• 제목/요약/키워드: Follower Load

검색결과 79건 처리시간 0.022초

FVF-Based Low-Dropout Voltage Regulator with Fast Charging/Discharging Paths for Fast Line and Load Regulation

  • Hinojo, Jose Maria;Lujan-Martinez, Clara;Torralba, Antonio;Ramirez-Angulo, Jaime
    • ETRI Journal
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    • 제39권3호
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    • pp.373-382
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    • 2017
  • A new internally compensated low drop-out voltage regulator based on the cascoded flipped voltage follower is presented in this paper. Adaptive biasing current and fast charging/discharging paths have been added to rapidly charge and discharge the parasitic capacitance of the pass transistor gate, thus improving the transient response. The proposed regulator was designed with standard 65-nm CMOS technology. Measurements show load and line regulations of $433.80{\mu}V/mA$ and 5.61 mV/V, respectively. Furthermore, the output voltage spikes are kept under 76 mV for 0.1 mA to 100 mA load variations and 0.9 V to 1.2 V line variations with rise and fall times of $1{\mu}s$. The total current consumption is $17.88{\mu}V/mA$ (for a 0.9 V supply voltage).

일단고정 타단스프링으로 지지된 변단면 Beck 기둥의 임계하중 (Critical Loads of Tapered Beck's Columns with Clamped and Spring Supports)

  • 김석기;박광규;이병구
    • 한국전산구조공학회논문집
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    • 제19권1호
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    • pp.85-92
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    • 2006
  • 이 논문은 일단고정 타단스프링으로 지지된 변단면 Beck 기둥의 임계하중에 관한 연구이다. 기둥의 변단면을 중실 직사각형 단면을 갖는 선형 변단면으로 채택하고, Bernoulli-Euler보 이론을 이용하여 경사종동력이 작용하는 소위 Beck 기둥의 자유진동을 지배하는 상미분방정식과 경계조건을 유도하였다. 이 미분방정식을 수치해석하여 하중-고유진동수 곡선을 얻고 이로부터 발산임계하중 및 동요임계하중을 산출하였다. 수치해석의 결과로부터 변단면 형태, 경사변수 및 스프링 강성이 임계하중에 미치는 영향을 고찰하였다

보조말뚝의 충격하중에 의한 PHC말뚝의 파손유형 고찰 (Study on the Fractures Types of PHC Pile by Impact Load of Follower)

  • 서동남;최상호;김진식;김민갑;이동현;조성준
    • 한국건축시공학회:학술대회논문집
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    • 한국건축시공학회 2021년도 가을 학술논문 발표대회
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    • pp.144-145
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    • 2021
  • This study analyzed the cases of cracks in piles due to the use of followers under construction conditions where water exists inside the piles, and confirmed whether the piles were cracked through a field test simulating the construction conditions in which water pressure inside the piles was generated by a hammer. According to the construction case, under the construction condition where the pile length is 20% to 30% shorter than the drilled length, about 80% cracks occur, so there is a high possibility of cracking due to water inside the pile. A field test was conducted to confirm the type of pile failure due to hammer under the construction condition in which water exists inside the pile. The pile head was not destroyed by the compressive load, and one or more longitudinal cracks occurred along the PC steel wire. The closed end pile generates water pressure by hammer. the follower and cushion(compression plywood) must be drilled at least 0.4D. It is expected that improved quality control will be possible as the water pressure inside the pile is reduced.

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Dynamic Instability of Rocket-Propelled Flying Bodies

  • Sugiyama, Yoshihiko
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2003년도 제21회 추계학술대회 논문집
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    • pp.1-5
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    • 2003
  • This paper deals with dynamic instability of slender rocket-propelled flying bodies, such as launch vehicle and advances missiles subjected to aerodynamic loads and an end rocket thrust. A flying body is simplified into a uniform free-free beam subjected to an end follower thrust. Two types of aerodynamic loads are assumed in the stability analysis. Firstly, it is assumed that two concentrated aerodynamic loads act on the flying body at its nose and tail. Secondly, to take account of effect of unsteady flow due to motion of a flexible flying body, aerodynamic load is estimated by the slender body approximation. Extended Hamilton's principle is applied to the considered beam for deriving the equation of motion. Application of FEM yields standardeigen-value problem. Dynamic stability of the beam is determined by the sign of the real part of the complex eigen-values. If aerodynamic loads are concentrated loads that act on the flying body at its nose and tail, the flutter thrust decreases by about 10% in comparison with the flutter thrust of free-free beam subjected only to an end follower thrust. If aerodynamic loads are distributed along the longitudinal axis of the flying body, the flutter thrust decreases by about 70% in comparison with the flutter thrust of free-free beam under an end follower thrust. It is found that the flutter thrust is reduced considerably if the aerodynamic loads are taken into account in addition to an end rocket thrust in the stability analysis of slender rocket-propelled flying bodies.

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저전력 용량성 센서 인터페이스를 위한 저잡음 CMOS LDO 레귤레이터 설계 (Design of the low noise CMOS LDO regulator for a low power capacitivesensor interface)

  • 권보민;정진우;김지만;박용수;송한정
    • 센서학회지
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    • 제19권1호
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    • pp.25-30
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    • 2010
  • This paper presents a low noise CMOS regulator for a low power capacitive sensor interface in a $0.5{\mu}m$ CMOS standard technology. Proposed LDO regulator circuit consist of a voltage reference block, an error amplifier and a new buffer between error amplifier and pass transistor for a good output stability. Conventional source follower buffer structure is simple, but has a narrow output swing and a low S/N ratio. In this paper, we use a 2-stage wide band OTA instead of source follower structure for a buffer. From SPICE simulation results, we got 0.8 % line regulation and 0.18 % load regulation.

근력을 적용한 경추 모델의 후방 충돌 해석 (Analysis of Whiplash by Rear End Collisions Using a Cervical Spine Model with Preloaded Muscles)

  • 오현우;양석조
    • 대한기계학회논문집A
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    • 제34권2호
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    • pp.139-143
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    • 2010
  • 자동차 충돌에 의하여 편타성 손상이 일어나게 되는데, 대부분 경추부분에서 발생한다. 이러한 편타성손상의 메카니즘은 아직까지 명확히 밝혀지지 않고 있다. 본 논문에서는 다물체 경추에 근육을 부착한 모델을 만들고, 부착된 근육에 follower load 개념에 근거한 최적화방법을 이용하여 계산된 초기힘(preloads)를 가하였다. 경추모델에서 추체, 추간판 및 근육은 인간의 해부학적 정보와 일치시켜 제작되었다. 이번 연구의 목적은 경추모델에 부착된 근육에 초기힘이 존재할 때 초기힘의 편타성 손상에의 영향을 조사하는 것이다. 결론적으로, 초기힘이 존재하는 근육-경추모델의 경우가 초기힘이 존재하지 않는 모델에 비하여 좀더 실제와 일치하는 경향성을 보여주었다.

자유단이 회전스프링으로 구속된 Beck 기둥의 안정성 (Stability of beck's column with a rotatory spring restraining its free end)

  • 윤한익;임순홍;유진석
    • 대한기계학회논문집A
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    • 제21권9호
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    • pp.1385-1391
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    • 1997
  • An analysis is presented on the stability of an elastic cantilever column subjected to a concentrated follower force as to the influence of the elastic restraint and a tip mass at the free end. The elastic restraint is formed by the rotatory springs. For this purpose, the governing equations and boundary conditions are derived by using Hamilton's principle, and the critical flutter loads and frequencies are obtained from the numerical evaluation of the eigenvalue functions of the considered system.

Source-Follower Type Analog Buffer Using Low Temperature Poly-Si TFTs for AMLCDs

  • Chen, Bo-Ting;Tai, Ya-Hsiang;Wei, Ying-Jyun;Tsai, Chun-Chien;Chen, Hsu-Hsin;Huang, Chun-Yao;Kuo, Yu-Ju;Cheng, Huang-Chung
    • 한국정보디스플레이학회:학술대회논문집
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    • 한국정보디스플레이학회 2006년도 6th International Meeting on Information Display
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    • pp.1243-1246
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    • 2006
  • A new source follower circuit for the integrated circuit of AMLCDs is proposed. Active load is added and calibration operation is applied to compensate the circuits. Proposed circuit is capable of minimizing the variation from both timing and device variations through measured results, the uniformity and bias effect are discussed.

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박용디젤기관 밸브기구용 캠-롤러 사이의 탄성유체윤활해석 및 롤러 형상 수정에 관한 연구 (A Study on the Elastohydrodynanic Lubrication Analysis and the Modification of the Roller Profile in the Cam-Roller of the Valve Mechanism for a Marine Diesel Engine)

  • 구영필;강민호;이득우;조용주
    • 한국윤활학회:학술대회논문집
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    • 한국윤활학회 1999년도 제30회 추계학술대회
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    • pp.121-128
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    • 1999
  • In this study, a numerical procedure to analyze 3-dimensional unsteady elastohydrodynamic lubrication was developed. The procedure was applied to the actual cam and roller follower of the valve mechanism for a marine diesel engine. The pressure distribution between the cam and roller follower was calculated for the several cam rotating angles. The pressure spike is shown near the roller edge and it is getting higher as the external load is increased. The roller profile for reducing the pressure spike was suggested by the Hertzian contact analysis.

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유체유동 파이프의 안정성에 미치는 크랙의 영향 (Influence of a Crack on Stability of Pipe Conveying Fluid)

  • 안성진;손인수;윤한익
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2006년도 춘계학술대회논문집
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    • pp.254-257
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    • 2006
  • In this paper a dynamic behavior(natural frequency) of a cracked cantilever and simply supported pipe conveying fluid is presented. In addition, an analysis of the flutter and buckling instability of a cracked pipe conveying fluid subjected to a follower compressive load is presented. Based on the Euler-Bernouli beam theory, the equation of motion can be constructed by using the Lagrange's equation. The crack section is represented by a local flexibility matrix connecting two undamaged beam segments. The crack is assumed to be in the first mode of fracture and to be always opened during the vibrations.

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