• 제목/요약/키워드: Thrust Force

검색결과 681건 처리시간 0.031초

Prediction of a research vessel manoeuvring using numerical PMM and free running tests

  • Tiwari, Kunal;Hariharan, K.;Rameesha, T.V.;Krishnankutty, P.
    • Ocean Systems Engineering
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    • 제10권3호
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    • pp.333-357
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    • 2020
  • International Maritime Organisation (IMO) regulations insist on reduced emission of CO2, noxious and other environmentally dangerous gases from ship, which are usually let out while burning fossil fuel for running its propulsive machinery. Contrallability of ship during sailing has a direct implication on its course keeping and changing ability, and tries to have an optimised routing. Bad coursekeeping ability of a ship may lead to frequent use of rudder and resulting changes in the ship's drift angle. Consequently, it increases vessels resistance and also may lead to longer path for its journey due to zigzag movements. These adverse effects on the ship journey obviously lead to the increase in fuel consumption and higher emission. Hence, IMO has made it mandatory to evaluate the manoeuvring qualities of a ship at the designed stage itself. In this paper a numerical horizontal planar motion mechanism is simulated in CFD environment and from the force history, the hydrodynamic derivatives appearing in the manoeuvring equation of motion of a ship are estimated. These derivatives along with propeller thrust and rudder effects are used to simulate different standard manoeuvres of the vessel and check its parameters against the IMO requirements. The present study also simulates these manoeuvres by using numerical free running model for the same ship. The results obtained from both these studies are presented and discussed here.

풍력 발전기 블레이드에 걸친 3차원 유동장 해석 및 팁 형상 설계 (3-DIMENSIONAL FLOW FIELD ANALYSIS AND TIP SHAPE DESIGN IN A WIND TURBINE BLADE)

  • 정재호;유철;이정상;김기현;최재웅
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2011년 춘계학술대회논문집
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    • pp.243-248
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    • 2011
  • The 3-dimensional flow field has been investigated by numerical analysis in a 2.5MW wind turbine blade. Complicated and separated flaw phenomena in the wind turbine blade were captured by the Reynolds-averaged Navier-Stokes(RANS) steady flaw simulation using general-purpose code, CFX and the mechanism of vortex structure behavior is elucidated. The vortical flow field in a wind turbine rotor is dominated by the tip vortex and hub separation vortex. The tip vortex starts to be formed near the blade tip leading edge. As the tip vortex develops in the tangential direction, interacting with boundary layer from the blade tip trailing edge. The hub separation vortex is generated near the blade hub leading edge and develops nearly in the span-wise direction. Furthermore, 3-dimensional blade tip shape has been designed for increasing shrift power and reducing thrust force on the wind turbine blade. It is expected that the behavior of the tip vortex and hub separation vortex plays a major role in aerodynamic and aeroacoustic characteristics.

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부하추종형 고효율 지열히트펌프 시스템에 관한 연구 (1) (A Study on the High Efficiency Ground Source Heat Pump System (1))

  • 고득용;김욱중;최상규;장기창
    • 신재생에너지
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    • 제1권4호
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    • pp.30-37
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    • 2005
  • Cycle simulation of Ground Source Heat Pump[GSHP] system was carried out to determine the design specification of basic components such as turbo compressor and heat exchangers. Part load operation characteristics of the designed GSHP system was estimated using the compressor and heat exchanger performance data. A 50RT class turbo compressor for GSHP system is now under development, in which R134a refrigerant is adopted as working fluid. The compressor with variable cascade diffusers is designed to work both in cooling and heating modes so that it can actively keep up with the climate change with high efficiency. The normal running speeds of the compressor are 59000rpm for heating mode and 70000rpm for tooling mode respectively. It has two identical impellers at both ends of the rotor so as to minimize aero-induced thrust force effectively. GSHP system was coupled with a vortical type heat exchanger, and heat gain and heat loss from ground were evaluated per a bore hole. For the optimal integration of the heat pump system, its header for circulating fluid was combined with the ground heat exchangers in parallel and series configuration.

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세포 운동 가시화를 통한 상처 치유 과정 내 경계 이동의 규명 (Identification of boundary migration during the wound healing through the visualization of cell migrations)

  • 정현태;이재성;신현정
    • 한국가시화정보학회지
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    • 제18권2호
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    • pp.10-17
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    • 2020
  • The curvature of wound boundaries has been identified as a key modulator that determines a type of force responsible for cell migration. While several studies report how certain curvatures of the boundary correlate with the rate at which the wound closes, it remains unclear how these curvatures are spatiotemporally formed to regulate the healing process. We investigated the dynamic changes in the boundary curvatures by visualizing cell migration patterns. Locally, cells at the convex boundary continuously move forward with transmitting kinetic responses behind to the cells away from the boundary, and cells at the concave boundary exhibit dramatic contracting motion, like a purse-string, when they accumulate enough negative curvatures to gain the thrust toward the void. Globally, the dynamics of boundary geometries are controlled by the diffusive flow of cells driven by the density gradient between the wound area and the cell layer.

Coordinated Control of an Independent Multi-phase Permanent Magnet-type Transverse Flux Linear Machine Based on Magnetic Levitation

  • Hwang, Seon-Hwan;Kwon, Soon-Kurl;Hwang, Young-Gi;Bang, Deok-Je
    • 조명전기설비학회논문지
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    • 제28권12호
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    • pp.95-102
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    • 2014
  • This paper proposes a coordinated control for an independent multi-phase transverse flux linear synchronous motor (IM-TFLSM) based on magnetic levitation. The stator structures of the IM-TFLSM are composed of a two set, which has independent three-phase windings and a double-sided air-gap as opposed to the conventional Y-connected three-phase linear motors. A suitable control algorithm is necessary to operate the applied linear machine. This study proposes a coordinated control algorithm for adjusting the mover air-gap and thrust force of the IM-TFLSM in order to maintain air-gap and phase shifted current control of the independent 3-phase modules. In addition, the principle of operation and its special structures are described in detail and the validity and effectiveness of the control algorithm is verified through multiple experimental results.

Determination of effective parameters on surface settlement during shield TBM

  • Kim, Dongku;Pham, Khanh;Park, Sangyeong;Oh, Ju-Young;Choi, Hangseok
    • Geomechanics and Engineering
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    • 제21권2호
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    • pp.153-164
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    • 2020
  • Tunnel excavation in shallow soft ground conditions of urban areas experiences inevitable surface settlements that threaten the stability of nearby infrastructures. Surface settlements during shield TBM tunneling are related to a number of factors including geotechnical conditions, tunnel geometry and excavation methods. In this paper, a database collected from a construction section of Hong Kong subway was used to analyze the correlation of settlement-inducing factors and surface settlements monitored at different locations of a transverse trough. The Pearson correlation analysis result revealed a correlation between the factors in consideration. Factors such as the face pressure, advance speed, thrust force, cutter torque, twin tunnel distance and ground water level presented a modest correlation with the surface settlement, while no significant trends between the other factors and the surface settlements were observed. It can be concluded that an integrated effect of the settlement-inducing factors should be related to the magnitude of surface settlements.

헬리콥터 능동 진동/소음 제어 기법 해외 동향 및 사례 (Technology Trend of Vibration/Noise Active Control in Helicopter)

  • 김덕관;윤철용;정기훈;김승호
    • 항공우주산업기술동향
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    • 제9권1호
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    • pp.77-89
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    • 2011
  • 헬리콥터는회전하는구동시스템에의해추력및비행제어력을발생하기때문에회전체에서기체로전달되는 진동 및 소음을 줄이는 것이 아주 중요하다. 과거에는 수동적 방법으로 특정주파수에 해당하는 진동 및 소음을 줄였지만, 기술이 발달함에 따라 주파수를 변동시킬 수 있는 장치를 적용할 수 있는 능동적 진동 및 소음 제어방법이 개발되었다. 본 논문에서는 이러한 헬리콥터 진동 및 소음을 제어하는 능동적 방법에 대한 세계적인 기술동향 및 사례를 기술하였다. 서론에서는 헬리콥터 진동 및 소음을 제어하는 일반적인 방법론을 소개하고, 본론에서는 능동적으로 제어하는 사례 및 동향을 중심으로 기술하였다. 현재 가장 활발하게 진행되고 있는 능동적 플랩구동장치 및 비틀림장치 등을 중심으로 소개하였다.

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초공동 운동체 구조물의 동적 불안정성 연구 (The Study of Dynamic Instability of Supercavitating Shell Structures)

  • 김승조;변완일;장채규;조진연
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2010년도 제34회 춘계학술대회논문집
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    • pp.469-471
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    • 2010
  • 초공동 수중 운동체의 구조물은 수중 운동 시에 유동 마찰에 의해 생성되는 높은 축 방향 하중과 추력의 조합에 의해 좌굴 현상이 발생하게 되며, 이는 구조물의 손상과 연결된다. 따라서 운용하고자 하는 수동 운동체의 속도 범위에서 이러한 좌굴이 발생되지 않도록 구조 설계가 요구되며, 이는 유한요소 해석을 이용한 정적 및 동적 좌굴 해석으로 좌굴 예측이 가능하다. 본 연구에서는 이러한 좌굴 해석을 위한 기초적인 소개와 유한요소 좌굴 해석에 필요한 고유치 해법을 소개하고, 좌굴 해석에 앞서 고유치 해법을 통한 고유 진동수 및 모드 형상을 DIAMOND/IPSAP 프로그램을 통해 예측하여 보았다.

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공심 코일형 리니어 DC 모터의 설계 및 동특성 해석 (Design and Dynamic Analysis of Air-core Coil type Linear DC Motor)

  • 강규홍;홍정표;김규탁;하근수;정중기;임태빈
    • 대한전기학회논문지:전기기기및에너지변환시스템부문B
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    • 제49권3호
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    • pp.165-171
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    • 2000
  • This paper proposes a technique to design of air-core type Linear DC Motor(LDM) by using Equivalent Magnetizing Current(EMC) method and has performed its dynamic analysis. The magnetic flux density differ in accordance with airgap position due to difference of mechanical and magnetic air gap length and the coil shape has an influence on the thrust. Therefore, the analysis of magnetic field due to the magnets is carried out by EMC. The phenomena according to the various coil various coil shape under the same Magneto Motive Force(MMF) has been analyzed and its result is applied to the design process. The appropriateness of the proposed technique is confirmed by Finite Element Method(FEM) and its dynamic analysis is carried out from the coupling of the electrical circuit equation and mechanical kinetic equation.

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횡자속 선형전동기의 추력특성에 따른 선형액추에이터의 동특성 (Dynamic response of linear actuator with the thrust force of transverse flux linear motor)

  • 우병철;홍도관;강도현;장정환;김종무
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2005년도 제36회 하계학술대회 논문집 B
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    • pp.1192-1194
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    • 2005
  • 선형전동기는 일반적으로 회전형 전동기를 잘라 평면에 펼친 다음 회전형 전동기와 같이 구동할 경우 직선운동을 하는 전동기이다. 회전형 전동기에 비해서 효율특성을 다소 떨어지지만 직선운동을 위한 전동기가 필요할 경우에는 많이 사용하고 있는 실정이며 회전형의 경우 고정자와 회전자의 극간격을 유지하기 위해서 축을 중심으로 구동할 수 있게 제작하고 있는 실정이다. 그러나 선형전동기의 경우 정확한 극간경의 유지를 위해서 LM guide를 사용하는 것이 일반적이며 이로 인해서 고정자회 이동자 사이의 정확한 간격을 유지할 수 있게 된다. 또한 자속의 흐름과 이동자의 이동방향에 따라 일반적으로 선형전동기를 구분하는데 자속의 흐름으로 인해 만들어지는 평면과 이동자가 움직이는 방향이 같은 면 상에 있으면 종자속이라고 하고 횡방향으로 놓여질 경우 횡자속 선형전동기라고 부른다. 본 연구에서는 횡자속 선형전동기에서 발생되는 추력특성을 고려하여 선형액추에이터를 설계할 경우 발생되는 추력읜 불균일성에 대한 내용으로 전동기의 추력 특성 파형에 따른 성형 액추에이터의 동특성을 알아보았다. 특히 액추에이터에서 발생되는 공진특성을 기준으로 불때 같은 에너지로 약 2배의 동특성을 얻을 수 있었고 반력은 거의 같은 특성을 얻을 수 있었다.

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