• 제목/요약/키워드: ON-OFF jet

검색결과 143건 처리시간 0.021초

연료의 열분해특성과 비예혼합 제트화염의 부상특성에 관한 기초실험 (Basic Experimental Study on Characteristics of Fuel Pyrolysis and Lift-off of Non-premixed Jet-flame)

  • 전민규;이민정;김남일
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2014년도 제49회 KOSCO SYMPOSIUM 초록집
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    • pp.119-121
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    • 2014
  • In general, high temperature combustion technique has been adopted as an efficient one. However, hydrocarbon-based fuel can be decomposed under high temperature, and it can affect the stabilization mechanism of edge flame. In this research, basic experimental study was conducted to identify the effect of fuel pyrolysis on the lift-off flame stabilization by changing the temperature of the plug flow reactor. Schmidt number of the gas fuel can be changed with temperature variation due to the fuel pyrolysis. Eventually, this study will help to establish and clarify the stabilization mechanism of lift-off edge flame.

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직기에 있어서 Computer의 응용 (A study on the application of computer used in a loom)

  • 조백희;김광영;김종수;이태세
    • 한국기계연구소 소보
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    • 통권19호
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    • pp.171-180
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    • 1989
  • The automation of textile machinery in the fabric manufacture is strongly demanded in order to improve the industrial structure related to labour-force and cost curtailment, in addition, to keep step with the various and small production system and the consumption tendency requesting a high quality fabrics. In this thesis, the technology applying the computer to an air jet loom and characteristics obtained from it are derived. To efficently apply an automized and unmanned textile machinery, an air jet loom is equipped with the let-off, take-up and weft insertion device attached a central processing unit(CPU) which can automatically operate according to a program. As a result, an air jet loom is available for the factory automation, which has advantages including productivity promotion, high quality security, energy savings, specification & variety, efficient production control, in fabric manufacturing process.

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Fabrication of TFTs by using Ink-Jet Printing Process with Poly(4-vinylphenol) Bank layer and TIPS-Pentacene Semiconductor

  • Kim, Se-Min;Kim, Min-Jung;Park, Jong-S.;Song, Chung-Kun
    • 한국정보디스플레이학회:학술대회논문집
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    • 한국정보디스플레이학회 2009년도 9th International Meeting on Information Display
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    • pp.937-939
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    • 2009
  • In this paper, we report electrical properties of OTFTs made by ink-jet printing with polyvinylphenol (PVP) for bank layer and bis(triisopropylsilylenthynyl) pentacene (TIPS-pentacene) for semiconductor. We could achieve better crystallization and surface uniformity of TIPS pentacene by employing PVP bank layer. The OTFT with PVP bank layer exhibited an field-effect mobility of 0.18 $cm^2$/Vs, current on/off ratio of $2.09{\times}10^5$, and subthreshold slope of 0.42 V/decane.

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마이크로 마스크를 가진 미세입자분사가공을 위한 가공경로의 생성 (Tool Path Generation for Micro-Abrasive Jet Machining Process with Micro-Mask)

  • 김호찬;이인환;고태조
    • 한국기계가공학회지
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    • 제10권6호
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    • pp.95-101
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    • 2011
  • Micro-abrasive jet machining(${\mu}AJM$) using mask is a fine machining technology which can carve a figure on a material. The mask should have holes exactly same as the required figure. Abrasive particles are jetted into the holes of the mask and it collide with the material. The collision break off small portion of the material. And the ${\mu}AJM$ nozzle should move all over the machining area. However, in general the carving shape is modeled as in a bitmap figure, because it often contains characters. And the mask model is also often modeled from the bitmap image. Therefore, the machining path of the ${\mu}AJM$ also efficient if it can be generated from the bitmap image. This paper suggest an algorithm which can generate ${\mu}AJM$ tool path directly from the bitmap image of the carving figure. And shows some test results and applications.

Structural Analysis of Lift-Fan Rotor for Jet-VTOL Aircraft

  • Hojo, Masahiro;Ogawa, Akinori;Saito, Yoshio;Hashimoto, Ryosaku
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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    • pp.521-523
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    • 2004
  • The Japan Aerospace Exploration Agency (JAXA) has proposed new vertical take-off and landing (VTOL) aircraft known as the Jet-VTOL aircraft shown in Fig.1. The Jet-VTOL aircraft is based on a canard wing configuration. The aircraft has the clustered lift-fans mounted near the center of gravity for vertical flight, and has the clustered fans mounted beside the vertical tail for cruise flight. Both fans are driven by the core engine mounted inside the aft end of fuselage. The propulsion system is innovative and attractive not to be seen even in the world.

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공동현상 이론을 고압분사주입공법에 적용하기 위한 실험적 연구 (Experimental Study on Enhanced Jet Grouting by Cavitation Theory)

  • 이상익;김창종;오세헌;김영욱
    • 한국지반공학회논문집
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    • 제21권1호
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    • pp.43-50
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    • 2005
  • 고압분사주입공법은 지반개량, 차수벽, 흙막이벽, 기초 보강말뚝 등에 사용되고 있다. 고압분사주입공법은 사질토지반에 대해서는 지수목적으로, 연약한 점성토 지반에서는 지반강화를 위하여 사용되고 있다. 그러나 현재 국내에 적용되고 있는 경우의 대부분은 지반조건에 따른 강도증가 효과를 경험적으로 파악하여 설계에 적용하고 있는 실정이고 이에 대한 많은 연구가 진행되고 있다. 본 연구에서는 고압분사주입공법의 지반교란에의 효율성을 증대시킬 목적으로 공동현상(cavitation) 이론을 응용하고자 하였다. 그리고 이를 정량적으로 분석하기 위하여 공동현상(cavitation)을 적용한 경우와 적용하지 않은 경우에 대해 지반조건, 주입압력 및 주입시간 등을 변화시켜가며 점성토 및 사질토 모형지반에 대하여 그라우팅을 실시하였다. 시험결과 공동현상(cavitation)을 적용한 경우 점성토 및 사질토 지반 모두 좋은 결과를 보여, 실제 공법에 적용가능성이 높은 것으로 나타났다.

주유동에 수직으로 분사되는 난류 비예혼합 분류 화염의 특성 (Characteristics of Turbulent Nonpremixed Jet Flame in Cross Air Flow)

  • 이기만;박정
    • 대한기계학회논문집B
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    • 제26권1호
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    • pp.125-132
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    • 2002
  • An experimental study on the characteristics of stability of propane turbulent nonpremixed jet flames discharged normal to air free-streams with uniform velocity profile is conducted. Experimental observations are focused on the flame shape, the stability considering two kinds of flame, lift-off distance, and the flame length according to velocity ratio. In order to investigate the mixing structure of the flame base at the lower limit, we employ the RMS technique and measure the species concentration by a gas chromatography. In the results of the stability curve and lifted flame, it is fecund that the dependency of nozzle diameter is closely related to the large-scale vortical structure representing counter-rotating vortices pair. Also, the detailed discussion on the phenomenon of blowout due to this large vortical motion, is provided.

항공안전인증을 고려한 소형제트항공기 플랩 재설계 (Re-Design of Wing Flap for Very Light Jet Aircraft Incorporating Airworthiness Certification)

  • 윤정원;이효진;이재우;김상호;변영환;김임권
    • 한국항공운항학회지
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    • 제19권3호
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    • pp.1-9
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    • 2011
  • In this paper, a conceptual design process for Very Light Jet aircraft has been proposed incorporating aircraft safety certification. During the proposed design process, satisfaction of the airworthiness certification for an intermediate resulting aircraft configuration is evaluated and then redesigns are carried out if necessary and until the designed aircraft configuration satisfies the airworthiness requirements. Certification database has been developed using FAR 23, AC 23, KAS 23, and CS 23 as the airworthiness certification. Based on the developed certification database Design Certifcation Related Table has been produced to use the airworthiness requirements as design constraints in the propsed design process. Using Quality Function Deployment the design variables for a redesign are carefully selected and a design optimization is performed. To demonstrate the feasibility and effectiveness of rapid aircraft conceptual design using the proposed approach, a Very Light Jet design optimization including a redesign of wing flap has been performed and the design results have been presented.

유동가시화 기법을 이용한 레이저가공의 보조가스 충돌특성에 관한 연구 (Study of Characteristics of Assist Gas in Laser Machining Using Flow Visualization Techniques)

  • 손상혁;이열;민성규
    • 대한기계학회논문집B
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    • 제35권2호
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    • pp.153-160
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    • 2011
  • 레이저가공에서 가공부위의 용융물질을 제거하는 보조가스의 역할을 살펴보기 위하여, 절단경사면에 충돌하는 초음속 동축/탈축노즐 유동의 특성이 실험적으로 관찰되었다. 보조가스의 압력, 노즐과 절단면과의 사이거리, 절단폭, 그리고 탈축노즐의 위치 등 다양한 관계변수의 변화에 대하여, 수백 개의 고해상도의 쉴러린 영상이 획득되었다. 그 결과, 단순한 보조가스의 증가가 절단면 하부에서 발생하는 유동박리를 제거하는데 효율적이지 않음이 관찰되었고, 절단폭의 증가와 탈축노즐의 운용으로 절단면에서의 박리현상을 경감시킬 수 있음이 확인되었다. 또한 음속노즐에 비하여 초음속노즐의 경우는 노즐출구와 가공면 사이의 사이거리가 절단면에서의 박리현상에 큰 영향을 미치지 않음이 관찰되었다.

설계점 및 탈설계점에서의 원심압축기 회전차 내부 2차유동 (Secondary flows through an impeller of centrifugal compressor at design and off-design conditions)

  • 최영석;강신형
    • 대한기계학회논문집B
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    • 제20권11호
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    • pp.3573-3588
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    • 1996
  • The flow through a centrifugal compressor impeller was calculated using the 3-dimensional Navier-Stokes solution method. A control volume method based on a rotating curvilinear coordinate system was used to solve the time-averaged Navier-Stokes equations, and a standard k-.epsilon. model was used to obtain eddy viscosity. Numerical results and experimental data were compared for the overall performance of the impeller, the pressure distributions along the shroud wall and the detailed flowfields at the design and off-design conditions, which showed good coincidence. The flow through the impeller is complex with the curvature of the streamlines and rotation. The development of secondary flows and the jet-wake flow characteristics, which is the main source of flow loss, was discussed. Calculation results show quite different patterns as the flow rate changes.