• 제목/요약/키워드: Mode instability

검색결과 396건 처리시간 0.021초

연소불안정 저감을 위한 음향학적 감쇠기능성 스월 인젝터 (Acoustic Damping Swirl Injector for Reduction of Combustion Instability)

  • 김현성;김병선;김동준;윤영빈
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2007년도 제28회 춘계학술대회논문집
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    • pp.7-12
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    • 2007
  • 액체로켓엔진에서 고주파 연소불안정을 제어하기 위하여 다단 접선 유입구를 갖는 스월 인젝터를 분석하였다. 음향흡수자로서 인젝터의 효과를 분석하기 위하여 인젝터는 1/4 파장 공명기로 해석하였고, 상온에서 감쇠 효과의 적합성을 검증하였다. 이러한 인젝터는 모델 챔버의 고유주파수에 동조 시킬 수 있는 고유주파수를 갖게 된다. 각각의 모드에 동조된 인젝터를 배(anti-node point)에 장착하여야만, 타겟모드의 진폭을 감소시킬 수 있었고, 큰 지름의 인젝터를 사용하였을 때 보다 큰 진폭의 감쇠를 동반하면서 모드 분리 현상이 나타났다. 이러한 실험 결과로부터 타겟모드에 동조된 인젝터를 적당한 볼륨으로 배(anti-node point)에 장착한다면, 모드 진폭이 감쇠하게 되고, 완전한 배(anti-node point)에서는 모드분리현상이 발생됨을 확인하였다.

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우주 발사체의 포고현상 예측을 위한 공급/추진계의 파이프 압력모드 해석 기법 제안 (Proposal of Pipe Pressure Mode Analysis Method in Propulsion System for Predicting the Pogo of Space Launch Vehicle)

  • 이상구;이시훈;신상준
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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    • pp.714-717
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    • 2017
  • 액체 추진제를 사용하는 우주발사체의 설계 단계에서 고려되는 사항 중 축방향 동적 불안정성인 포고현상에 관한 연구를 진행하였다. 포고 현상이란 발사체 구조계의 축방향 진동이 공급/추진계의 압력 및 유량의 변화를 유발하고, 이러한 변화가 구조계를 다시 가진하는 닫힌계를 구성하여 발사체의 진동을 점차적으로 증가시키는 불안정성을 말한다. 본 논문에서는 포고 현상 중 발사체 공급/추진계에서 발생하는 압력 및 유량의 변화에 대한 동적해석에 초점을 맞추었다. 우주왕복선의 연구사례를 바탕으로 공급/추진계의 음향모드 해석을 수행하여 구조계의 불안정성을 유발하는 공급라인의 모드를 예측하고자 하였다.

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동축 와류형 분사기의 연소안정성에 대한 분사기 리세스 및 연소실 길이의 영향 (Effects of Injector Recess and Combustion Chamber Length on Combustion Stability of Swirl Coaxial Injectors)

  • 박수진;황동현;안규복;윤영빈
    • 한국추진공학회지
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    • 제24권1호
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    • pp.24-33
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    • 2020
  • 본 연구에서는 액체로켓엔진용 동축 와류형 분사기의 연소불안정 특성을 파악하기 위해 기체 추진제를 이용한 모델 연소실험을 수행하였다. 연소실 공진 주파수와 분사기 혼합조건의 영향을 알아보고자, 연소실 길이, 분사기, 리세스 길이, 추진제 혼합비를 변경하면서 연소실 압력섭동을 측정하였다. 실험 결과, 각 실험조건에 따른 압력섭동 변화를 확인하였으며 안정성 매핑을 통해 연소안정성을 평가하였다. 그리고 연소실 길이와 리세스 길이 변화에 따라 종방향 모드 및 켈빈-헬름홀츠 불안정이 발생함을 발견하였다.

EFFECTS OF SUPPORT STRUCTURE CHANGES ON FLOW-INDUCED VIBRATION CHARACTERISTICS OF STEAM GENERATOR TUBES

  • Ryu, Ki-Wahn;Park, Chi-Yong;Rhee, Hui-Nam
    • Nuclear Engineering and Technology
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    • 제42권1호
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    • pp.97-108
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    • 2010
  • Fluid-elastic instability and turbulence-induced vibration of steam generator U-tubes of a nuclear power plant are studied numerically to investigate the effect of design changes of support structures in the upper region of the tubes. Two steam generator models, Model A and Model B, are considered in this study. The main design features of both models are identical except for the conditions of vertical and horizontal support bars. The location and number of vertical and horizontal support bars at the middle of the U-bend region in Model A differs from that of Model B. The stability ratio and the amplitude of turbulence-induced vibration are calculated by a computer program based on the ASME code. The mode shape with a large modal displacement at the upper region of the U-tube is the key parameter related to the fretting wear between the tube and its support structures, such as vertical, horizontal, and diagonal support bars. Therefore, the location and the number of vertical and horizontal support bars have a great influence on the fretting wear mechanism. The variation in the stability ratios for each vibrational mode is compared with respect to Model A and Model B. Even though both models satisfy the design criteria, Model A shows substantial improvements over Model B, particularly in terms of having greater amplitude margins in the turbulence-excited vibration (especially at the inner region of the tube bundle) and better stability ratios for the fluid-elastic instability.

Analysis of the buckling failure of bedding slope based on monitoring data - a model test study

  • Zhang, Qian;Hu, Jie;Gao, Yang;Du, Yanliang;Li, Liping;Liu, Hongliang;Sun, Shangqu
    • Geomechanics and Engineering
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    • 제28권4호
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    • pp.335-346
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    • 2022
  • Buckling failure is a typical slope instability mode that should be paid more attention to. It is difficult to provide systematic guidance for the monitoring and management of such slopes due to unclear mechanism. Here we examine buckling failure as the potential instability mode for a slope above a railway tunnel in southwest China. A comprehensive model test system was developed that can be used to conduct buckling failure experiments. The displacement, stress, and strain of the slope were monitored to document the evolution of buckling failure during the experiment. Monitoring data reveal the deformation and stress characteristics of the slope with different slipping mass thicknesses and under different top loads. The test results show that the slipping mass is the main subject of the top load and is the key object of monitoring. Displacement and stress precede buckling failure, so maybe useful predictors of impending failure. However, the response of the stress variation is earlier than displacement variation during the failure process. It is also necessary to monitor the bedrock near the slip face because its stress evolution plays an important role in the early prediction of instability. The position near the slope foot is most prone to buckling failure, so it should be closely monitored.

고속 충돌제트의 불안정 특성 (Instability of High-Speed Impinging Jets(II))

  • 권영필;임정빈
    • 대한기계학회논문집B
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    • 제22권4호
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    • pp.450-467
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    • 1998
  • The characteristics of the unstable impinging circular jet is investigated based on the frequency characteristics and the sound field of the impinging-tones. Two symmetric modes S1 and S2, associated with low frequency and high frequency respectively, and one helical mode H have been observed. At low speed the S2 mode is dominant and switched by the S1 mode as the speed increases. When the jet speed is high the S1 mode is very active over the impinging distance from half the nozzle diameter to its ten times, while the S2 mode occurs at shorter distance corresponding to stage 2 and 3. The helical mode H seems unstable, likely to be influenced much by the experimental environment, and occurs at relatively high speed with almost the same frequency characteristics as the S2 mode. By estimating the convection speed of the unstable jet, it is found that the ratio of the convection speed to the jet speed decreases with both Strouhal number and Reynolds number and the speed of S2 mode is faster than the Si mode. When the present experimental results are compared with the previous investigations performed for the hole tone and the impinging tone with a small plate, the S1 mode is found to be associated with the ring vortex of large diameter with low speed, but the S2 mode with the vortex of small diameter with high speed. In addition, the frequency is found to be influenced by the nozzle configuration but the characteristics is almost the same. From the impinging distance and frequency range, it can be deduced that S1 mode is related with the jet column mode and S2 mode with the shear mode.

Peak-Valley Current Mode Controlled H-Bridge Inverter with Digital Slope Compensation for Cycle-by-Cycle Current Regulation

  • Manoharan, Mohana Sundar;Ahmed, Ashraf;Park, Joung-Hu
    • Journal of Electrical Engineering and Technology
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    • 제10권5호
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    • pp.1989-2000
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    • 2015
  • In this paper, digital peak current mode control for single phase H-bridge inverters is developed and implemented. The digital peak current mode control is achieved by directly controlling the PWM signals by cycle-by-cycle current limitation. Unlike the DC-DC converter where the output voltage always remains in the positive region, the output of DC-AC inverter flips from positive to negative region continuously. Therefore, when the inverter operates in negative region, the control should be changed to valley current mode control. Thus, a novel control logic circuit is required for the function and need to be analyzed for the hardware to track the sinusoidal reference in both regions. The problem of sub-harmonic instability which is inherent with peak current mode control is also addressed, and then proposes the digital slope compensation in constant-sloped external ramp to suppress the oscillation. For unipolar PWM switching method, an adaptive slope compensation in digital manner is also proposed. In this paper, the operating principles and design guidelines of the proposed scheme are presented, along with the performance analysis and numerical simulation. Also, a 200W inverter hardware prototype has been implemented for experimental verification of the proposed controller scheme.

Hydrogen Plasma Characteristics for Photoresist Stripping Process in a Cylindrical Inductively Coupled Plasma

  • Yang, Seung-Kook;Cho, Jung Hee;Lee, Seong-Wook;Lee, Chang-Won;Park, Sang-Jong;Chae, Hee-Sun
    • JSTS:Journal of Semiconductor Technology and Science
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    • 제13권4호
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    • pp.387-394
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    • 2013
  • As the feature size of integrated circuits continues to decrease, the challenge of achieving an oxidation-free exposed layer after photoresist (PR) stripping is becoming a critical issue for semiconductor device fabrication. In this article, the hydrogen plasma characteristics in direct plasma and the PR stripping rate in remote plasma were studied using a $120{\Phi}$ cylindrical inductively coupled plasma source. E mode, H mode and E-H mode transitions were observed, which were defined by matching the $V_{rms}$ and total impedance. In addition, the dependence of the E-H mode transition on pressure was examined and the corresponding plasma instability regions were identified. The plasma density and electron temperature increased gradually under the same process conditions. In contrast, the PR stripping rate decreased with increasing proportion of $H_2$ gas in mixed $H_2/N_2$ plasma. The decrease in concentration of reactive radicals for the removal of PR with increasing $H_2$ gas flow rate suggests that NH radicals have a dominant effect as the main volatile product.

분기 모우드를 활용한 얇은 빔의 혼돈 역학에 관한 연구 (On the Chaotic Vibrations of Thin Beams by a Bifurcation Mode)

  • 이영섭;주재만;박철희
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 1995년도 춘계학술대회논문집; 전남대학교, 19 May 1995
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    • pp.121-128
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    • 1995
  • The results are summarized as what follows: 1) The modeling of thin beams, which is a continuous system, into a two DOF system yields satisfactory results for the chaotic vibrations. 2) The concept of "natural forcing function" derived from the eigenfunction of the bifurcation mode is very useful for the natural responses of the system. 3) Among the perturbation techniques, HBM is a good estimate for the response when the geometry of motion is known. 4) It is known that there exist periodic solutions of coupled mode response for somewhat large damping and forcing amplitude, as well as weak damping and forcing. 5) The route-to-chaos related with lateral instability in thin beams is composed of period-doubling and quasiperiodic process and finally follows discontinuous period-doubling process. 6) The chaotic vibrations are verified by using Poincare maps, FFT's, time responses, trajectories in the configuration space, and the very powerful technique Lyapunov characteristics exponents.exponents.

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A New Small Signal Modeling of Average Current Mode Control

  • Jung, Young-Seok;Kang, Jeong-Il;Youn, Myung-Joong
    • 전력전자학회:학술대회논문집
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    • 전력전자학회 1998년도 Proceedings ICPE 98 1998 International Conference on Power Electronics
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    • pp.609-614
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    • 1998
  • A new small signal modeling of an average current mode control is proposed. In order to analyze the characteristics of the control scheme, the discrete and continuous time small signal models are derived. The derivation are mainly come from the analysis of the sampling effect presented in the current control loop. By the mathematical interpretation of practical sampler representing the sampling effect of a current control loop, the small signal models of an average current mode control can be easily derived. The instability of the current control loop, which gives rise to the subharmonic oscillation, can be identified by the proposed models. To show the usefulness of the proposed models, the simulation and experiment are carried out. The results show that the predicted results by the proposed model are much better agreed with the measured ones than that of the conventional model, even though the high gain of the compensation network of a current control loop is employed.

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