• 제목/요약/키워드: Inertia mass

검색결과 335건 처리시간 0.023초

형상비 3.5 RC교각의 실험 방법에 의한 내진성능 분석 (Seismic Performance Analysis of RC Bridge Piers with 3.5 Aspect Ratio depending on Testing Methods)

  • 홍현기;박창영;정영수
    • 한국콘크리트학회:학술대회논문집
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    • 한국콘크리트학회 2008년도 춘계 학술발표회 제20권1호
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    • pp.93-96
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    • 2008
  • 이 논문은 근단층지반운동(NFGM)하에서 내진성능을 평가하기 위한 RC교각의 진동대, 준정적, 유사동적 실험을 다룬다. 5개의 실험체가 수행되었다. 축소 모형을 제작하고 상부구조물의 중량 에 의한 축력의 효과는 프리스트레스에 의해 구현하였다. 지진이 발생할 때 상부 구조물의 횡방향 관성력은 진동대의 제한된 용량 때문에 교각 실험체에 연결한 질량 프레임으로 모사하였다. 특히, 진동대 실험에서 질량 모사 프레임이 교각 모델과 같은 변위로 움직이면서 마찰 효과를 최소화할 수 있도록 고려하였고 이에 대한 검증을 실시하였다. RC교각의 축소 계수를 4.25로 설정 하였다.

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Electronic Wedge Brake 시스템의 클램핑력 추정 및 Failsafe 제어 알고리즘 설계에 관한 연구 (A Study on the Clamping Force Estimation and Failsafe Control Algorithm Design of the Electronic Wedge Brake System)

  • 정승환;이형철
    • 한국자동차공학회논문집
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    • 제24권1호
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    • pp.16-23
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    • 2016
  • The EWB(electronic wedge brake) is one in which the braking force is developed in a wedge and caliper system and applied to a disk and wedge mechanism. The advantage of the wedge structure is that it produces self-reinforcing effect and hence, utilizes minimal motor power, resulting in reduced gear and current. The extent of use of clamping force sensors and protection from failure of the EWB system directly depends on the level of vehicle mass production. This study investigated the mathematical equations, simulation modeling, and failsafe control algorithm for the clamping force sensor of the EWB and validated the simulations. As this EWB system modeling can be applied to motor inductance, resistance, screw inertia, stiffness, and wedge mass and angle, this study could improve the accuracy of simulation of the EWB. The simulation results demonstrated the braking force, motor speed, and current of the EWB system when the driver desired to the step and pulse the brake force inputs. Moreover, this paper demonstrated that the proposed failsafe control algorithm accurately detects faults in the clamping force sensor, if any.

지점 위에 질량과 강성이 큰 연결기를 갖는 다경간 보의 모드편재 (Mode Localization in Multispan Beams with Massive and Stiff Couplers on Supports)

  • Dong-Ok Kim;Sun-Kyu Park;In-Won Lee
    • 소음진동
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    • 제8권6호
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    • pp.1166-1171
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    • 1998
  • 본 연구에서는 이웃한 두 경간 사이에 있는 질량과 강성을 갖는 연결기가 모드편재에 미치는 영향을 해석적으로 분석하고 수치예제를 통해 그 결과를 검증하였다. 연결기의 강성이 구조물의 모든 고유모드를 모드편재에 민감하게 만드는 반면 연결기의 질량은 고차모드의 민감도를 심각히 증가시킨다. 또한 본 연구에서는 일부 고유모드에서 새로운 형태의 반편재현상을 관찰하였다. 반편재현상이 발생하는 모드에서는 경간 사이의 연성이 매우 약하고 구조 변화가 심각하게 발생하더라도 모드편재 현상이 발생하지 않거나 발생하더라도 매우 미약하게 나타난다. 해석적 분석에서는 연결기를 사이에 두고 있는 두개의 부구조물을 단순화 시킨 강성-질량 시스템을 대상으로 하였다. 수치예제에서는 중간 지점에 회전강성과 회전질량을 갖으며 단순지지된 이경간 연속보를 해석하였다.

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Suppression of aerodynamic response of suspension bridges during erection and after completion by using tuned mass dampers

  • Boonyapinyo, Virote;Aksorn, Adul;Lukkunaprasit, Panitan
    • Wind and Structures
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    • 제10권1호
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    • pp.1-22
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    • 2007
  • The suppression of aerodynamic response of long-span suspension bridges during erection and after completion by using single TMD and multi TMD is presented in this paper. An advanced finite-element-based aerodynamic model that can be used to analyze both flutter instability and buffeting response in the time domain is also proposed. The frequency-dependent flutter derivatives are transferred into a time-dependent rational function, through which the coupling effects of three-dimensional aerodynamic motions under gusty winds can be accurately considered. The modal damping of a structure-TMD system is analyzed by the state-space approach. The numerical examples are performed on the Akashi Kaikyo Bridge with a main span of 1990 m. The bridge is idealized by a three-dimensional finite-element model consisting of 681 nodes. The results show that when the wind velocity is low, about 20 m/s, the multi TMD type 1 (the vertical and horizontal TMD with 1% mass ratio in each direction together with the torsional TMD with ratio of 1% mass moment of inertia) can significantly reduce the buffeting response in vertical, horizontal and torsional directions by 8.6-13%. When the wind velocity increases to 40 m/s, the control efficiency of a multi TMD in reducing the torsional buffeting response increases greatly to 28%. However, its control efficiency in the vertical and horizontal directions reduces. The results also indicate that the critical wind velocity for flutter instability during erection is significantly lower than that of the completed bridge. By pylon-to-midspan configuration, the minimum critical wind velocity of 57.70 m/s occurs at stage of 85% deck completion.

선형(線形) 변단면(變斷面) I-형(型) 부재(部材)의 자유진동(自由振動) (Free Vibrations of Linearly Tapered I-Beams)

  • 이용우;민경주
    • 대한토목학회논문집
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    • 제14권5호
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    • pp.1023-1031
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    • 1994
  • 선형변단면(線形變斷面) I-형(型) 부재(部材)의 3차원(次元) 공간(空間)에서의 고유진동해석(固有振動解析)을 위하여 회전관성(回轉慣性)도 포함하는 컨시스턴트 질량행렬(質量行列)을 유도하였다. 유도과정(誘導過程)에서 정확한 형상함수(形狀函數)를 사용했다. 일반적으로 많이 사용되는 변단면부재(變斷面部材)의 경사(傾斜)는 매우 작으므로 '정형식(整形式)'으로 표현된 행렬(行列)을 사용하여 변단면(變斷面) 부재(部材)를 포함하는 구조물(構造物)을 해석할 때에 신빙성 없는 결과를 얻게 된다. 이러한 수치적(數値的) 오류(誤謬)를 피하기 위하여 '급수식(級數式)'을 유도했다. 변단면(變斷面) 부재(部材)의 구조물(構造物)을 해석하기 위하여 본 연구에서 유도된 질량행렬(質量行列)을 사용하여 구한 고유진동수(固有振動數)와 변단면(變斷面) 부재(部材)를 균일단면(均一斷面)의 탑형태(塔形態)로 표현하여 ANSYS에서 구한 고유진동수(固有振動數)를 비교하여 본 연구 결과 효율성과 정확성이 증진된 것을 확인하였다. 본 연구에서 유도된 질량행렬(質量行列)은 변단면(變斷面) 부재(部材)와 균일단면(均一斷面) 부재(部材)의 자유진동해석(自由振動解析)에 사용할 수 있다.

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수중운동체의 강제동요시험 및 포텐셜 계산에 의한 부가질량 추정 (Added Mass of Submerged Bodies Obtained by Forced Oscillation Tests and Numerical Calculations of Potential Flow)

  • 김동진;이경중;권창섭;김연규;박진영;전봉환
    • 대한조선학회논문집
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    • 제59권4호
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    • pp.214-224
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    • 2022
  • It is necessary to estimate manoeuvring characteristics of submerged bodies at the design stage in order to ensure the safe operations. In this study, added mass coefficients in the mathematical model of submerged bodies are estimated by captive model tests and numerical calculations. Two kinds of models, MARIN 'BB2'submarine model and AUV (Autonomous unmanned vehicle) model are utilized in the forced oscillation tests. Compared to BB2 submarine, AUV with cylindrical type hull form shows relatively small added masses in roll, pitch, and yaw directions. Next, numerical calculations based on potential theory are performed under the assumption that viscous effects on inertia forces are negligible. Added masses obtained by numerical calculations are in good agreements with forced oscillation test results. And if slow manoeuvres of submerged bodies are presumed, some of velocity coupled terms can be approximated by combinations of added mass coefficients.

대형 자동차 하이브리드 유압 구동시스템의 회로구성과 특성해석에 관한 연구 (A Study on the Circuit Composition and Characteristics Analysis for Heavy-Duty Vehicular Hybrid Hydraulic Driving System)

  • 이재구;이재천;한문식
    • 한국자동차공학회논문집
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    • 제12권2호
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    • pp.197-204
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    • 2004
  • An accumulator in hydraulic systems stores kinetic energy during braking action, and then that controls hasty surge pressure. An energy recovery system using accumulator seems to be advantageous for ERBS due to its high energy density. This study suggests a method to decide suitable accumulator volume for ERBS. The method is based upon energy conservation between kinetic energy of moving inertia and elastic energy of accumulator. The energy conversion was analyzed and a simple formula was derived. Also accumulator tests were conducted for different load mass and motor speed. A series of test work were carried out in the laboratory and the dynamic characteristics of the hydraulic motor system, such as the surge pressure and response time, were investigated in both brake action and acceleration action and these results show that the proposed design is effective for decision accumulator volume in ERBS.

A Study on the Hydraulic Pump/Motor Control in the Flywheel Hybrid Vehicle

  • Oh, Boem-Sueng;Ahn, Kyoung-Kwan;Cho, Yong-Rae
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2004년도 ICCAS
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    • pp.307-311
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    • 2004
  • In this study, a novel hybrid vehicle is proposed. The vehicle has a flywheel-engine hybrid system. Flywheels are more effective as energy charge systems than electric batteries in a respect of output power density. However, transmissions to effectively drive flywheels are very complex systems such as CVTs (Continuously Variable Transmissions). In the proposed hybrid vehicle, Constant Pressure System is employed, which is hydraulic power transmission. Using Constant Pressure Systems, hydraulic CVTs are easily realized with variable displacement pumps/motors. In this paper, firstly, the proposed flywheel hybrid vehicle making use of Constant Pressure System is described. Secondly, fuel consumption characteristics of the flywheel hybrid vehicle are experimentally examined with the stationary test facility, which employs a flywheel as a load emulating vehicle inertia. Finally, the experimental results and discussions are described. Fuel consumption of 26km/L is expected for 10 mode driving schedule with vehicle mass of 1500kg.

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Closed-form solutions for non-uniform axially loaded Rayleigh cantilever beams

  • Sarkar, Korak;Ganguli, Ranjan;Elishakoff, Isaac
    • Structural Engineering and Mechanics
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    • 제60권3호
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    • pp.455-470
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    • 2016
  • In this paper, we investigate the free vibration of axially loaded non-uniform Rayleigh cantilever beams. The Rayleigh beams account for the rotary inertia effect which is ignored in Euler-Bernoulli beam theory. Using an inverse problem approach we show, that for certain polynomial variations of the mass per unit length and the flexural stiffness, there exists a fundamental closed form solution to the fourth order governing differential equation for Rayleigh beams. The derived property variation can serve as test functions for numerical methods. For the rotating beam case, the results have been compared with those derived using the Euler-Bernoulli beam theory.

끝단 강체를 갖고 맥동 제어추력을 받는 양단 자유보의 동적 안정성 (Dynamic Stability of a Free-Free Beam with a Tip Rigid Body under a Controlled Pulsating Thrust)

  • 류봉조;이규섭;성윤경;최봉문
    • 대한기계학회논문집A
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    • 제24권1호
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    • pp.232-239
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    • 2000
  • The paper describes the parametric instability of free-free beams subjected to a controlled pulsating follower force. The beam has a tip rigid body not a mass point, and the direction of pulsating follower force is controlled by the direction control sensor. Equations of motion are derived by Hamilton's principle and the instability regions are obtained by finite element formulation. The effects of magnitude, rotary inertia, the distance between free end of the beam and the center of gravity of the rigid body on the instability types and regions are investigated by the change of the constant and periodic part of the follower force.