• Title/Summary/Keyword: 동조주파수

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Analysis of flexure stiffness and stiffness test in DTG (동조 자이로스코프 서스펜션의 굽힘자 해석 및 시험)

  • Youn, J.O.;Kim, J.H.;Lee, J.G.
    • Journal of the Korean Society for Precision Engineering
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    • v.13 no.5
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    • pp.30-37
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    • 1996
  • The objective of this research is to explore the analysis and test method for the reliable design and fabrication of a high precision dynamically tuned gyroscope. The tuning frequency is decided by the calculation of mass moment of inertia of rotor and gimbal and the stiffness of flexures. Due to the complex geometry of the flexure, calculation of the stiffness of the suspension flexure is difficult. In this paper, three analytical methods for obtaining the stiffness of the flexure are porposed and a special testing method is used for checking the accuracy of the computed results.

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A Numerical Study on Acoustic Behavior in Combustion Chamber with Acoustic Cavity (음향공이 장착된 로켓엔진 연소실의 음향장 해석)

  • Sohn, Chae-Hoon;Kim, Young-Mog
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.30 no.4
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    • pp.28-37
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    • 2002
  • Acoustic behavior in combustion chamber with acoustoc cavity is numerically investigated by adopting linear acoustic analysis. Helmholtz-type resonator is employed as a cavity model to suppress acoustic instability passively. The tuning frequency of acoustic cavity is adjusted by varying the sound speed in acoustic cavity. Through harmonic analysis, acoustic pressure responses of chamber to acoustic oscillating excitation are shown and the resonant acoustic modes are identified. Acoustic damping effect of acoustic cavity is quantified by damping factor. As the tuning frequency approaches the target frequency of the resonant mode to be suppressed, mode split from the original resonant mode to lower and upper modes appears and thereby damping effect is degraded significantly. Considering mode split and damping effect as a function of tuning frequency, it is desirable to make acoustic cavity tuned to maximum frequency of those of the possible splitted upper modes.

쌍안정 진동형 에너지 하베스터의 특성

  • Jeong, Ji-Hyeon;Seok, Jong-Won
    • Journal of the KSME
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    • v.55 no.4
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    • pp.43-47
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    • 2015
  • 이 글에서는 쌍안정 진동형 에너지 하베스터에 대한 필요성과 유용성 및 이의 동적 특성을 소개하고, 쌍안정 특성을 이용하여 넓은 영역의 주파수 성분에 대해 동조 가능하도록 하는 주파수 광대역화 기술에 대해 설명하고자 한다.

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A Study on the Improvement of Performance in VCO Using In/Out Common Frequency Tuning (입출력 공동 주파수 동조를 통한 VCO의 성능 개선에 관한 연구)

  • Suh, Kyoung-Whoan;Jang, Jeong-Seok
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.21 no.5
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    • pp.468-474
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    • 2010
  • In this paper, a VCHO(Voltage Controlled Harmonic Oscillator) for K-band application has been designed and implemented. The proposed oscillator has a structure of two hair-pin resonators placed on input and output of active device. Using in/out common frequency tuning structure, the VCHO yields some advantages of the enhanced fundamental frequency suppression characteristic as well as the improved output power of second harmonic. According to implementation and measurement results, it was shown that a VCHO provides an output power of -2.41 dBm, a fundamental frequency suppression of -21.84 dBc, and phase noise of -101.44 dBc/Hz at 100 kHz offset. In addition, as for the bias voltage from 0 V to -10 V for the varactor diode, output frequency range of 10.58 MHz is obtained with a power variation of ${\pm}0.19\;dB$ over its frequency range.

Higher Order Spectral Analysis of Non-linear Pitching Motion (고차스펙트럼을 이용한 선체 종동요의 비선형적 거동에 관한 해석)

  • Kang, Byung-Ho;Carlos, Miguel Mejia;Kim, Tae-Ho;Park, Jun-Mo;Kong, Gil-Young
    • Journal of Navigation and Port Research
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    • v.41 no.1
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    • pp.1-8
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    • 2017
  • The estimation of non-linear ship motion is one of the most important issues in recent studies of ship stability. In this paper, bispectral analysis and bicoherence analysis were introduced in order to analyze the non-linear ship motion. In addition to the previously observed non-linear pitching motion in following seas, this study observed the non-linear phase coupling of pitching motion in following & quartering seas, and starboard beam seas. By comparing phase coupling between each frequency quantitatively via the bicoherence analysis, it was confirmed that non-linear phase coupling was much stronger in frequency regions other than the peak frequencies of a power spectrum. Furthermore, it was found out that the results of bicoherence calculation were analagous to each other, although the different normalization methods were applied.

A Study on the Voltage-controlled Oscillator for 2.3lGHz Wireless Local Loop (2.3GHz WLL용 전압제어발진기 설계에 관한 연구)

  • 최준수;허창우
    • Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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    • 2001.10a
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    • pp.630-633
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    • 2001
  • 본 논문에서는 2.3GHz대역의 WLL(무선가입자 회선망)에 사용하는 전압제어발진기를 설계하였다. 설계된 전압 제어 발진기는 3.2V, 10mA에서 동작하고 출력은 0.67dBm, 위상잡음 특성은 100kHz 옵셋 주파수에서 -102dBc/Hz이고 동조대역폭은 1V-3V의 전압변화에 2200∼2240MHz까지 40MHz의 동조 대역폭을 얻을 수 있었다. 따라서 제작된 전압제어 발진기는 무선가입자 회선망에 적용할 수 있다고 본다.

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A Semi-Active Control of the Combustion Instability in a Ducted Premixed Flame (덕트 형상 연소기의 연소불안정에 대한 Semi-Active Control)

  • Song, Jae-Cheon;Song, Jin-Kwan;Hwang, Jeong-Jae;Yoon, Young-Bin;Lee, Jong-Guen
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.37 no.11
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    • pp.1131-1139
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    • 2009
  • Combustion Instabilities are caused by a coupling between acoustic waves and unsteady heat release. They can be eliminated using passive controller such as a Helmholtz resonator. But, Helmholtz resonator is normally only effective over a narrow frequency range. In this work, Helmholtz resonator is applied for reducing the combustion oscillations and we vary the Helmholtz resonator volume using piston in oder to tune in the wide range of operating conditions. As the result, it is found that the dominant combustion oscillations can be largely reduced by optimizing the size of resonator volume. And, interesting relation for phase difference of dynamic pressure both combustor and the helmholtz resonator are presented in this paper. Also, we investigate semi-active control using Helmholtz equation and phase difference.

Effect of Swirl Injector with Multi-Stage Tangential Entry on Acoustic Damping in Liquid Rocket Engine (액체로켓에서 다단 접선 유입구를 갖는 스월인젝터의 음향학적 감쇠기능)

  • ;;;;Bazarov, V. G.
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.34 no.10
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    • pp.71-79
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    • 2006
  • Swirl injector with multi-stage tangential entry was analyzed to suppress high-frequency combustion instability in Liquid Rocket Engines. In order to analyze the effect of swirl injector as an acoustic absorber, swirl injector was regarded as a quarter-wave resonator and it's damping capacity is verified in atmospheric temperature. It has a finite mode of vibration and natural frequencies which can be tuned to the natural frequencies of a model combustion chamber. The interior air core shape of injector is more stable in the case of using the swirl injector with multi-stage entry than with single-stage entry. Also, when the swirl injector with multi-stage entry is used, tuned-injector length for unstable mode is well agreed with the calculated length. From the experimental data, it is proved that if the interior air core shape of swirl injector is stable, the fine tuned swirl injector can decrease the unstable mode of model chamber effectively and increase the damping rate.

Spatial - Frequency Analysis of time-varying Coherence using ERP signals for attentional visual stimulus (시각 자극의 집중에 따른 시간 변화에 대한 뇌 유발전위의 공간 - 주파수간 상관 변화 분석)

  • Lee, ByuckJin;Yoo, Sun-Kook
    • Science of Emotion and Sensibility
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    • v.16 no.4
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    • pp.527-534
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    • 2013
  • In this study, we analyzed spatial-frequency relationship related brain function for change of the time during attentional visual stimulus through the analysis of Coherence. With experimentation about ERP(Event Related Potential)data, it revealed that change of the phase synchronization between different scalp locations at ${\theta}$, ${\alpha}$ band. ERP between left and right frontal lobes, between the frontal and central lobes showed the phase synchronization at the P100, N200, ERP between the frontal and occipital lobes showed the phase synchronization at the P300 related information of visual stimulus. Compared to STFT using the window of a fixed length, CWT is able to multi-resolution analysis with the adjustment of parameters of mother wavelet. Thus, coherence results with CWT was found to be effective for analysis of time-varying spatial-frequency relationship in ERP. The phase synchronization for inattentional visual stimulus was not observed.

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

  • Kim, Hyun-Sung;Kim, Byung-Sun;Kim, Dong-Jun;Yoon, Young-Bin
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2007.04a
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    • pp.7-12
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    • 2007
  • Swirl injector with multi-stage tangential entry was analyzed to suppress high-frequency combustion instability in Liquid Rocket Engines. In order to analyze the effect of swirl injector as an acoustic absorber, swirl injector was regarded as a quarter-wave resonator and it's damping capacity is verified in atmospheric temperature. It has a finite mode of vibration and natural frequencies which can be tuned to the natural frequencies of a model combustion chamber. When the targeted injector for each modes is located at anti-node point, the amplitude of modes was decreased. And when the injector of large diameter is mounted, the split of mode which accompanies the decrease of amplitude appeared. From the experimental data, it is proved that if the location of injector mounted is located at an anti-node position of the targeted modes with proper volume, the amplitude of modes is decreased and the split of modes occurs at anti-node point.

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