• Title/Summary/Keyword: 상대허용진동변위

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A Study on the Determination of Vibration Criteria and Vibration Reduction at Projection Room Floor in a Complex Building (복합상가건물 영화관 영사실의 진동허용 규제치 결정 및 저감 대책)

  • Park, Hae-Dong;Kim, Kang-Boo;Baek, Jae-Ho
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2002.11b
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    • pp.671-675
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    • 2002
  • 영화관의 구조설계에서 중요한 고려 인자 중에서 음향적 관점뿐만 아니라, 영사기의 진동으로 인한 영상의 떨림 현상은 관람석에서 미치는 구조물의 동적 특성 문제에 있다. 이는 영사기-스크린-관람객 사이의 3인자에 내한 상대진동허용변위에 의해 지배됨을 고려하여, 이를 만족시키는 변수 등에 따른 진동허용규재치를 결정하는 절차가 필요하다. 본 연구에서는 영화관의 진동허용규제치를 이들 3인자에 대한 변수들을 고려한 결정 과정을 공학적인 차원에서 정리하였으며, 복합상가 건물내의 영화관 영사실에 이를 만족하기 위한 진동 저감설계 자료에 활용하였다.

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Put English Title Here (복합상가건물 영화관 영사실의 진동허용 규제치 결정 및 저감 대책)

  • 박해동;김강부;백재호
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2002.11a
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    • pp.367.2-367
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    • 2002
  • 영화관의 구조설계에서 중요한 고러 인자 중에서 음향적 관점뿐만 아니라, 영사기의 진동으로 인한 영상의 떨림 현상은 관람석에서 미치는 구조물의 동적 특성 문제가 있다. 이는 영사기-스크린-관람객 사이의 3인자에 대한 상대진동허용변위에 의해 지배됨을 고려하여, 이를 만족시키는 변수 등에 따른 진동허용규제치를 결정하는 절차가 필요하다 본 연구에서는 영화관의 진동허용규제치를 이들 3인자에 대한 변수들을 고려한 결정 과정을 공학적인 차원에서 정리하였으며, 복합상가 건물내의 영화판 영사실에 이를 만족하기 위한 진동 저감설계 자료에 활용하였다.

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A Study on the Determination of Vibration Criteria for Vibration Sensitive Equipments Using Impact Test (충격시험을 이용한 고정밀장비의 진동허용규제치 결정기법에 관한 연구)

  • 이홍기;박해동;김두훈;김사수
    • Journal of KSNVE
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    • v.7 no.2
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    • pp.247-254
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    • 1997
  • In the case of a precision equipment, it requires a vibration free environment to provide its proper function. Especially, lithography and inspection devices, which have sub-nanometer class high accuracy and resolution, have come to necessity for producing more improved giga class semiconductor wafers. This high technology equipments require very strict environmental vibration standard in proportion to the accuracy of the manufacturing, inspecting devices. The vibration criteria are usually obtained either by the real vibration exciting test on the equipment or by the analytical calculation. This paper proposes a new method to solve this problem at a time. The permissible vibration level to a precision equipment can be easily obtained by analyzing a process of Frequency Response Function. This paper also demonstrates its effectiveness by applying the proposed method to finding the vibration criteria of a Computer Hard Disk Driver by Impact Test.

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A Study on the Vibration Criteria Decision for High Technology Facilities using FRF (주파수 응답함수를 이용한 고정밀 장비의 진동허용규제치 결정기법에 관한 연구)

  • 이홍기;김두훈;김사수
    • Journal of KSNVE
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    • v.6 no.3
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    • pp.363-373
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    • 1996
  • In the case of a precision equipment, it requires a vibration free environment to provide its proper function. Especially, lithography and inspection devices, which have sub-nanometer class high accuracy and resolution, have come to necessity for producing more improved giga class semiconductor wafers. This high technology equipments require very strict environmental vibration standard in promotion to the accuracy of the manufacturing, inspecting devices. The vibration criteria are usually obtained either by the real vibration exciting test on the equipment or by the analytical calculation. The former is accurate but requires a great deal of time and efforts while the latter lacks reliability. This paper proposes a new method to solve this problem at a time. The permissible vibration level to a precision equipment can be easily obtained by analyzing the process of Frequency Response Function(FRF). This paper also demonstrates its effectiveness by applying the proposed method to finding the permissible vibration criteria of a Computer Hard Disk Drive.

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Estimating Fatigue Life of APD Electronic Equipment for Activation of a Spaceborne X-band 2-axis Antenna (2축 짐벌식 X-band 안테나 구동용 전장품 APD 제어보드의 피로수명 평가)

  • Jeon, Young-Hyeon;Oh, Hyun-Ung
    • Journal of Aerospace System Engineering
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    • v.11 no.1
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    • pp.1-7
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    • 2017
  • While a satellite is carried into orbit by a launch vehicle, it is exposed to the severe launch environment with random vibrations and shock. Accordingly, these vibration sources affect electronic equipment, particularly the printed circuit board (PCB) in the satellite. When the launch load impacts the PCB, it causes negative behavior. This causes perpendicular bending around the boundary of fixation points that finally leads to the failure of solder joints, lead wires, and PCB cracks. To overcome these issues, the electronic equipment design must meet reliability requirements. In this paper, Steinberg's method is used to derive allowable and maximum deflection to verify design from a life perspective concerning the control board of the Antenna Pointing Driver (APD) mounted on KOMPSAT-3.