• Title/Summary/Keyword: Double chamber

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모의 추진제를 이용한 액체로켓엔진용 다중 분사기의 연소안정성 평가 방법 (Combustion stability assessment of muti-injector using simulant propellant in LRE)

  • 서성현;송주영;설우석;이광진
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2004년도 제23회 추계학술대회 논문집
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    • pp.229-234
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    • 2004
  • The objective of the present study is to conduct model combustion tests for double swirl coaxial injectors to identify their combustion stability characteristics. Gaseous oxygen and mixture of methane and propane have been used as simulant propellants. Two model chambers tuned to the If acoustic resonance mode of a full-scale thrust chamber were manufactured to be used as a combustion cylinder. The main idea of the experiment is that the mixing mechanism is considered as a dominant factor significantly affecting combustion instability in a full-scale thrust chamber. Self-excited dynamic pressure values in a model chamber show different combustion stability zones with respect to a recess number. Upon test results, couplings between combustion conditions and the IT acoustic resonance mode become strengthened with the increase of a recess length.

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이중원추형 모형연소기에서 압력과 공기비에 따른 화염 구조 및 NOx 배출특성 (Effect of pressure and stochiometric air ratio on flame structure and NOx emission in gas turbine dump combustor with double cone burner)

  • 남현수;한동식;김규보;전충환
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2012년도 제44회 KOSCO SYMPOSIUM 초록집
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    • pp.177-179
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    • 2012
  • This work presents an experimental investigation to study $NO_x$ emissions under stoichiometric air ratio and elevated pressure (2~10bar) in a High Press Combustor(HPC) equiped with double cone burner which was designed by Pusan Clean Coal Center(PC3). Exaust gas temperature and $NO_x$ emissions were measured at the end of the combustion chamber. The $OH^*$ radical concentration and $NO_x$ emission were decreased as a function of increasing ${\lambda}$ generally. On the other hand, $OH^*$ radical concentration and $NO_x$ emission increased with ${\lambda}$ pressure of the combustion chamber. $NO_x$ emissions which were governed by thermal $NO_x$, were highly increased under the elevated pressure, but slightly increased at sufficiently low fuel concentrations (${\lambda}>2.0$).

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이중 O링의 접촉거동 해석에 관한 수치적 연구 (A Numerical Study on the Contact Behavior Analysis of Double Layer O-rings)

  • 김청균;조승현
    • Tribology and Lubricants
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    • 제19권1호
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    • pp.9-14
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    • 2003
  • The sealing performance of an elastomeric O-ring using the double layered material has been analyzed fer the contact stress behaviors that develop between the O-ring seal and the surfaces with which it comes into contact. The leakage of an O-ring will occur when the pressure differential across the seal Just exceeds the initial (or static) peak contact stress. The contact stress behaviors that develop in compressed O-rings, in common case of dovetail grooved geometry, are investigated using the finite element method. The FE analysis includes material hyperelasticity and axisymmetry. The computed FEM results show that the contact stress behaviors are related to the ratio of diameter between the inner ring and the outer ring, and the temperature of vacuum chamber.

이중와류 분사기를 적용한 고압 모델 연소기의 연소 특성 연구 (Combustion Characteristics of Double Swirl Coaxial Injector in High Pressure Thrust Chamber)

  • 서성현;이광진;한영민;김승한;김종규;설우석
    • 한국추진공학회지
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    • 제8권1호
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    • pp.54-60
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    • 2004
  • 로켓 엔진 분사기 성능에 주요한 영향을 미치는 설계 인자 파악을 위해 이중 와류 동축형 분사기의 연소 특성에 대한 실험적 연구를 수행하였다. 본 시험에서 적용한 강제 냉각 구리 노즐은 모델 연소기를 재 사용할 수 있도록 하였다. 연소 특성에 큰 영향을 미치는 함몰 길이 변화에 따른 연소 특성 변화 파악을 위해 두 가지 종류의 분사기가 제작되어 시험에 사용되었다. 함몰 길이의 변화는 분사기의 연소 시험 시 수력학적 특성뿐만 아니라 연소 효율에 많은 영향을 미치는 것으로 파악되었다. 함몰 계수가 2인 경우 내부 혼합이 이루어지며 이는 함몰 계수가 1인 경우에 대비하여 연소 효율이 증가하며, 안정된 연소 특성을 보였다 그러나 동일한 추진제 유량을 분사하기 위해 요구되는 압력 차이가 내부 혼합이 이루어지는 경우 상대적으로 상승하는 것으로 밝혀졌다.

A SCATTERING MECHANISM IN OYSTER FARM BY POLARIMETRIC AND JERS-l DATA

  • Lee Seung-Kuk;Won Joong Sun
    • 대한원격탐사학회:학술대회논문집
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    • 대한원격탐사학회 2005년도 Proceedings of ISRS 2005
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    • pp.538-541
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    • 2005
  • Tidal flats develop along the south coast ofthe Korean peninsula. These areas are famous for sea farming. Specially, strong and coherent radar backscattering signals are observed over oyster sea farms that consist of artificial structures. Tide height in oyster farm is possible to measure by using interferometric phase and intensity of SAR data. It is assumed that the radar signals from oyster farm could be considered as double-bouncing returns by vertical and horizontal bars. But, detailed backscattering mechanism and polarimetric characteristics in oyster farm had not been well studied. We could not demonstrate whether the assumption is correct or not and exactly understand what the properties of back scattering were in oyster farm without full polarimetric data. The results of AIRSAR L-band POLSAR data, experiments in laboratory and JERS-l images are discussed. We carried out an experiment simulating a target structure using vector network analyser (Y.N.A.) in an anechoic chamber at Niigata University. Radar returns from vertical poles are stronger than those from horizontal poles by 10.5 dB. Single bounce components were as strong as double bounce components and more sensitive to antenna look direction. Double bounce components show quasi-linear relation with height of vertical poles. As black absorber replaced AI-plate in bottom surface, double bounce in vertical pole decreased. It is observed that not all oyster farms are characterized by double bounced scattering in AIRSAR data. The image intensity of the double bounce dominant oyster farm was investigated with respect to that of oyster farm dominated by single bounce in JERS-l SAR data. The image intensity model results in a correlation coefficient (R2 ) of 0.78 in double bounce dominant area while that of 0.54 in single bouncing dominant area. This shows that double bounce dominant area should be selected for water height measurement using In8AR technique.

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강제교란 방법을 이용한 액체로켓엔진 연소기의 연소안정성 시험 (Combustion Stability Test of LRE Thrust Chamber using Artificial Perturbation Method)

  • 이광진;서성현;한영민;최환석;고영성
    • 한국추진공학회지
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    • 제14권3호
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    • pp.52-60
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    • 2010
  • 이중와류 동축형 분사기가 사용된 추력 30톤급 액체로켓엔진 연소기의 연소안정성시험을 강제교란방법을 이용하여 국내 지상연소시험설비에서 수행하였다. 시험에는 분사기 리세스 수, 배플 길이, 막냉각 및 연소실 직경과 같은 설계 요소가 변경된 연소기가 사용되었으며 시험결과는 이 변수들이 액체로켓엔진 연소기의 고주파 연소안정성과 깊은 관계가 있음을 보여주었다. 강제교란에 의한 액체로켓엔진 연소기의 연소안정성 분석에 있어서 감쇠시간 대신 진동 감분을 사용한 결과로부터 감쇠인자의 증가는 액체로켓엔진 연소기의 고주파 연소안정성 향상에 영향을 미침을 확인하였다.

연소실 설계에 따른 실물형 가스발생기의 연소 안정성 특성 (Effect of Combustion Chamber Design on Combustion Stability Characteristics of a Full-scale Gas Generator)

  • 이광진;서성현;한영민;최환석;안규복
    • 한국추진공학회지
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    • 제11권1호
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    • pp.11-17
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    • 2007
  • 연소실 설계에 따른 실물형 가스발생기의 연소 안정성 특성에 대한 실험적 연구가 수행되었다. 연소성능에 주요한 영향을 미치는 분사기 헤드에는 1.5의 리세스 수를 갖는 내부 혼합형 이중 스월 분사기 37개가 배치되었다. 본 논문에서는 연소실 길이, 직경, 그리고 교반링 등 연소실 설계 변경에 따른 연소 안정성 특성에 대하여 살펴보았다. 연소시험 결과 연소실의 유효 길이가 줄어듦에 따라 불안정 주파수는 고주파 영역에서 발생되며, 압력의 강도는 전반적으로 줄어들어 유해하지 않은 수준으로 감소가 가능하였다. 하지만 축방향 공진주파수에 해당하는 압력 섭동을 완전히 제거시키지는 못하는 것으로 판단된다.

Fabrication of a polymerase chain reaction micro-reactor using infrared heating

  • Im, Ki-Sik;Eun, Duk-Soo;Kong, Seong-Ho;Shin, Jang-Kyoo;Lee, Jong-Hyun
    • 센서학회지
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    • 제14권5호
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    • pp.337-342
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    • 2005
  • A silicon-based micro-reactor to amplify small amount of deoxyribonucleic acid (DNA) has been fabricated using micro-electro-mechanical systems (MEMS) technology. Polymerase chain reaction (PCR) of DNA requires a precise and rapid temperature control. A Pt sensor is integrated directly in the chamber for real-time temperature measurement and an infrared lamp is used as external heating source for non-contact and rapid heating. In addition to the real-time temperature sensing, PCR needs a rapid thermocycling for effective PCR. For a fast thermal response, the thermal mass of the reactor chamber is minimized by removal of bulk silicon volume around the reactor using double-side KOH etching. The transparent optical property of silicon in the infrared wavelength range provides an efficient absorption of thermal energy into the reacting sample without being absorbed by silicon reactor chamber. It is confirmed that the fabricated micro-reactor could be heated up in less than 30 sec to the denaturation temperature by the external infrared lamp and cooled down in 30 sec to the annealing temperature by passive cooling.

KSTAR 진공용기 시작품 제작관련 기술분석 (Asay of the fabrication technology of the KSTAR vacuum vessel mockup)

  • 조승연
    • 한국진공학회지
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    • 제8권4A호
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    • pp.391-396
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    • 1999
  • KSTAR vacuum vessel mockup was fabricated by Korea Heavy Industries. The fabrication technology chosen for the mockup is introduced and assessed in this paper. KSTAR vacuum vessel is a huge vacuum chamber of 52 cubic meters never built in this country. Through the experiency of the KSTAR mockup fabrication, welding methods for obtaining both ultra high vacuum and structural integrity of the large vacuum chamber are extracted. The fabrication and assembly techniques for the complicated structure composed of reinforced ribs, double walls and various ports are also developed. A nondestructive test on the welding spot was performed and the results show that no major leaks violating the criterion were found. The one of the main objectives of the mockup fabrication is to measure the dimensions of the structure before and after fabrication, which plays an important role in the fabrication and the assembly. By assaying the problems occurred during mockup fabrication, the KSTAR mockup will provide the techniques for the fabrication of the main vacuum vessel.

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대형엔진용 액상분사식 LPG 연료공급방식에 대한 기초연구 (2) (The Fundamental Study on Liquid Phase LPG Injection System for Heavy-Duty Engine (II))

  • 김창업;오승묵;강건용
    • 한국자동차공학회논문집
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    • 제9권6호
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    • pp.1-7
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    • 2001
  • Recently, several LPG engines for heavy-duty vehicles have been developed, which can replace some diesel engines that are one of a main source for air pollution in urban area. As a preliminary study on the liquid phase LPG injection (hereafter LPLI) system applicable to a heavy duty LPG engine, the engine output and combustion performance were investigated with various combustion chambers and fuel compositions using a single cylinder engine equipped. Experimental results revealed that ellipse, double ellipse and nebula type combustion chamber made a more advantage in breaking swirl flow into small turbulence scale than bathtub type. Especially, performance of nebula type showed most highest efficiency and engine output under lean mixture conditions. An investigation fur various LPG fuel compositions was also carried out, and revealed that the case with 40% propane and 60% butane shows the lowest efficiency at stoichiometry, however, as the mixture became leaner its efficiency increased and became even higher for 100% propane case.

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