• 제목/요약/키워드: Frequency instability

검색결과 644건 처리시간 0.021초

산화제 과잉 삼중분사기 예연소기 개발 시험 (Design and Test of Oxidizer-Rich Triplex Injector Preburner)

  • 하성업;문일윤;강상훈;문인상;이수용
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2012년도 제38회 춘계학술대회논문집
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    • pp.76-80
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    • 2012
  • 산화제 과잉 삼중분사기에 대한 설계와 제작이 이루어졌으며, 이를 사용한 단일분사기 예연소기가 제작되어 연소시험을 수행하였다. 1100Hz의 1L 모드 고주파 불안정과 100 Hz 저주파 불안정이 관찰되었으며, 연소실 직경 수정과 터뷸런트 링 적용에 의해 고주파 불안정은 억제되었다. 현재는 저주파 압력섭동 억제에 주안을 두고 연구가 진행중에 있다.

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기체 탄화수소 연료 연소시험에서 연소불안정의 개루프 제어 (Open-Loop Control of Combustion Instability in Hot-Firing Test Using Gaseous Hydrocarbon Fuel)

  • 황동현;안규복
    • 한국추진공학회지
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    • 제22권6호
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    • pp.28-36
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    • 2018
  • 기체 탄화수소 연료를 사용하는 덤프 연소기의 연소불안정에 개루프 제어를 적용하는 연구를 수행하였다. 연료들의 특성화학시간이 유사한 연소조건에서 음향 발생기를 이용하여 제어 출력과 주파수를 변화시켰다. 연소불안정 주파수와 동일한 주파수의 개루프 제어에서는 음향 발생기의 출력이 제어성능에 영향을 주었다. 연소불안정 주파수와 다른 주파수의 개루프 제어결과로부터 개루프 제어주파수는 연소불안정 주파수와 유사하게 설정하는 것이 효과적임을 알 수 있었다.

캘리퍼 브레이크 스퀼 소음의 불안정성 해석에 관한 연구 (A Study on the Squeal Noise Instability Analysis on Caliper Brake)

  • 이정환;김성환
    • 한국소음진동공학회논문집
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    • 제23권11호
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    • pp.957-965
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    • 2013
  • This paper deals with analytical methods for low frequency and high frequency brake squeal noise on brake-rear caliper. In order to improve low frequency and high frequency squeal noise, we take survey caliper bracket shape parameters and housing shape parameters. Besides, using the combination of bracket and housing parameter were surveyed. Thus, using the combination of bracket Alt_05 and housing Alt_45 specifications, instability analysis and brake dynamo test were carried out. Based upon the two models, low and high frequency squeal noise of base model were improved. But, for 6.0 kHz frequency noise, which is not improved, it needs to additionally study on instability analysis and combination of the other brake components.

연소 불안정 현상의 비선형적 특성 고찰 (Note on Nonlinearity of Combustion Instability)

  • 서성현
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2003년도 제20회 춘계학술대회 논문집
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    • pp.240-243
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    • 2003
  • Combustion instability phenomena have been observed in various different combustion systems. For each specific combustion system, pressure fluctuations measured during high frequency combustion instability presented many different characteristics. High frequency instability occurring in a lean premixed gas turbine combustor mar be dominantly affected by a nonlinear relation between pressure oscillations and heat release rate fluctuations, and gas dynamics plays a crucial role in determining an amplitude of a limit cycle for a liquid rocket thrust chamber. Combustion instability phenomena manifest their inherent nonlinear characteristics. One is a limit cycle and the other bifurcation described by nonlinear time series analysis.

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PLIF 및 자발광 계측을 이용한 이중선회 가스터빈 연소기에서 연소불안정 모드 연구 (A Study of Combustion Instability Mode in Dual Swirl Gas Turbine Combustor by PLIF and Chemiluminescence Measurement)

  • 최인찬;이기만
    • 한국연소학회지
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    • 제19권1호
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    • pp.29-38
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    • 2014
  • This paper described an experimental investigations of combustion instability mode in a lean premixed dual swirl combustor for micro-gasturbine system. When such the instability occurs, a strong coupling between pressure oscillations and unsteady heat release excites a self-sustained acoustic wave which results in a loud, annoyed sound and may also lead a structural damage to the combustion chamber. The detailed period of flame behavior and heat release in combustion instability mode have been examined with high speed OH and CH-PLIF system and $CH^*$ chemiluminescence measurement, flame tomography with operated at 10 kHz and 6 kHz each. Experiment results suggest that unstable flame behavior has a specific frequency with 200 Hz and this frequency is accords with about 1/2 sub-harmonic of combustor resonance frequency, not fundamental frequency. This is very interesting phenomenon that have not reported yet from other previous works. Therefore, when a thermo-acoustic instability with Rayleigh criterion occurs, the fact that the period of heat release and flame behavior are different each other was proposed for the first time through this work.

Numerical study of the effect of periodic jet excitation on cylinder aerodynamic instability

  • Hiejima, S.;Nomura, T.
    • Wind and Structures
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    • 제5권2_3_4호
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    • pp.141-150
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    • 2002
  • Numerical simulations based on the ALE finite element method are carried out to examine the aerodynamics of an oscillating circular cylinder when the separated shear flows around the cylinder are stimulated by periodic jet excitation with a shear layer instability frequency. The excitation is applied to the flows from two points on the cylinder surface. The numerical results showed that the excitation with a shear layer instability frequency can reduce the negative damping and thereby stabilize the aerodynamics of the oscillating cylinder. The change of the lift phase seems important in stabilizing the cylinder aerodynamics. The change of lift phase is caused by the merger of the vortices induced by the periodic excitation with a shear layer instability frequency, and the vortex merging comes from the high growth rate, the rapid increase of wave number and decrease of phase velocity for the periodic excitation in the separated shear flows.

연소장치에서 발생하는 고주파 연소 불안정 특성 (Characteristics of High-Frequency Combustion Instabilities Occurring in Combustion Devices)

  • 서성현
    • 한국연소학회지
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    • 제17권1호
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    • pp.30-36
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    • 2012
  • Dynamic characteristics of combustion occurring in various combustion devices have been extensively studied since most of high-performance combustion devices are susceptible to hazardous, unstable combustion that deteriorates combustor's lifetime. One of the most severe unstable combustion phenomena is high-frequency combustion instability in which heat release fluctuations from combustion are coupled to resonant modes of the combustor. Here in this study, characteristics of high-frequency combustion instabilities observed in three different combustion devices have been presented. Lean-premixed combustion instability occurs mainly due to equivalence ratio fluctuations which induce large heat release oscillations at lean conditions. Liquid-fueled combustion also shows high-frequency instability from energy coupling between pressure and heat release oscillations.

화염거동을 통한 이중선회 가스터빈 모델 연소기에서 연소실 길이에 따른 연소 불안정성 이해 (Combustion Instability Comprehension with Combustion Chamber Length in Dual Swirl Gas Turbine Model Combustor from Flame Behaviors)

  • 장문석;이기만
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2015년도 제51회 KOSCO SYMPOSIUM 초록집
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    • pp.233-235
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    • 2015
  • This study is to investigate the combustion instability of the variation of combustion chamber length in dual swirl gas turbine model combustor. When equivalence ratio was fixed at 1.1, as the length of the combustion chamber increases the value of the frequency decreased in 7kW while the value of the frequency was constant in 4kW. The analysis of flame behaviors by high speed camera was conducted to identify such trend.

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초음속 공기흡입식 엔진 연소기의 연소불안정 발생 및 분석 (Occurance and Analysis of Combustion Instability in Supersonic Airbreathing Engine)

  • 황용석;이종근;최호진;길현용;변종렬;윤현걸;임진식
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2009년도 춘계학술대회 논문집
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    • pp.83-87
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    • 2009
  • 램제트 엔진은 다른 공기흡입식 엔진에 비해 상대적으로 매우 긴 유로를 지니고 있음으로 인해 저주파 연소불안정에 취약한 단점을 지니고 있다. 본 연구에서는 램제트 엔진에서 발생하는 연소 현상과 동일한 메카니즘을 모사할 수 있는 연료분사장치 및 V-gutter 형태의 화염안정화장치를 장착한 소형 연소기를 설계/제작하여, 램제트 연소기에서 발생할 수 있는 연소불안정 현상을 시현하였다. 이 연소기에서 발생한 연소불안정은 연소시스템의 음향학적인 공진 주파수와 유사하게 나타남을 확인하였으며, 이를 통해 thermo-acoustic coupling에 의한 전형적인 연소 불안정이 발생하였음을 확인할 수 있었다.

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Carcinoma Microsatellite Instability Status as a Predictor of Benefit from Fluorouracil-Based Adjuvant Chemotherapy for Stage II Rectal Cancer

  • Yang, Liu;Sun, Yan;Huang, Xin-En;Yu, Dong-Sheng;Zhou, Jian-Nong;Zhou, Xin;Li, Dong-Zheng;Guan, Xin
    • Asian Pacific Journal of Cancer Prevention
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    • 제16권4호
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    • pp.1545-1551
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    • 2015
  • Purpose: Rectal cancers with high microsatellite-instable have clinical and pathological features that differentiate them from microsatellite-stable or low-frequency carcinomas, which was studied rarely in stage II rectal cancer, promoting the present investigation of the usefulness of microsatellite-instability status as a predictor of the benefit of adjuvant chemotherapy with fluorouracil in stage II rectal cancer. Patients and Methods: Data of 460 patients who underwent primary anterior resection with a double stapling technique for rectal carcinoma at a single institution from 2008 to 2012 were retrospectively collected. All patients experienced a total mesorectal excision (TME) operation. Survival analysis were analyzed using the Cox regression method. Results: Five-year rate of disease-free survival (DFS) was noted in 390 (84.8%) of 460 patients with stage II rectal cancer. Of 460 tissue specimens, 97 (21.1%) exhibited high-frequency microsatellite instability. Median age of the patients was 65 (50-71) and 185 (40.2%) were male. After univariate and multivariate analysis, microsatellite instability (p= 0.001), female sex (p<0.05) and fluorouracil-based adjuvant chemotherapy (p<0.001), the 3 factors were attributed to a favorable survival status independently. Among 201 patients who did not receive adjuvant chemotherapy, those cancers displaying high-frequency microsatellite instability had a better 5-year rate of DFS than tumors exhibiting microsatellite stability or low-frequency instability (HR, 13.61 [95% CI, 1.88 to 99.28]; p= 0.010), while in 259 patients who received adjuvant chemotherapy, there was no DFS difference between the two groups (p= 0.145). Furthermore, patients exhibiting microsatellite stability or low-frequency instability who received adjuvant chemotherapy had a better 5-year rate of DFS than patients did not (HR, 5.16 [95% CI, 2.90 to 9.18]; p<0.001), while patients exhibiting high-frequency microsatellite instability were not connected with increased DFS (p= 0.696). It was implied that female patients had better survival than male. Conclusion: Survival status after anterior resection of rectal carcinoma is related to the microsatellite instability status, adjuvant chemotherapy and gender. Fluorouracil-based adjuvant chemotherapy benefits patients of stage II rectal cancer with microsatellite-stable or low microsatellite-instable, but not those with high microsatellite-instable. Additionally, free of adjuvant chemotherapy, carcinomas with high microsatellite-instable have a better 5-year rate of DFS than those with microsatellite-stable or low microsatellite-instable, and female patients have a better survival as well.