameters of Serial Manipulators for Improving the Energy Efficiency)

  • 황순웅;김현국;최윤성;신규식;한창수
    • 한국산학기술학회논문지
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    • 제17권11호
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    • pp.395-402
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    • 2016
  • 이 논문은 직렬형 머니퓰레이터의 관성 성질을 고려하여 에너지 효율을 향상 시키기 위한 설계 방법에 대해 논하였다. 이 방법은 운동방정식에 가장 많은 영향을 끼치는 관성 행렬을 분석하여 최적화 문제의 구속 조건에 대입하는 방식이다. 이를 위해, 첫 번째로 초기에 설계된 머니퓰레이터에 대한 동적 모델링을 도출하고 여기서 표현되는 관성 행렬의 특성을 분석한다. 두 번째로 분석된 관성 행렬의 변화 정도를 정량화하는 지표를 정의하여 구속 조건과 설계 파라미터의 경계조건을 설정하였다. 마지막으로 토크를 목적 함수로 정하고 앞서 정의된 구속 조건과 경계조건을 통하여 최적화를 수행한다. 또한, 목적 함수 외에 관성, 에너지 및 질량에 관련된 보조 지표를 정의하고 최적화된 파라미터가 요구성능을 만족하는지 다시 한번 확인하는 과정을 거치는 설계 알고리즘을 제안하였다. 제안한 설계 알고리즘의 수행 결과로 토크 최소화를 통하여 에너지 효율이 향상되었으며, 제안된 방법을 공간상의3 자유도 직렬 머니퓰레이터에 시뮬레이션 테스트 하였다. 이 설계 알고리즘은 일반적으로n 자유도를 가지는 머니퓰레이터에도 적용이 가능하다.