• Title/Summary/Keyword: nozzle path

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A Monte Carlo Simulation Study of a Therapeutic Proton Beam Delivery System Using the Geant4 Code (Geant4 몬테카를로 코드를 이용한 양성자 치료기 노즐의 전산모사)

  • Shin, Jungwook;Shim, Hyunha;Kwak, Jungwon;Kim, Dongwook;Park, Sungyong;Cho, Kwan Ho;Lee, Se Byeong
    • Progress in Medical Physics
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    • v.18 no.4
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    • pp.226-232
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    • 2007
  • We studied a Monte Carlo simulation of the proton beam delivery system at the National Cancer Center (NCC) using the Geant4 Monte Carlo toolkit and tested its feasibility as a dose verification framework. The Monte Carlo technique for dose calculation methodology has been recognized as the most accurate way for understanding the dose distribution in given materials. In order to take advantage of this methodology for application to external-beam radiotherapy, a precise modeling of the nozzle elements along with the beam delivery path and correct initial beam characteristics are mandatory. Among three different treatment modes, double/single-scattering, uniform scanning and pencil beam scanning, we have modeled and simulated the double-scattering mode for the nozzle elements, including all components and varying the time and space with the Geant4.8.2 Monte Carlo code. We have obtained simulation data that showed an excellent correlation to the measured dose distributions at a specific treatment depth. We successfully set up the Monte Carlo simulation platform for the NCC proton therapy facility. It can be adapted to the precise dosimetry for therapeutic proton beam use at the NCC. Additional Monte Carlo work for the full proton beam energy range can be performed.

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Application of CFD Methods to Improve Performance of Denitrification Facility (탈질 설비의 성능 개선을 위한 CFD 기법 적용에 관한 연구)

  • Min-Kyu Kim;Hee-Taeg Chung
    • Clean Technology
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    • v.29 no.4
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    • pp.305-312
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    • 2023
  • Due to the strengthening of environmental requirements, aging denitrification facilities need to improve their performance. The present study aims to suggest the possibility of improving performance using computational analysis techniques. This involved modifying both the geometric design and the operating conditions, including the flow path shape of the equipment such as the inlet guide vane and the curved diffusing part, and the flow control of the ammonia injection nozzle. The conditions presented in this study were compared with existing operating conditions in terms of the flow uniformity, the NH3/NO molar ratio of the mixed gas flowing into the catalyst layer, and the total pressure drop of the facility. The flow field applied in the computational analysis ranged from the outlet of the economizer in the combustion furnace to the inlet of the air preheater, the full domain of the denitrification facility. The performances were derived by solving the flow fields using ANSYS-Fluent and the injection amount of ammonia was adjusted for each nozzle using Design Xplorer. Compared to the denitrification performances of the equipment currently in operation, the conditions proposed in this study showed an improvement in the flow uniformity and NH3/NO composition ratio by 45.1% and 8.7%, respectively, but the total pressure drop increased by 1.24%.

Experiemtnal Tests of Cryogenic Liuid Spill on a Plate (극저온 유체 유출현상에 관한 연구)

  • Ryu, Yong Hee;Hwang, Yun Ji;Lee, Yun Han;Kim, Kwang Seok;Lee, Jae Hun;Sim, Hee Jun
    • Plant Journal
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    • v.16 no.3
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    • pp.42-46
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    • 2020
  • In the large LNG process in FLNG or FSRU, sudden temperature drops of the steel in the event of LNG leaks may cause brittle fracture of the structure. In this paper, we investigate the principle and process of forming a cryogenic fluid on a steel plate through a cryogenic spillage experiment, and analyze the correlation of the temperature distribution of the steel plate according to the distance from the nozzle and exposure time. Two types of cryogenic fluids were used: LN2 and LNG. The cyogenic liquid was released on the steel plate at 1.6L/min for LN2 and 1.5L/min for LNG. For the steel, DH was used and the temperature was measured at 10 points in total. The Leidenfrost effect was observed on the steel plate, and the temperature distribution of the steel was varied according the flow path and the heat of evaporation of the fluid.

A Unified 3D Numerical Analysis of a Model Scramjet Engine with a Cavity Flame-Holder and Two Intake Side Walls (공동형 보염기를 갖는 모델 스크램제트 엔진의 흡입구 측면효과를 고려한 3차원 통합 유동해석)

  • Yeom, Hyo-Won;Kim, Sung-Jin;Sung, Hong-Gye;Kang, Sang-Hoon;Yang, Soo-Suk
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2009.11a
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    • pp.590-593
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    • 2009
  • To identify the detailed 3D flow characteristics of a model scramjet engine, a unified 3D numerical analysis was performed. The numerical domain of concern includes the entire flow path of the model scramjet engine extending from the intake to the nozzle exhaust. Turbulent models($k-{\omega}$ SST and low Reynolds number k-e with Sarkar model) were applied with comparison of experiment result. Intake side wall's effect on flow characteristics was analyzed in view points of flow quality at inlet duct and near the flame holder as well. The code is paralleled with multi-block feature using MPI(Massage Passing Interface) library to speed up the 3D calculation.

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Secondary Neutron Dose Measurement for Proton Line Scanning Therapy

  • Lee, Chaeyeong;Lee, Sangmin;Chung, Kwangzoo;Han, Youngyih;Chung, Yong Hyun;Kim, Jin Sung
    • Progress in Medical Physics
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    • v.27 no.3
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    • pp.162-168
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    • 2016
  • Proton therapy is increasingly being actively used in the treatment of cancer. In contrast to photons, protons have the potential advantage of delivering higher doses to the cancerous tissue and lower doses to the surrounding normal tissue. However, a range shifter is needed to degrade the beam energy in order to apply the pencil beam scanning technique to tumors located close to the minimum range. The secondary neutrons are produced in the beam path including within the patient's body as a result of nuclear interactions. Therefore, unintended side effects may possibly occur. The research related to the secondary neutrons generated during proton therapy has been presented in a variety of studies worldwide, since 2007. In this study, we measured the magnitude of the secondary neutron dose depending on the location of the detector and the use of a range shifter at the beam nozzle of the proton scanning mode, which was recently installed. In addition, the production of secondary neutrons was measured and estimated as a function of the distance between the isocenter and detector. The neutron dose was measured using WENDI-II (Wide Energy Neutron Detection Instruments) and a Plastic Water phantom; a Zebra dosimeter and 4-cm-thick range shifter were also employed as a phantom. In conclusion, we need to consider the secondary neutron dose at proton scanning facilities to employ the range shifter reasonably and effectively.

A Study on Steady-State and Transient Simulation of Turboprop Engine Using SIMULINK® Model (SIMULINK® Model를 이용한 터보프롭엔진의 정상상태 및 천이모사 연구)

  • Gong, Chang Deok;Im, Gang Taek
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.31 no.5
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    • pp.100-109
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    • 2003
  • A performacne simulation model of the PT6A-62 turboprop engine using the $SIMULINK^R$ was proposed to predict transient and steady state behaviors. The $SIMULINK^R$ has several advantages such as user-friendliness due to the GUI(Graphic User Interfaces) and ease in the modification of the computer program. The $SIMULINK^R$ model consists of subsystems to represent engine gas path components such as flight initial subsystem, compressor subsystem, burner subsystem, compressor turbine subsystem, power turbine, exhaust nozzle subsystem and integrator subsystem. In addition to subsystems, there are search subsystems to find an appropriate operating point by scaling from the 2-D components look-up table, Gasprop Subsystem to calculate the gas property precisely. In case of steady state validation, performance results analyzed by the proposed $SIMULINK^R$ model were agreed well with the analysis results by the commercial GASTURB program. Moreover in validation of the transient model, it was found that performance simulation results by the proposed model were reasonable agreement with analysis results by the well-proved computer program using FORTRAN.

Quality Evaluation of the 1st Stage Scraped and Casted Buckets of 1,100℃ Gas Turbine Blade (1,100℃급 가스터빈 1단 버켓 사용품 및 주조품 품질평가)

  • Chang, Sung Yong;Kim, Doo Soo
    • KEPCO Journal on Electric Power and Energy
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    • v.5 no.2
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    • pp.93-101
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    • 2019
  • The mechanical properties and microstructure of 1st stage used and casted buckets of $1,100^{\circ}C$ class gas turbine were analyzed to evaluate quality of the components. Gas turbine 1st stage buckets are exposed and operated in the most severe environment except 1st nozzle among the hot path gas components. Additionally, since the 1st stage bucket is a rotating component, so it may cause additional damage to the rear buckets and nozzles which cause a huge financial loss. Therefore, the quality of the casted bucket must be evaluated prior to use at the plant site. In this study, the microstructure analysis and mechanical properties of the casted bucket were evaluated to verify the casting quality and it was confirmed that the quality conditions designed by KEPCO were satisfied. A bucket operated 46% (11,067EOH) of its life time also evaluated for quality comparison.

Acoustic Modeling in a Gas Turbine Combustor with Backflow Using a Network Aproach (역류형 가스터빈 연소기에서 네트워크 접근법을 이용한 음향장 모델링)

  • Son, Juchan;Hong, Sumin;Hwang, Jeongjae;Kim, Min Kuk;Kim, Daesik
    • Journal of the Korean Society of Propulsion Engineers
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    • v.25 no.5
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    • pp.18-26
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    • 2021
  • In this work, we have developed a 1D network model aimed at predicting eigenvalues for resonance frequency analysis in a lab-scale industrial gas turbine single nozzle combustion system. Modern industrial gas turbines generally adopt combustors with very complex geometry and flow path to meet various design requirements simultaneously. The current study has developed a network model for combustion systems with backflow at the same axial location. The modeling results of resonance frequencies and mode distributions for a given system using the network model were validated from comparisons with prediction results using a 3D Helmholtz solver.

Two Spool Mixed-Flow Turbofan Engine Performance Analysis Modeling (2 스풀 혼합흐름 배기방식 터보팬 엔진 성능해석 모델링)

  • Seungheon Lee;Hyoung Jin Lee;Sangjo Kim;Gyujin Na;Jung Hoe Kim
    • Journal of the Korean Society of Propulsion Engineers
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    • v.27 no.1
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    • pp.37-48
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    • 2023
  • In this study, performance analysis modeling of two spool mixed flow type turbofan engine according to steady-state and transient is performed. The target engine is selected as F100-PW-229 from Pratt & Whitney, and main engine components including fan, high pressure compressors, combustion, high pressure turbines, low pressure turbines, mixer, convergent-divergent nozzle are modeled. The cooling effect of turbine through secondary flow path are considered in engine simulation model. We develop in-house Matlab/Simulink-based engine performance analysis program capable of analyzing internal engine state and compare it with GASTURB which is generally used as a commercial engine analysis program.

A numerical study on the aerodynamic characteristics of a variable geometry throttle valve(VGTV) system controlling air-flow rate (유량 제어장치인 가변스로틀밸브의 기하학적 형상변화에 따른 공기역학 특성분석 연구)

  • Cho, Hyun-Sung;Kim, Chul-Ho
    • Journal of Advanced Marine Engineering and Technology
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    • v.37 no.4
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    • pp.378-383
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    • 2013
  • A butterfly throttle valve has been used to control the brake power of an SI engine by controlling the mass flow-rate of intake air in the induction system. However, the valve has a serious effect on the volumetric efficiency of the engine due to the pressure resistance in the induction system. In this study, a new intake air controlling valve named "Variable Geometry Throttle Valve(VGTV)" is proposed to minimize the pressure resistance in the intake system of an SI engine. The design concept of VGTV is on the application of a venturi nozzle in the air flow path. Instead of change of the butterfly valve angle in the airflow field, the throat width of the VGTV valve is varied with the operating condition of an SI engine. In this numerical study, CFD(computational fluid dynamics) simulation technique was incorporated to have an aerodynamics performance analysis of the two air flow controlling systems; butterfly valve and VGTV and compared the results to know which system has lower pressure resistance in the air intake system. From the result, it was found that VGTV has lower pressure resistance than the butterfly valve. Especially VGTV is effective on the low and medium load operating condition of an SI engine. The averaged pressure resistance of VGTV is about 49.0% lower than the value of the conventional butterfly throttle valve.