• 제목/요약/키워드: Acoustic chamber

검색결과 253건 처리시간 0.028초

액체 램제트 엔진용 소형 연소기 직접 연결식 시험장치의 설계 방법과 시험 데이터 분석 (I) (Design Method and Preliminary Data Analysis of Subscale Direct-Connect Test Facility for Liquid Ramjet Combustor (I))

  • 성홍계;김인식;이규준;김경무;이도형;변종렬;황용석;오석진;한정식
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2003년도 제20회 춘계학술대회 논문집
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    • pp.59-63
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    • 2003
  • 액체 램제트의 연소 현상을 연구하기 위한 소형 직접 연결식 시험 장치에 대한 개념 설계 방법을 기술하였다. 본 시험 장치를 이용하여 수 차례의 시험 결과 시험장치가 정상적으로 작동됨을 확인하였다. 측정된 연소실 압력 데이터에서 약190Hz대의 특정 주파수가 계측되었으며, 이는 연소실의 1L 음향 주파수(1200Hz)와는 차이가 큰 것이다. 불안정 모드를 야기하는 원인으로 dump combustor에서 발생되는 흡입 공기의 vortex street, 쵸크 되지 않은 긴 흡입관에서 발생되는 흡입구의 resonance, 관측창으로 인해 변형된 연소실 형상 등이 그 원인으로 판단된다.

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연료 과농 가스발생기의 연소 안정성 특성 연구 (Combustion Stability Characteristics of Fuel-Rich Gas Generators)

  • 서성현;한영민;최환석
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2007년도 제29회 추계학술대회논문집
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    • pp.119-122
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    • 2007
  • 본 연구에서는 가스발생기의 연소 안정 특성을 파악하기 위해 실험적 방법을 적용하였다. 액체산소와 Jet A-1을 추진제로 사용하며 연료 과농 상태에서 작동하는 실험 가스발생기는 연소실 축 방향 공진 모드에 결합된 1200 Hz 대역의 고주파 연소불안정을 겪었다. 이 연소불안정의 발생 유무는 연소실 출구부의 음향 경계 조건과 화염의 열 발생 축 방향 위치에 매우 민감하게 반응하였다. 결과적으로 단일 분사기 노즐 크기 증가에 의한 화염의 축 방향 길이 증가는 연소안정성을 확연하게 향상시켰다.

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경계배치법에 의한 근거리 음장 해석 기법 연구; 가중치를 갖는 선배열 음원의 최적 측정점 개수의 결정 (Study on Sound Field Analysis in Near-Field using Boundary Collocation Method; Decision of Optimum Points of Measurement for Line Array Sound Source with Weighting Value)

  • 김원호
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2000년도 춘계학술대회논문집
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    • pp.1752-1761
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    • 2000
  • This paper describes the far-field estimation using the near-field measurement data. Measurement in far-field region gives us the acoustical characteristics of the source but in general measurement is made in near-field such as acoustic water tank or anechoic chamber, so far-field acoustical characteristics of the source should be predicted from near-field data. In this case, the number of measurement points in the near field which relates to the accuracy of the predicted field and the amount of data processing, should be optimized. Existing papers say that measurement points is proportional to kL and depends on geometry and directivity of the source. But they do not give us any definite criterion for the required number of measurement points. Boundary Collocation Method which is one of the far-field prediction methods, is analyzed based on Helmholtz integral equation and Green function and it has been found that the number of measurement points is optimized as 0.54kL which is about one half of the existing results.

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셀룰로오즈 흡음재의 음향적 특성 평가 (Evaluations of the Acoustics Characteristics of Cellulose Absorbers)

  • 연준오;김경우;양관섭
    • 한국소음진동공학회논문집
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    • 제23권5호
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    • pp.456-462
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    • 2013
  • Eco-friendly material applied to building would be one of the materials which is must developed for global environmental conservation and reduction of carbon dioxide. For development of eco-friendly material, a cellulose absorber has been developed with waste paper through adjustment of various mix proportions. The developed cellulose absorber has been tested for its acoustic properties such as absorption coefficient and dynamic stiffness. The absorption coefficient was evaluated by developing six samples and using impedance tube and reverberation chamber. As a result of the evaluation, 0.64(NRC) was secured in absorption coefficient and 4.7 $MN/m^3$ was indicated in dynamic stiffness. Also, for practical use of developed absorbers as inner heartwood in drywall, comparison test of sound reduction index was performed with existing glass wool absorbers and constructed drywall of gypsum board. The results have shown 55 dB(Rw) of sound reduction index in glass-wool wall and 46 dB(Rw) in cellulose.

연소실 및 추진제 변화에 따른 고체로켓 모터의 L* 불안정에 관한 연구 (Effect of Combustors and Propellant Parameters on the L* Instability of Solid Rocket Motors)

  • 이동희;류승현;주성민;김준성;문희장;성홍계;양준서
    • 한국항공운항학회지
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    • 제23권4호
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    • pp.30-35
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    • 2015
  • In this paper, a theoretical study of low frequency non acoustic instability, the $L^*$ instability, of a solid rocket motor is investigated. The $L^*$ stability criterion is determined by analysing the $L^*$ stability curves of two very distinct propellants for five different geometrical combustors. The $L^*$ instability of two extreme fuels showed totally different behavior in terms of operating pressure of the combustor. A parametric study on the stability for different chamber volume and different throat area keeping constant $L^*$ is conducted and analyzed. It was found that one of the main parameters, the non-dimensional critical characteristic time, requires an enough margin from the critical $L^*$ stability curve.

압축기 흡입배관 압력 맥동 특성의 실험 및 해석 (Analysis and Experiment of Pressure Pulsation in a Suction Pipe of Compressor)

  • 오한음;정의봉;안세진;김민성
    • 한국소음진동공학회논문집
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    • 제24권10호
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    • pp.756-762
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    • 2014
  • This paper dealt with numerical estimation of the pressure pulsation of the refrigerant in a suction pipe of the compressor. The behavior of the pressure pulsation was assumed to satisfy the wave equation. The boundary conditions and properties of refrigerant are necessary as input data of the simulation. The pulsating pressures at 15 points in a pipe were measured simultaneously from the pressure transducers. From the experimental data, the complex phase speed and impedance at the end of the pipe of the refrigerant were estimated using the signal processing and used as the input conditions of the numerical analysis. A commercial acoustic software was used to solve the behavior of pressure pulsation. The numerical results for the pressure pulsation in a pipe with and without expansion chamber were carried out and compared with those by experiments. Finally, numerical procedure to estimate the pressure pulsation in a pipe was established and verified.

탄성표면파 필터용 ZnO 압전 박막의 제조 (The Preparation of ZnO Piezo-electric Thin Film for Surface Acoustic Wave Filter)

  • 이동윤;박재준
    • 한국전기전자재료학회:학술대회논문집
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    • 한국전기전자재료학회 2005년도 춘계학술대회 논문집
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    • pp.10-14
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    • 2005
  • Zinc Oxide(ZnO) thin films on Si (100) substrates were deposited by RF magnetron reactive sputtering. The characteristics of zinc oxide thin films with changing sputtering conditions such as argon/oxygen gas ratios, RF power, and substrate temperature, chamber pressure and target-substrate distance were investigated. To analyze a crystallographic properties of the films, $\theta/2{\theta}$ mode X -ray diffraction, SEM, and AFM analyses. C-axis preferred orientation, resistivity, and surface roughness highly depended on Ar/$O_2$ gas ratios. The resistivity of ZnO thin films rapidly increased with increasing oxygen ratio and the resistivity value of $9{\times}10^7\;{\Omega}cm$ was obtained at a working pressure of 10 mTorr with Ar/$O_2$=50/50. The surface roughness was also improved with increasing oxygen ratio and the ZnO films deposited with Ar/$O_2$=50/50 showed the excellent roughness value of $28.7{\AA}$.

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기판 온도 변화에 따른 AlN 박막 성장에 잔류 산소가 미치는 영향 (Influence of Residual Oxygen on the growth of AlN Thin Films with Substrate Temperature)

  • 김병균;이을택;김응권;정석원;노용한
    • 한국전기전자재료학회논문지
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    • 제21권5호
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    • pp.463-467
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    • 2008
  • Aluminum nitride (AlN) thin films have been deposited on Au electrodes by using reactive RF magnetron sputtering method in a gas mixture of Ar and $N_2$ at different substrate temperature. It was found that substrate temperature was varied in the range up to $400^{\circ}C$, highly c-axis oriented film can be obtained at $300^{\circ}C$ with full width at half maximum (FWHM) $3.1^{\circ}$. Increase in surface roughness from 3.8 nm to 5.9 nm found to be associated with increase in grain size, with substrate temperature; however, the AlN film fabricated at $400^{\circ}C$ exhibited a granular type of structure with non-uniform grains. The Al 2p and N 1s peak in the X-ray photoelectron spectroscopy (XPS) spectrum confirmed the formation of Al-N bonds. The XPS spectrum also indicated the presence of oxynitrides and oxides, resulting from the presence of residual oxygen in the vacuum chamber. It is concluded that the AlN film deposited at substrate temperature of $300^{\circ}C$ exhibited the most desirable properties for the application of high-frequency surface acoustic devices.

상압기상연소시험을 통한 동축형 스월 분사기와 충돌형 분사기의 연소 안정성 평가 (An Experimental Assessment of Combustion Stability of Coaxial Swirl Injectors and an Impinging Injector through Simulating Combustion Test)

  • 박준형;김홍집
    • 한국연소학회지
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    • 제22권1호
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    • pp.46-52
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    • 2017
  • High-frequency combustion instabilities may occur during the development of feasible engine combustors. These instabilities can result in irreparable damages to the wall of combustors or the degradation of engine performance. So, it is essential to identify injectors that have high stability characteristics during the early stages of development. The objective of present study was to assess the stability of coaxial injectors and an impinging injector with different recess lengths in order to develop stable injectors optimally. Stability margin was evaluated based on the distance from operating condition to the unstable regions. A simulating combustion test method was used to analyze the stability of injectors. A small-scale combustion chamber was designed to simulate the first tangential acoustic mode of the actual combustor. Gaseous oxygen and a mixture of methane and propane were used as simulant propellants to satisfy their flow similarity to the actual propellants of a combustor in a liquid rocket combustor. The results indicated that injectors having small recess lengths showed relatively large combustion stability margins. For the injectors of large recess lengths, instability regions with large and super-large amplitude oscillations were observed. Thus, injector with shorter recess lengths had a higher stability than that of longer one due to the different mixing processes.

空氣밸브型 脈動燃燒器의 特性에 관한 實驗的 硏究 (An experimental study of the overall characteristics in an aero-valved pulsating combustor)

  • 오상헌;최병륜;임광열
    • 대한기계학회논문집
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    • 제11권2호
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    • pp.271-278
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    • 1987
  • 본 논문에서는 공기밸브형 진동연소기에 관한 이해를 더 증진시키기 위해서 기본적인 공기밸브형 진동연소기를 제작해서 압력진동 및 발생되는 소음특성, 작동주 파수, 그리고 연소특성에 관해 실험적 고찰을 행했다.