• Title/Summary/Keyword: 작동주파수

Search Result 233, Processing Time 0.029 seconds

Reviewing of Operating Stability about Pulse Detonation Engine's Ignition Circuit to the Type of Power Sources (점화 신호 종류에 따른 PDE 점화회로의 작동 안정성 연구)

  • Kim, Jungmin;Han, Hyung-Seok;Oh, Sejong;Choi, Jeong-Yeol
    • Journal of the Korean Society of Propulsion Engineers
    • /
    • v.22 no.6
    • /
    • pp.11-18
    • /
    • 2018
  • A pulse detonation engine (PDE) requires high operating frequency greater than 100 Hz to get meaning thrust as a propulsion devise. Thus a PDE needs an ignition circuit operating precisely at high operating frequencies. In this paper AC(alternating current) and DC(direct current) types of ignition circuits were designed and compared. Each circuit was tested at operating frequencies from 16.66 to 100.00 Hz by measuring the input signal of each circuit and the voltage change in the primary coil of the transformer. Results show that the DC power circuit can attain a maximum error rate of 5.15% at higher operating frequencies, whereas the AC power circuit displays a negligible agreement with the operating signal at frequencies greater than 33.33 Hz. Therefore it is confirmed that DC-powered ignition circuit is preferable for the PDE operating at high frequencies.

Design and evaluation of LIPCA-actuated flapping device (LIPCA 작동기로 구동되는 날갯짓 기구의 설계 및 성능평가)

  • Lee, Seung-Sik;Syaifuddin, Moh;Park, Hoon-Cheol;Yoon, Kwang-Joon;Goo, Nam-Seo
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.33 no.12
    • /
    • pp.48-53
    • /
    • 2005
  • In this paper, we present our recent progress in the LIPCA (Lightweight Piezo-Composite Actuator) application for actuation of a flapping wing device. The flapping device uses linkage system that can amplify the actuation displacement of LIPCA. The feathering mechanism is also designed and implemented such that the wing can rotate during flapping. The natural flapping-frequency of the device was about 9 Hz, where the maximum flapping angle was achieved. The flapping test under 4 Hz to 15 Hz flapping frequency was performed to investigate the flapping performance by measuring the produced lift and thrust. Maximum lift and thrust were produced when the flapping device was actuated at about the natural flapping-frequency.

Analyses on Working Frequency of A γ-type Free-piston Stirling Engine (감마형 자유피스톤 스털링 엔진의 작동주파수 분석)

  • Jang, Seon-Jun;Sim, Kyuho;Lee, Yoon-Pyo
    • Transactions of the Korean Society for Noise and Vibration Engineering
    • /
    • v.23 no.7
    • /
    • pp.654-661
    • /
    • 2013
  • The dynamic characteristics of a free-piston stirling engine(FPSE) with regard to the working frequency is investigated from theoretical and experimental studies. The FPSE is modeled as a two degree-of-freedom linear vibration system. A theoretical expression on the working frequency is derived from the instability condition for self-excitation based on the linear vibration model. A ${\gamma}$-type free-piston stirling engine is fabricated for experimental studies, and its working frequency is measured on various heater temperatures. Comparisons between the theoretical and experimental results reveal that the working frequency of the test FPSE depends on both the temperature of the compression space and the temperature difference between the expansion and compression spaces.

Three Dimensional Electro-Fluid-Structural Interaction Simulation for Pumping Performance Evaluation of a Valveless Micropump (무밸브 마이크로 펌프의 성능평가를 위한 3차원 전기-유체-구조 상호작용 해석)

  • Pham, My;Phan, Van Phuoc;Han, Cheol-Heui;Goo, Nam-Seo
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.37 no.8
    • /
    • pp.744-750
    • /
    • 2009
  • In this study, the pumping performance of a piezoelectric valveless micropump is simulated. The micropump, which was developed in the previous work, is composed of a four-layer lightweight piezocomposite actuator, a polydimethylsiloxane (PDMS) pump chamber, and two diffusers. The piezoelectric domain, the fluid domain and the structural domain are coupled in the three-dimensional simulation. We used ANSYS for the piezoelectric and structural domains and ANSYS CFX for the fluid domain. The effects of driven frequency on the flow rate have been investigated by simulating the flow characteristics for 10 Hz and 40 Hz driven frequencies. The flow rates with respect to driven frequencies up to 300 Hz have been calculated.

Equivalent mechanical model of smart actuators and optimal operating conditions (지능형 공진작동기의 기계적상사와 최적작동조건)

  • Kim, Jun-Sik
    • Proceedings of the Computational Structural Engineering Institute Conference
    • /
    • 2011.04a
    • /
    • pp.285-287
    • /
    • 2011
  • 본 논문에서는 지능형 작동기의 효율적 설계와 특성예측을 위하여 기계적 상사 모델을 개발하고, 작동기의 최적작동 조건을 고찰한다. 먼저 지능형 작동기의 기계적 상사는 단순한 2자유도 스프링-메스-뎀퍼 시스템으로 등가 시스템을 구현하였다. 이 때 스프링 강성계수는 시스템의 강성 또는 전기-기계 연성계수 등으로 상사되며, 전기회로 구성품 등은 질량, 뎀퍼 등으로 상사되어진다. 단순화된 기계적 상사모델을 이용하여 작동조건에서의 전기회로 구성품의 튜닝을 최적화 할 수 있다. 특히 작동기의 공진주파수에서의 특성을 고려하여 최적조건을 도출함으로써 그 성능을 극대화 할 수 있다.

  • PDF

A study on the design of a trumpet horn for automobiles based on acoustic reactance at the horn throat (혼 입구에서의 음향 리액턴스에 근거한 자동차용 트럼펫 혼의 설계 연구)

  • Junsu Lee;Woongji Kim;Daehyun Kim;Dongwook Yoo;Wonkyu Moon
    • The Journal of the Acoustical Society of Korea
    • /
    • v.43 no.1
    • /
    • pp.39-48
    • /
    • 2024
  • A car horn serves a crucial safety role as a means of communication between drivers and a part that alerts pedestrians in advance. While previous studies have utilized finite element method and electric circuit model to simulate and analyze characteristics of the car horns, there remains a lack of research on design methods of a trumpet horn. This paper presents a design approach that predicts the operating frequency based on the acoustic reactance at the throat of the horn, once the vibrating part is determined. We deal with a horn combining both an exponential horn and a waveguide in the acoustic section, and confirm that the acoustic reactance at the horn throat measured by impedance tube experiment agrees well compared with the numerical result obtained using the finite element method. The resonance frequency of the car horn is predicted using the COMSOL Multiphysics finite element numerical analysis model, and the proposed design method is validated by measuring the operating frequency of the designed horn in a sound pressure experiment. As a result, the resonance measured in a semi-anechoic chamber environment by applying a DC voltage of 12 [V] excluding the holder occurs accurately within a few [Hz] of the design operating frequency. This paper discuss the design method of a trumpet horn from the perspective of the horn's acoustic reactance, and is expected to be useful for designing horn systems.

Interfacial Evaluation and Hydrophobicity of Multifunctional Hybrid Nanocomposites for Self-sensing and Actuation (자체 감지능 및 작동기용 다기능 하이브리드 나노복합재료의 계면 특성 및 소수성 표면 연구)

  • Wang, Zuo-Jia;GnidaKouong, Joel;Jang, Jung-Hoon;Kim, Myung-Soo;Park, Joung-Man
    • Composites Research
    • /
    • v.23 no.2
    • /
    • pp.24-30
    • /
    • 2010
  • Interfacial evaluation and hydrophobicity of Ni-nanopowder/epoxy composites were investigated for self-sensing and actuation. Contact resistance and resistivity were measured using gradient micro-specimens. The actuation of the composites in the electromagnetic field was studied with three wave functions, i.e., sine, triangle and square functions. Due tothe presence of hydrophobic domains on the heterogeneous surface, the static contact angle of Ni-nanopowder/epoxy nanocomposite wasabout $100^{\circ}$, which was rather lower than that for super-hydrophobicity. The dynamic contact angle showed the similar trend of static contact angle. Ni-nanopowder/epoxy composite was responded wellfor both self-sensing and actuation in electromagnetic field due to the intrinsic metal property of Ni-nanopowder. Displacement of the actuator of Ni-nanopowder/epoxy composite was evaluated to obtain the maximum and the optimum performance using laser displacement sensor as functions of the wave type, frequency, and voltage. Actuation of Ni-nanopowder/epoxy composites also increased as functions of applied frequency and voltage. Actuated strain increased more rapidly at sine wave with increasing voltage compared to those of triangle or rectangular waves.

Broadband Piezoelectric Vibration Energy Harvester Using Pole-Zero Cancellation Technique (극점-영점 상쇄 기법을 이용한 광대역 압전 진동 에너지 하베스터)

  • Kim, Gi-Woo
    • Transactions of the Korean Society for Noise and Vibration Engineering
    • /
    • v.24 no.2
    • /
    • pp.87-92
    • /
    • 2014
  • This paper presents a new design for a piezoelectric energy harvester with the potential to harvest vibration energy over a wide range of excitation frequencies, particularly beyond the resonance frequency. The piezoelectric vibration energy harvester employs the concept of pole-zero cancellation occurring in a lever type anti-resonant system. The experimental results show that the proposed energy harvester can provide the potential possibility of a broadband piezoelectric vibration energy harvester.

자궁암 치료 시 고선량률 근접 치료기와 사용될 초음파 온열치료기 개발

  • Lee, Re-Na;Seo, Hyeon-Suk;Lee, Gyeong-Ja;Choe, Jin-Ho
    • Proceedings of the Korean Society of Medical Physics Conference
    • /
    • 2004.11a
    • /
    • pp.81-84
    • /
    • 2004
  • 자궁암 치료시 고선량률 강내 근접치료기와 병행하여 사용할 초음파 온열 치료기가 개발되었다. 온열치료기는 텐덤형, 오보이드 형, 원통형으로 디자인 되었다. 각각의 치료기들에 사용될 초음파원 으로 PZT물질이 사용되었다. 텐덤형의 경우 외부직경이 2mm 이고 길이가 24.5mm 인 PZT5A가 사용되었고 오보이드형은 직경 20mm, 길이 20mm 인 원통형의 PZT 8 물질을 반으로 나누어 사용하였으며 원통형 치료기는 외경 25.4mm, 길이가 15.2 mm 인 원통형 PZT 8물질이 이용되었다. 각각의 트랜스듀서의 초음파 발생효율을 측정하였다. 텐덤형의 경우 3.2MHz 로 작동하였고 평균효율성은 16.7% 이다. 오보이드형의 작동 주파수는 1.5MHz 이며 효율성을 32${\sim}$46% 이다. 마지막으로 원통형의 작동주파수는 1.7MHz 이며 측정?? 효율성의 범위는 55${\sim}$65%이다. 특성분석 결과 온열치료에 사용될 초음파원으로 사용가능함이 입증되었다. 따라서 3개의 텐덤형 드랜스듀서를 연결하여 자궁내막의 길이가 73.5mm까지 치료가능한 텐덤형 온열치료기가 제작되었고 2개의 반원통형 트랜스듀서를 연결하여 치료길이가 40mm 인 오보이드형 치료기가 제작되었다. 마지막으로 4개의 원통형 트랜스듀서를 연결하여 질암등에 사용이 가능하고 61mm 까지 치료가 가능한 원통형 온열 치료기가 제작되었다.

  • PDF

Vibration Control of a Beam with a Tip Mass using a Lightweight Piezo-composite Actuator (경량 압전 복합재료 작동기를 이용한 끝단 질량이 부착된 보의 진동 제어)

  • Martua, Landong;Park, Hoon-Cheol;Goo, Nam-Seo
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.35 no.3
    • /
    • pp.218-224
    • /
    • 2007
  • Although piezoelectric materials such as PZT have been widely used as actuators in the field of active vibration suppression, the use of bare PZT as an actuator may cause some drawbacks such as critical breaks in the installation process, short circuits in the host material and low fatigue performance. The LIPCA-C2 (lightweight piezocomposite actuator) was developed to alleviate these problems. We implemented the LIPCA as an actuator to suppress the vibration of an aluminum cantilever beam with a tip mass. In our test, we used positive position feedback control algorithm. The filter frequency for this type of feedback should be tuned to the natural frequency of the target mode. The first three experimental natural frequencies of the aluminum cantilever beam agree well with the results of finite element analysis. The effectiveness of using the LIPCA as an actuator in active vibration suppression was investigated with respect to the time and frequency domains, and the experimental results show that LIPCAs with PPF control can significantly reduce the amplitude of forced vibrations and the settling time of free vibrations. For a case study, the forced vibration control of several beams with different thicknesses were performed.