• Title/Summary/Keyword: 2X 진동

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Characteristics Analysis of a Pseudoelastic SMA Mesh Washer Gear for Jitter Attenuation of Stepper-actuated Gimbal-type Antennas (스텝모터 구동형 짐벌 안테나의 미소진동저감을 위한 초탄성 형상기억합금 메쉬 와셔 기어의 기본특성 분석)

  • Park, Yeon-Hyeok;You, Chang-Mok;Oh, Hyun-Ung
    • Journal of Aerospace System Engineering
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    • v.12 no.2
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    • pp.46-58
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    • 2018
  • A two-axis gimbal-type X-band antenna is widely used to transmit bulk image data from high-resolution observation satellites. However, undesirable microvibrations induced by driving the antenna should be attenuated, because they are a main cause of image-quality degradation of the observation satellite. In this study, a pseudoelastic memory alloy (SMA) gear was proposed to attenuate the microvibrations by driving the antenna in an azimuth angle. In addition, the proposed gear can overcome the limitations of the conventional titanium blade gear, which is not still enough and is vulnerable to plastic deformations under excessive torque. To investigate the basic characteristics of the proposed SMA mesh washer gear, a static load test was performed on the thickness of the SMA mesh washer and the rotation of the gear. Moreover, The microvibration measurement test demonstrated that the SMA mesh washer gear proposed in this study is effective for microvibration attenuation.

Modal Analysis and FEA of a Compressor Motor for 120Hz Resonance Reducing (컴프레서용 모터 120Hz 공진 저감을 위한 연구)

  • Shin, Hyun-Jang
    • Transactions of the KSME C: Technology and Education
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    • v.5 no.2
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    • pp.81-87
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    • 2017
  • 315Fr compressor motor exceeds vibration specifications. To find the reason, first a modal impact test with free-free condition is done. Second a modal test with fixed condition is done. Thereafter the test results are compared with FEM simulation results. Using free-free condition modal impact test, FEM simulation conditions (boundary, mesh..) are modified. The motor has rolling motion around 120Hz. FEM simulation also shows same result. FEM simulation will be used to develop other series compressor motors. Using this, manufacturing test model and doing test will be useless.

Micro-vibration Isolation Performance of X-band Antenna using Blade Gear (블레이드 기어를 적용한 X-밴드 안테나 미소진동 절연성능)

  • Jeon, Su-Hyeon;Kwon, Seong-Cheol;Kim, Tae-Hong;Kim, Yong-Hoon;Oh, Hyun-Ung
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2014.10a
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    • pp.893-899
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    • 2014
  • X-band antenna has been widely used to effectively transmit the high resolution image data from the observation satellite to the ground station. To achieve above mission, X-band antenna is mainly composed of the 2-axis gimbal system using stepping motors and gears. However, the micro-vibration induced by the stepping motor actuation and the imperfect gear teeth alignment during this on-orbit operation is the main source of image quality degradation. In this paper, X-band antenna combined with a blade gear for micro-vibration isolation was suggested and investigated. The structural safety of the blade gear with low rotational stiffness was confirmed by structure analysis based on the derived torque budget. The isolation performance of the X-band antenna with the blade gear was verified through micro-vibration measurement test using the dedicated micro-vibration measurement device proposed in this study.

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The Effect of Vibration of Subway on Earth & Structures in the Region of Subway (지하철 진동이 주변지반 및 인접구조물에 미치는 영향)

  • Kang, Ho Jung;Oh, Jae Eung;Chun, Byung Sik
    • KSCE Journal of Civil and Environmental Engineering Research
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    • v.7 no.2
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    • pp.1-8
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    • 1987
  • Recently, as subway traffic have been increased, vibration of each parts of subway influence on structures above subway tunnel. This paper presents a new method to reduce which was generated by subway traffic. By comparing directional coherence relationship of X, Y, Z-axis and vibrational coherence relationship of spherical signal which was unified by three directional signals, effective vibration diminishing method was proposed. It can be found that locomotive vibration(specially 1-2Hz) have the worst effect on the vibration of structures and the vibration of subway box ranked 2nd, the vibration of earth ranked 3rd.

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Infrared Absorption in $XAs_2S_3-(1-X)GeS_2$ Glassses in Multiphonon Region ($XAs_2S_3-(1-X)GeS_2$ 유리의 Multiphonon 영역에서의 적외선 흡수)

  • 마동성
    • Journal of the Korean Ceramic Society
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    • v.22 no.3
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    • pp.67-71
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    • 1985
  • 2.5~40$mu extrm{m}$ 영역에서 $XAs_2S_3-(1-X)GeS_2$ 유리의 적외선 흡수에 관하여 연구했다/ Lucovsky와 그의 연구팀이 제창한 ""분자모델""에 의하면 $8-20\mu\textrm{m}$ 영역에서 위의 유리물질의 multiphonon 흡수대는 고립된 각 분자의 기본진동대의 overtone 및 combination 과 같다. 그러므로 multiphonon 흡수영역에서 AsY3 와 GeY3의 기본진동수를 모두 가지고 있는 combination 대는 관찰되지 않고 또한 혼합된 $XAs_2S_3-(1-X)GeS_2$ 유리의 흡수계수는 순수한 $As_2Y_3$$GeY_2$ 유리의 흡수계수를 더한 것으로 표현된다. 실험에서 얻은 흡수계수는 이 분자모델로부터 예상되는 값과 잘 일치한다.값과 잘 일치한다.

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Method of Lateral Vibration Control of Korean High-Speed Railway 350x (한국형고속열차 횡방향 진동제어)

  • Kim, Sang-Soo;Kim, Young-Kuk;Park, Chan-Kyoung;Kim, Jong-Sun;Kim, Ki-Hwan
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2006.05a
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    • pp.974-978
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    • 2006
  • To improve the riding comfort and to increase the speed of high-speed railway, it needs active suspension system for railway more and more. In Korea, Korean Train Express (KTX) was opened to commercial traffic 2years ago. Korea High-speed Railway (HSR 350x) is being developed and succeeded 350km/h test run. With the increase of the speed, the vibration control of the high-speed railway becomes important to meet high ride quality. In this paper, we suggest the install of lateral damper to HSR 350x. The result shows better ride quality.

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Investigation on Forced Vibration Behavior of Composite Main Wing Structure Excited by Engine and Propeller (엔진 및 프로펠러 가진에 의한 위그선 복합재 날개 진동 해석)

  • Kong, Chang-Duk;Yoon, Jae-Huy;Park, Hyun-Bum
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2007.04a
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    • pp.217-221
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    • 2007
  • In this study, forced vibrations analysis was performed for main wing of small scale WIG vehicle which is equipped two-stroke pusher type propeller engine, in terms of structural. for the frequency response analysis, excitations were assumed by H-mode(Horizontal mode), X-mode(Twisted mode) which is main vibration mode of engine, and for the transient response analysis, excitations were assumed by L-mode(Longitudinal mode) with propeller thrust which is occurred when it revolution.

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A Study on Tail Vibration Reduction for the Next Generation High Speed EMU (차세대 분산형 고속열차의 후미진동 저감에 관한 연구)

  • Jeon, Chang-Sung;Kim, Young-Guk;Kim, Seok-Won;Kim, Sang-Soo;Choi, Sung-Hoon;Park, Tae-Won
    • Journal of the Korean Society for Railway
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    • v.15 no.6
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    • pp.543-549
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    • 2012
  • This study describes the tail vibration reduction for the next generation high speed EMU(HEMU-430X). The model of 6 cars was generated and the calculation was performed using VAMPIRE(railway vehicle dynamic software). In view of ride characteristics, HEMU-430X was expected to sway at the tail because of the yaw damper direction. The lateral acceleration of vehicle body exceeded the criteria because of hunting. To reduce this hunting motion, some methods such as wheel profile change, the change of damping coefficient for the 2nd lateral damper, the damping coefficient change of yaw damper were tested, but had little effect. Finally, the yaw damper direction was changed and the tail vibration disappeared. In real running test, the tail vibration appeared at the speed of 150km/h and the yaw damper direction change made the vehicle stable at the speed of 300km/h. The maximum test speed of HEMU-430X is 430km/h. If the tail vibration appears at higher speed, some other methods in this study may be considered to reduce it.

Investigation on Forced Vibration Behavior of Composite Main Wing Structure of A Small Scale WIG Craft Excited by Engine and Propeller (엔진 및 프로펠러에 의해 가진되는 소형 위그선 복합재 주날개의 진동 거동 해석)

  • Kong, Chang-Duck;Yoon, Jae-Huy;Park, Hyun-Bum
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.35 no.11
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    • pp.1028-1035
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    • 2007
  • this study, forced vibration analysis was performed on the composite main wing structure of a small scale WIG craft which is equipped two-stroke pusher type reciprocating engine. The structural vibration analysis based on the finite element method was performed using a commercial FEM code, MSC/NASTRAN. Excitations for the frequency response analysis were assumed as the H-mode(horizontal mode), the V-mode(vertical mode) and the X-mode(twisted mode) which are typical main vibration modes of engine. And excitations for the transient response analysis were assumed as the L-mode(longitudinal mode) with the oscillating propeller thrust which occurs.