• 제목/요약/키워드: Air Nozzle System

검색결과 308건 처리시간 0.03초

Carbon Contained Ammonium Diuranate Gel Particles Preparation in Mid-process of High-temperature Gas-cooled Reactor Fuel Fabrication

  • Jeong, Kyung Chai;Cho, Moon Sung
    • Nuclear Engineering and Technology
    • /
    • 제48권1호
    • /
    • pp.175-181
    • /
    • 2016
  • This study investigates the dispersibility of carbon in carbon contained ammonium diuranate (C-ADU) gel particles and the characteristics of C-ADU gel liquid droplets produced by the vibrating nozzle and integrated aging-washing-drying equipment. It was noted that the excellent stability of carbon dispersion was only observed in the C-ADU gel particle that contained carbon black named CB 10. ADU gel liquid droplets containing carbon particles with the excellent sphericity of approximately 1,950 mm were then obtained using an 80-100-Hz vibrating nozzle system. Dried C-ADU gel particles obtained by the aging-washing-drying equipment were thermal decomposed until $500^{\circ}C$ at a rate of $1^{\circ}C/min$ in an air or in 4% $H_2$ gas atmosphere. The thermally decomposed C-ADU gel particles showed 24% weight loss and a more complicated profile than that of ADU gel particles.

고점성 유체 내부에서의 다상유동장 가시화 및 PIV 측정 (Flow Visualization and PIV Measurement of Multiphase Flow in Highty Viscous Liquid)

  • 김현동;류승규;김경천
    • 한국가시화정보학회:학술대회논문집
    • /
    • 한국가시화정보학회 2006년도 추계학술대회 논문집
    • /
    • pp.48-54
    • /
    • 2006
  • A visualization study of flow characteristics in a mixer using multi-nozzle bubbling was performed. The mixer is filled with liquid glycerin (dynamic viscosity = $1000mPa{\cdot}$ s at $25^{\circ}C$) and convective mixing is induced by air bubbles generated from 9 orifices installed on the bottom of the mixer. To visualize the flow field, PIV (Particle Image Velocimetry) system consisting of 532nm Nd:YAG laser, $2k\times2k$ CCD camera and synchronizer is adopted. The bubbles generated with uniform size and frequency form bubble stream, and bubble streams rise vertically without interaction between bubble streams. Mixing efficiency is affected by the height of bubbler and the effective height of bubbler is 20mm from the bottom of the mixer.

  • PDF

역선회 이류체 미립화기의 선회각 변화에 따른 미립화 특성연구 (Study on the Atomization Characteristics of a Counter-swirling Two-phase Atomizer with Variations of Swirl angle)

  • 김남훈;이삼구;하만호;노병준;강신재
    • 대한기계학회:학술대회논문집
    • /
    • 대한기계학회 2001년도 춘계학술대회논문집E
    • /
    • pp.125-130
    • /
    • 2001
  • Experimental and analytical researches have been conducted on the twin-fluid atomizers for better droplet breakup during the past decades. But, the studies on the disintegration mechanism still present a great challenge to understand the drop behavior and breakup structure. In an effort to describe the aerodynamic behavior of the sprays issuing from the internal mixing counter-swirling nozzle, the spatial distribution of axial (U) radial (V) and tangential (W) components of droplet velocities are investigated across the radial distance at several axial locations of Z=30, 50, 80, 120 and 170mm, respectively. Experiments were conducted for the liquid flow rates which was kept constant at 7.95 g/s and the air injection pressures were varied from 20 kPa to 140 kPa. Counter-swirling internal mixing nozzles manufactured at angles of $15^{\circ},\;30^{\circ},\;45^{\circ}$ and $60^{\circ}$ the central axis with axi-symmetric tangential-drilled holes was considered. The distributions of velocities and turbulence intensities are comparatively analyzed. PDPA is installed to specify spray flows, which have been conducted along the axial downstream distance from the nozzle exit. Ten thousand of sampling data was collected at each point with time limits of 30 second. 3-D automatic traversing system is used to control the exact measurement. It is observed that the sprays with all swirl angle have the maximum SMD for on air injection pressure of 20 kPa and 140 kPa with centerline, respectively. The nozzle with swirl angle of $60^{\circ}$ has vest performance.

  • PDF

항공기 후방동체 열유동장 및 IR 신호 예측 시스템 (Computation of Flowfield and Infrared Signature in Aircraft Exhaust System for IR Reduction Design)

  • 문혁;양영록;전수환;최성만;명노신;조태환
    • 한국항공우주학회지
    • /
    • 제39권7호
    • /
    • pp.652-659
    • /
    • 2011
  • 항공기 IR(Infrared; 적외선) 피탐지성 감소 연구를 위해 후방동체 주위 열유동장과 IR 신호를 예측하는 시스템을 구축하였다. 아음속 무인전투기(UCAV)를 대상 항공기로 고려하여 가상 임무 설정 및 성능해석을 통해 가상 엔진을 선정하였다. 또한 각 임무를 만족시키는 노즐을 설계한 후, 고속 고온 열유동장 CFD 해석코드를 이용하여 최대 출력에서의 노즐 내부 유동을 해석하였다. 예측된 노즐 표면 및 후방 동체의 온도는 고체표면 복사 열교환 및 신호 예측코드와 연계시키는 시스템과 연동시켜 최종적으로 IR 신호를 계산하였다. IR 밴드 및 관찰 각도에 대한 IR 신호의 변화를 분석하여 IR 감소설계를 위한 정성적 정보를 도출하였다.

OWC 파력발전장치의 공기실 성능예측에 대한 수치적인 연구 (Numerical Prediction of Chamber Performance for OWC Wave Energy Converter)

  • 김길원;현범수;류진;홍기용
    • 한국해양환경ㆍ에너지학회지
    • /
    • 제13권2호
    • /
    • pp.91-98
    • /
    • 2010
  • 진동수주형 파력발전장치에서 공기실 내의 수면 변화와 덕트 내 유량의 왕복유동은 시스템의 작동 성능을 결정짓는 매우 중요한 요소이다. 공기실 내의 수면 변화를 고찰하기 위하여 상용 CFD 코드인 Fluent 6.2를 이용하여 구현한 수치조파수조를 사용하였다. 수치조파수조의 지배방정식은 연속방정식과 Reynolds 평균 N-S 방정식이고 자유수면은 Two-phase VOF 기법을 이용하여 추적하였다. 공기실 내의 수면 변화와 공기실 윗부분에 설치된 덕트 내의 왕복유량을 계산하여 고찰하였고, 계산의 정확도를 검증하기 위하여 실험결과와 비교 분석을 수행하였다. 또한 동일한 입사파 조건에서 공기실 - 덕트 시스템의 노즐 비율이 시스템이 미치는 영향을 고찰하여 분석을 하였다.

초음속 유도무기 지상 시험용 가열기 개념 설계 (Concept Design on Heating System for Supersonic Air-Breathing Engine Test Facility)

  • 한풍규;남궁혁준;이경훈;김영수
    • 한국추진공학회:학술대회논문집
    • /
    • 한국추진공학회 2006년도 제26회 춘계학술대회논문집
    • /
    • pp.321-326
    • /
    • 2006
  • 초음속 유도무기에 사용되고 있는 공기흡입 추진기관의 지상 연소시험에서 요구되는 700K-6바의 공기를 공급하기 위한 Vitiated형 공기 가열기에 대한 개념설계를 수행하였다. 본 가열기는 여분의 기체 산소와 공기를 혼합하는 예혼합기, 예혼합 기체와 연료를 혼합시키는 혼합기, 점화기를 포함하는 연소실과 수축팽창 노즐, 그리고 디퓨저로 구성하였다. 가열기에 사용된 연료는 천연가스이며, 유동해석을 통해 가열기의 각 구성요소의 성능을 파악하였으며, 점화 후 화염유지가 이루지는 것을 해석적으로 확인하였다.

  • PDF

충돌분류시스템의 열전달 특성에 관한 수치적 연구 (Numerical Study on Heat Transfer Characteristics in Impinging Air Jet System)

  • 금성민;김동춘
    • 한국태양에너지학회 논문집
    • /
    • 제23권4호
    • /
    • pp.55-61
    • /
    • 2003
  • Heat transfer characteristics for an air jet vertically impinging on a flat plate with a set of hybrid rods was investigated numerically using the RNG k-$\varepsilon$turbulent model. A commercial finite-volume code FLUENT is used. The rods had cross sections of half circular and rectangular shapes. The heating surface was heated with a constant heat flux value of $1020W/m^2$. Parameters investigated were the jet Reynolds number, nozzle -to-plate spacing, the rod pitch and rod-to-plate clearance. The local and average Nusselt number were found to be dependent on the rod pitch and the clearance because installing rods disturbed the flow. Higher convective heat transfer rate occurred in the whole plate as well as in the wall jet region.

충돌공기제트시스템에서 직삼각형로드에 의한 열전달특성 (Heat Transfer Characteristics by the Right Angled Triangle Rod Array in Impinging Air Jet System)

  • 금성민
    • 한국분무공학회지
    • /
    • 제13권1호
    • /
    • pp.9-15
    • /
    • 2008
  • This experimental study was carried out to examine the heat transfer characteristics of impinging air jet on a flat plate with a set of right angled triangle rods. Each right angled triangle rod in the array was positioned normal to the flow direction and parallel to the flat plate surface. The clearances from a right angled triangle rod to flat plate surface (C=1, 2 and 4 mm) and the distance from nozzle exit to flat plate (H=100 and 500 mm) were changed for the pitch between each right angled triangle rods (P=40 mm). As a result, heat transfer shows best performance at the clearance of C=1 mm, in case clearance changed, and the average heat transfer enhancement rate increased up to 47% compared to the result of a flat plate without a right angled triangle rod.

  • PDF

충돌분류계에서 사다리형 로드를 이용한 열전달증진에 관한 연구 (A Study on the Heat Transfer Enhancement by Trapezoid Rod in Impinging Jet System)

  • 임태수;금성민;이창언
    • 대한기계학회:학술대회논문집
    • /
    • 대한기계학회 2001년도 춘계학술대회논문집D
    • /
    • pp.565-571
    • /
    • 2001
  • The objective of this study was to investigate the characteristics of air flow and heat transfer caused by trapezoid rods array in impinging air jet system. In this study, trapezoid rods have been set up on front of flat plate to act as a turbulence promoter. Local Nusselt numbers were determined as a function of three parameters: (a) the space from rods to heating surface(C=1, 2, 4mm), (b) the pitch between each rods(P=30, 40, 50mm), (c) the distance from nozzle exit to flat plate(H/B=2, 6, 10). And this research compared the above with the experiment without trapezoid rods. As a result, heat transfer performance was best under the condition of C=1mm and as the pitch is 30mm. In this case, maximum rate of heat transfer augmentation is about 1.9 times greater compared to that without trapezoid rods.

  • PDF

충돌 부탄 화염의 분석을 위한 복합 광학 계측 기법 개발 (Development of Combined Optical System for Analysis of Impinging Butane Flame)

  • 백승환;안성수;고한서
    • 한국가시화정보학회:학술대회논문집
    • /
    • 한국가시화정보학회 2005년도 추계학술대회 논문집
    • /
    • pp.69-73
    • /
    • 2005
  • Three-dimensional density distributions of an impinging and eccentric flame have been analyzed numerically and experimentally by a combined optical system with a digital speckle tomography. The flame has been ignited by premixed butane/air from air holes and impinged vertically against a plate located at the upper side of tile burner nozzle. In order to compare with experimental data, computer synthesized phantoms of impinging and eccentric flames have been made and reconstructed by a developed three-dimensional multiplicative algebraic reconstruction technique (MART). A new scanning technique has been developed for the analysis of speckle displacements to investigate wall jet regions of the impinging flame including sharp variation of the flow direction and pressure gradient. The reconstructed temperatures have been compared with a temperature photography by an infrared camera and results of numerical analysis using a finite-element method.

  • PDF