• 제목/요약/키워드: Multi-Flow

검색결과 2,278건 처리시간 0.027초

천연가스 다노즐 열원설비의 연료 유동 안정화 (Stabilization of Fuel F1ow in a Multi-Nozzle Combustion System Burning Natural Gas)

  • 박의철;차동진
    • 설비공학논문집
    • /
    • 제13권12호
    • /
    • pp.1255-1265
    • /
    • 2001
  • A numerical study has been conducted to characterize the transient flow in a utility gas turbine burning natural gas. The solution domain encompasses the supply gas pressure regulator to the combustor of the gas turbine that employs multi-nozzle fuel injectors. Some results produced for verification in the present study agree suite well with the experimental ones. It is found that the total gas flow may decrease noticeably during its combustion mode change, which would be the reason of momentary combustion upset, when a reference case of opening ratios of control valves in the system is applied. Several parameters are then varied in order to make the total gas flow stable over that period of time. Results of this study may be useful to understand the unsteady behavior of combustion system burning natural gas.

  • PDF

Optical Flow Based Collision Avoidance of Multi-Rotor UAVs in Urban Environments

  • Yoo, Dong-Wan;Won, Dae-Yeon;Tahk, Min-Jea
    • International Journal of Aeronautical and Space Sciences
    • /
    • 제12권3호
    • /
    • pp.252-259
    • /
    • 2011
  • This paper is focused on dynamic modeling and control system design as well as vision based collision avoidance for multi-rotor unmanned aerial vehicles (UAVs). Multi-rotor UAVs are defined as rotary-winged UAVs with multiple rotors. These multi-rotor UAVs can be utilized in various military situations such as surveillance and reconnaissance. They can also be used for obtaining visual information from steep terrains or disaster sites. In this paper, a quad-rotor model is introduced as well as its control system, which is designed based on a proportional-integral-derivative controller and vision-based collision avoidance control system. Additionally, in order for a UAV to navigate safely in areas such as buildings and offices with a number of obstacles, there must be a collision avoidance algorithm installed in the UAV's hardware, which should include the detection of obstacles, avoidance maneuvering, etc. In this paper, the optical flow method, one of the vision-based collision avoidance techniques, is introduced, and multi-rotor UAV's collision avoidance simulations are described in various virtual environments in order to demonstrate its avoidance performance.

태양열 해수담수화 시스템을 위한 다중효용 담수기 개발 (Development of Multi Effect Distillation for Solar Thermal Seawater Desalination System)

  • 주홍진;황인선;곽희열
    • 한국태양에너지학회 논문집
    • /
    • 제31권1호
    • /
    • pp.1-7
    • /
    • 2011
  • This study was accomplished to evaluate the performance of Multi Effect Distillation(MED) for solar thermal desalination system. It was designed Multi effect distillation with $3m^3$/day capacity and Shell&Tube type heat exchanger. Also, The effective heat transfer of Shell&Tube heat exchanger was used Cu(90%)-Ni(10%) corrugated tube. The parameters relating to the performance of Multi Effect Distillation are known as hot water flow rate. The experimental conditions for each parameters were $18^{\circ}C$ for sea water inlet temperature, $6m^3$/hour sea water inlet volume flow rate, $75^{\circ}C$ for hot water inlet temperature, 2.4, 3.6, and $4.8\;m^3$/hour for hot water inlet volume flow rate, respectively. The results are as follows, Development for Multi effect distillation was required about 40kW heat and 35kW cooling source to produce $3m^3$/day of fresh water. Based on the results of this study, It makes possible to secure economics of desalination system with solar energy which is basically needed development of high efficiency fresh water generator.

다점 피토관을 이용한 기체 유량 측정의 불확도 평가 (Uncertainty Assessment of Gas Flow Measurement Using Multi-Point Pitot Tubes)

  • 양인영;이보화
    • 한국유체기계학회 논문집
    • /
    • 제19권2호
    • /
    • pp.5-10
    • /
    • 2016
  • Gas flow measurement in a closed duct was performed using multi-point Pitot tubes. Measurement uncertainty was assessed for this measurement method. The method was applied for the measurement of air flow into a gas turbine engine in an altitude engine test facility. 46 Pitot tubes, 15 total temperature Kiel probes and 9 static pressure tabs were installed in the engine inlet duct of inner diameter of 264 mm. Five tests were done in an airflow range of 2~10 kg/s. The flow was compressible and the Reynolds numbers were between 450,000 and 2,220,000. The measurement uncertainty was the highest as 6.1% for the lowest flow rate, and lowest as 0.8% for the highest flow rate. This is because the difference between the total and static pressures, which is also related to the flow velocity, becomes almost zero for low flow rate cases. It was found that this measurement method can be used only when the flow velocity is relatively high, e.g., 50 m/s. Static pressure was the most influencing parameter on the flow rate measurement uncertainty. Temperature measurement uncertainty was not very important. Measurement of boundary layer was found to be important for this type of flow rate measurement method. But measurement of flow non-uniformity was not very important provided that the non-uniformity has random behavior in the duct.

다수 빼기 사출성형에서 캐비티간 충전균형을 위한 새로운 런너의 설계 (A Novel Runner Design for Flow Balance of Cavities in Multi-Cavity Injection Molding)

  • 박서리;김지현;류민영
    • 폴리머
    • /
    • 제33권6호
    • /
    • pp.561-568
    • /
    • 2009
  • 소형 플라스틱 부품들은 대부분 다수 캐비티 빼기 사출금형에서 성형된다. 이러한 다수 빼기 캐비티 금형에서의 사출성형은 캐비티간의 흐름 균형이 중요하다. 캐비티간 흐름의 불균형은 성형품의 캐비티간 물성 및 품질의 편차를 초래한다. 캐비티간의 흐름균형은 런너와 게이트에서의 흐름균형을 통하여 이루어지게 되는데 런너와 게이트에서 기하학적인 균형을 이루어도 열적 불균형으로 캐비티간 흐름의 불균형을 초래한다. 본 연구에서는 캐비티간 흐름의 균형을 위해 고안한 스크류 타입의 런너을 이용하여 캐비티간 충전균형을 고찰하였다. 여러 형태의 스크류 런너에서 결정성 수지와 비결정성 수지, 그리고 점도가 높은 수지와 점도가 낮은 수지를 이용하여 캐비티간 흐름을 관찰하였다. 흐름의 균형은 성형조건 중 사출속도에 따라 다르게 나타나기 때문에 사출속도를 변화해 가며 관찰하였다. 실험 결과를 성형해석과 비교 검토하였으며 서로 잘 일치함을 확인할 수 있었다. 스크류 런너에서 수지가 흐르면서 스크류 채널을 따라 회전운동을 하여 스크류 단면에서 온도가 균일하게 됨을 확인하였다. 그리구 이러한 균일한 온도 때문에 캐비티간 흐름 균형이 이루어지고 있음을 확인하였다. 결론적으로 실험에 사용된 새롭게 고안된 스크류 타입의 런너는 캐비티간 충전균형을 이루는데 매우 효과적임을 실험과 해석을 통해 검증할 수 있었다.

Simultaneous Multi-Channel Sensor System for Gas Flow Measurementtion Measurement

  • Kim, Young-Han;Joung, Ok-Jin
    • 제어로봇시스템학회:학술대회논문집
    • /
    • 제어로봇시스템학회 2002년도 ICCAS
    • /
    • pp.95.3-95
    • /
    • 2002
  • A multi-channel electrostatic probe is utilized to determine gas flow rate in a cylindrical container. A numerical analysis is conducted to compare experimental measurement with the computed gas velocity in radial and axial directions.

  • PDF

다수 캐비티의 사출성형품에서 충전의 불균형과 성형품 치수 편차의 교찰 (Investigation of the Filling Unbalance and Dimensional Variations in Multi-Cavity Injection Molded Parts)

  • 강민아;류민영
    • 폴리머
    • /
    • 제32권6호
    • /
    • pp.501-508
    • /
    • 2008
  • 렌즈나 휴대폰 부품 같은 소형 플라스틱 부품들은 일반적으로 다수 캐비티 사출금형에서 성형된다. 이러한 다수 캐비티 금형에서의 사출성형은 캐비티간의 충전 불균형이 일어날 수 있다. 이러한 충전 불균형 현상은 제품의 치수 및 중량의 편차뿐 아니라 제품의 물리적 특성에도 영향을 미친다. 충전 불균형은 무엇보다도 기하학적으로 균형 잡히지 않은 delivery system의 설계에서 기인된다. 하지만 delivery system이 기하학적으로 균형 있게 설계가 되었다 하더라도 충전 불균형 현상은 여전히 발생된다. 이러한 현상은 런너 단면에서의 온도분포에 기인하며 사출성형 공정 중 사출속도에 크게 영향을 받는 것으로 본 연구에서 파악되었다. 즉 충전 불균형은 부적절한 사출 성형 공정에 의해 발생되며 성형 공정 조건 중 사출속도는 충전에 영향을 주는 매우 중요한 요소이다. 본 연구에서는 재료와 사출 속도에 따른 충전 불균형 현상을 실험과 CAE을 통하여 관찰하였다. 사출속도 변화에 따른 충전 불균형 때문에 시편의 치수 및 무게가 불균일함을 확인하였다.

원심다익송풍기 유동의 삼차원 Navier-Stakes 해석 (Three-Dimensional Navier-Stokes Analysis of the Flow through A Multiblade Centrifugal Fan)

  • 서성진;첸시;김광용;강신형
    • 유체기계공업학회:학술대회논문집
    • /
    • 유체기계공업학회 1998년도 유체기계 연구개발 발표회 논문집
    • /
    • pp.42-48
    • /
    • 1998
  • Numerical study is presented for the analysis of three-dimensional incompressible turbulent flows in multiblade centrifugal fan. Reynolds-averaged Navier-Stokes equations with standard k - $\epsilon$ turbulence model are transformed to non-orthogonal curvilinear coordinates, and are discretized with finite volume approximations. Linear Upwind Differencing Scheme(LUDS) is used to approximate the convection terms in the governing equations. SIMPLEC algorithm is used as a velocity-pressure correction procedure. The computational area is divided into three blocks; core, impeller and scroll, which are linked by multi-block method. The flow inside of the fan is regarded as steady flow, and mathematical formula established from the cascade theory and empirical coefficient are employed to simulate tile flow through the impeller. From comparisons between the computational results and the experimental data, the validity of the mathematical formula for the blade forces was examined and good results were obtained qualitatively. Hence, we can get the flow characteristics of multi-blade centrifugal fan and it will be a corner stone of the development of the multiblade centrifugal fan.

  • PDF

Hybrid Fuzzy PI-Control Scheme for Quasi Multi-Pulse Interline Power Flow Controllers Including the P-Q Decoupling Feature

  • Vural, Ahmet Mete;Bayindir, Kamil Cagatay
    • Journal of Power Electronics
    • /
    • 제12권5호
    • /
    • pp.787-799
    • /
    • 2012
  • Real and reactive power flows on a transmission line interact inherently. This situation degrades power flow controller performance when independent real and reactive power flow regulation is required. In this study, a quasi multi-pulse interline power flow controller (IPFC), consisting of eight six-pulse voltage source converters (VSC) switched at the fundamental frequency is proposed to control real and reactive power flows dynamically on a transmission line in response to a sequence of set-point changes formed by unit-step reference values. It is shown that the proposed hybrid fuzzy-PI commanded IPFC shows better decoupling performance than the parameter optimized PI controllers with analytically calculated feed-forward gains for decoupling. Comparative simulation studies are carried out on a 4-machine 4-bus test power system through a number of case studies. While only the fuzzy inference of the proposed control scheme has been modeled in MATLAB, the power system, converter power circuit, control and calculation blocks have been simulated in PSCAD/EMTDC by interfacing these two packages on-line.