• Title/Summary/Keyword: Stagger

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Estimation Method of Single Stagger PRI and Future TOA for Active Cancellation (단일 스태거 PRI의 추정 및 능동 상쇄를 위한 예상 도착 시간 추정 기법)

  • Lim, Seongmok;Sim, Dongkyu;Lee, Chungyong
    • Journal of the Institute of Electronics and Information Engineers
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    • v.51 no.3
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    • pp.34-41
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    • 2014
  • Through applying hostile radar signals that use stagger PRI to PRI transform in real time, we can analyze stagger PRI and calculate the future TOA for active cancellation by using measured TOA and estimated PRI. We shows the effect of the errors that are contained in PRI and measured TOA. Then, it will suggest the technique to improve the accuracy of estimated PRI and the TOA averaging method for reducing the effect of measured TOA error. Finally, we will show that accuracy of estimated future TOA that is calculated by proposed scheme is higher than that of future TOA that is simply calculated with TDOA and newest TOA through comparing RMSE performance.

NUMERICAL PREDICTION OF THE OPTIMAL STAGGER ANGLES FOR A HIGH-POWER TURBO BLOWER (고마력 터보 블로어의 최적 깃배치각에 관한 수치 예측)

  • Park, T.G.;Chung, H.T.;Park, J.Y.;Sung, B.I.
    • Journal of computational fluids engineering
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    • v.16 no.3
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    • pp.75-81
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    • 2011
  • The turbo blowers having large power capacity are generally composed of the variable inlet guide vane, the impeller and the variable diffuser. In the present study, the effect of the stagger angles on the aerodynamic performances has been investigated by CFD methods. The design specifications of the reference model having 400kW power were given as 7.43kg/s of mass flow rate, 1.66 of pressure ratio with 12000rpm of impeller rotating speed. As the first simulation parameter, the diffuser vane angle was varied in the range of ${\pm}$20 degree from the initial-design point. The inlet guide vane angles, as the second one, was changed in the range of ${\pm}$40 degree from the initial-design point. The commercial Navier-Stokes solver, ANSYS-CFX, was applied to solve the three-dimensional unsteady flow fields inside the turbo blower. Through the numerical results, the desirable setting angles were proposed to fit the best performance to the variation of the operating conditions.

Implementation of Optical-based Measuring Instrument for Contact Wire Geometry in Electric Railway (전기철도의 전차선로 형상검측을 위한 광학기반 검측 장치 구현)

  • Park, Young;Cho, Yong-Hyeon;Jung, Ho-Sung;Lee, Ki-Won;Kim, Hyung-Chul;Kwon, Sam-Young;Park, Hyun-June;Kim, Won-Ha
    • Journal of the Korean Institute of Electrical and Electronic Material Engineers
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    • v.21 no.9
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    • pp.868-871
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    • 2008
  • We propose an optical-based measuring instrument of catenary system in electric railway. This system was made to utilize line scan camera as inspecting system to measure the stagger and height of overhead contact wire in railway and composed with optical type source and FPGA-based image acquisition system with PCI slot. Vision acquisition software has been used for the application to programming interface for image acquisition, display, and storage with a frequency of sampling. To check the validity of our approach for the intended application, we monitored height and stagger in the overhead wire of a high-speed catenary system in Korea. The proposed optical-based measuring instrument to measure the contact wire geometry such as the hight and stagger shows promising on-field applications for online condition motoring. We expect that a new generation of real-time instruments with demanding various conditions motoring requirement in railway can be easily integrated into optical-based measuring instrument system.

Radar Signal Pattern Recognition Using PRI Status Matrix and Statistics (PRI 상태행렬과 통계값을 이용한 레이더 PRI 신호패턴 인식)

  • Lee, Chang-ho;Sung, Tae-kyung
    • Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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    • 2016.10a
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    • pp.775-778
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    • 2016
  • In this paper, we propose a new method to automatically recognize PRI modulation type of radar signal at ES(Electronic Support) in electronic singal environment. The propose method stores pattern of PRI(Pulse Repetition Interval) of radar signal and uses statistic data, which firstly classifies into 2 classes. Then the proposed method recognizes each PRI signal using statistic characteristic of PRI. We apply various 5 kinds of PRI signal such as constant PRI, jitter PRI, D&S(dwell & switch) PRI, stagger PRI, sliding PRI, etc. The result shows the proposed method correctly identifies various PRI signals.

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Development of an Image Processing Based Method for Dynamic Stagger Extraction of Pantograph-Overhead Contact Line System (영상처리를 통한 팬터그래프-전차선로 동편위 추출 기술 개발)

  • Cho, Chul-Jin;Cho, Yong-Hyeon;Kwon, Sam-Young;Lee, Ki-Won;Jang, Sa-Sool;Ryoo, Hyang-Bok
    • Proceedings of the KSR Conference
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    • 2011.05a
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    • pp.1336-1341
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    • 2011
  • The pantograph-overhead contact line system is an interface that supplies power to high-speed trains used in many countries including Korea. Due to the fact that power is supplied through direct contact between contact wires and contact strips, wear may occur, increasing the possibility of accidents over periods of time. Therefore, there is a need to establish methods of effectively extracting safety related parameters. In this paper, an image processing based method that calculates and draws graphs of a pantograph's dynamic stagger is proposed. To assess reliability, the results were compared with data collected from conventional maintenance vehicles.

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Compressor Performance with Variation of Diffuser Vane Angle (디퓨저 베인각의 변화에 따른 압축기 성능 특성)

  • Shin, Y. H.;Kim, K. H.;Bae, M. H,;Kim, J. H.
    • The KSFM Journal of Fluid Machinery
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    • v.3 no.2 s.7
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    • pp.36-43
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    • 2000
  • This study presents the centrifugal compressor performance for three different vane stagger angles and wall pressure distribution within vaned diffuser channels, and is also discussed about the stability with respect to the compressor components. As the vane stagger angle decreases, the flow rate for the stall onset decreases, and higher pressure can be obtained at the low flow rate region, however, the effective operation range of the compressor decreases because of the blockage effect of the diffuser vane. Low pressure pocket within the vaned diffuser channel moves from the pressure side of leading edge to the suction side as the flow rate decreases. The compressor system stability mainly depends on that of the diffuser.

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Practical Study on Optimal Design of Axial-flow Fan (축류팬의 실용적 최적 설계에 대한 연구)

  • Lee Yeonkyoung;Sah Jongyoub
    • 한국전산유체공학회:학술대회논문집
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    • 2000.05a
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    • pp.73-77
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    • 2000
  • Small-sized fans for cooling electronic components are usually produced by injection molding in unified form including blade and hub. However, in case of middle and large-sized fans, they deal ill various products with varied numbers of blade or stagger angles after designing a single blade by molding or aluminum die casting. At this occasion, it is necessary to study design method for high-performance axial fans can be operated with various numbers of blades or stagger angle using unique blade for specified conditions. Therefore, the goal in this study is developing a optimal design method which improves performance of axial fans within the large range of operating by single blade.

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A Study on Trailing Edge Noise from a Blade Cascade in a Uniform Flow (케스케이드 날개 후단소음 특성에 관한 연구)

  • Son, J.M.;Kim, H.J.;Lee, S.;Jo, Seong-Min
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2002.11b
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    • pp.652-657
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    • 2002
  • It is addressed that the turbulent broadband sound power from a sirocco fan can be modeled by the trailing edge noise. The trailing edge noise is usually influenced by inflow turbulence, separation and boundary layer on the blade. The design parameters such as solidity(c/s) and stagger angle are specified to predict performance and noise level because the separation and slip velocity are strongly affected by them along with the flow coefficient. This paper reports the effects of the stagger angle upon the trailing edge noise for various trailing edge shapes. It is believed that the serrated trailing edge provides break-up mechanism for organized convecting vortices, thereby reduce the overall noise level.

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Experimental Study of Trailing Edge Shape of Forward Curved Blade upon Radiated Noise (원심 전향익 송풍기 날개 후단의 형상에 따른 소음 분석)

  • KIM, H.-J.;JUNG, K.-H.;LEE, C.-J.;LEE, S.
    • 유체기계공업학회:학술대회논문집
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    • 2000.12a
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    • pp.137-142
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    • 2000
  • The turbulent broadband sound power from a forward curved bladed fan can be modeled by the trailing edge noise. The trailing edge noise is usually influenced by inflow turbulence, separation, and boundary layer on the blade. This paper reports the effects of the solidity (C/s) and the stagger angles upon the trailing edge noise with respect to the trailing edge shapes of circular-arc cambered blade of multi-bladed fan, and discusses the major physical mechanism of reduced noise lot the circular trailing-edged case.

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Parametric Design of Axial Fan for Air-Conditioning Unit in terms of Aerodynamic Performance and Noise Level (공조용 축류홴 설계 및 설계변수에 따른 성능과 소음비교)

  • Lee, Seung-Jin;Choi, Go-Bong;Cho, Hong-Jun;Song, Woo-Seog;Lee, Seung-Bae
    • The KSFM Journal of Fluid Machinery
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    • v.13 no.3
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    • pp.24-29
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    • 2010
  • Axial fans for an air-conditioning unit are designed to equip the system with an expected flow-rate and low noise level by applying the blade design method of multi-sectioning and local camber generation. In this study, the distributions of chord length, stagger angle, and camber angle are globally and locally determined for the given specific speed, which is considered to be relatively high. The mock-up fans are observed to satisfy the aerodynamic performance and the noise level for the system simultaneously and discussed in terms of local flow patterns related to the emitted noise.