• 제목/요약/키워드: Hammer sounding

검색결과 3건 처리시간 0.015초

파괴 및 비파괴 검사를 이용한 노후 교량의 교각 두부 조사 (Inspection of A Deteriorated Bridge Pier Cap Using Common Nondestructive and Destructive Test)

  • 김태완;홍성남;한경봉;박선규
    • 한국구조물진단유지관리공학회 논문집
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    • 제12권2호
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    • pp.91-102
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    • 2008
  • 비파괴 검사 기술은 현존하는 구조물의 진단을 위해 빈번하게 사용되었고, 사용되고 있다. 이러한 검사들로 본 연구에서 사용된 검사로는 육안적 검사, 해머 사운딩, 슈미트 해머, 그리고 토모그래피를 포함한 초음파 검사 등이 있다. 완료된 비파괴 검사 결과는 국부적으로 수행될 파괴검사의 위치를 산정하는데 사용되었다. 그래서, 압축강도, 염화물, 암석 분류 실험으로 구성된 파괴검사를 수행하였다. 비파괴검사와 파괴검사의 결과들을 종합하여 교각두부의 건전성을 평가하였다. 본 논문에서는 파괴 검사와 비파괴 검사의 적용과 해석, 그리고 이어지는 보수, 보강, 유지 결정 과정에 대해서 나타내었다.

A study on new soil investigation method using seismic waves generated by dynamic penetration blows

  • Saito Hideki
    • 한국지구물리탐사학회:학술대회논문집
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    • 한국지구물리탐사학회 2005년도 제7회 특별심포지움 논문집
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    • pp.3-9
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    • 2005
  • In order to obtain more reliable data for the information on the ground, a new site Investigation method is proposed, in which seismic waves (S-waves) generated by the Swedish Ram Sounding Test (SRS) are used. It is indicated that the energy transferred from the hammer to the rod in SRS's is much more stable, compared to SPT's. A series of SRS with measurements of seismic waves at the ground surface were carried out to clarify the characteristics of seismic wave propagation in the ground. As the results of comparison between seismic S-wave amplitudes and $N_d$ (blow count for 20 cm penetration in SRS), it was found that amplitudes of S-waves generated by SRS correlate well with $N_d$. The amplitude of the S-wave is thought to be more adequate parameter for the soil strength and rigidity than $N_d$.

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우주비행체 분리장치 작동에 의한 충격현상 모의 시험기 개발 (Development of Shock Testing M/C to Simulate Pyro-technic Device Explosion of Space vehicle)

  • 김홍배;오진호;문상무;우성현;이상설
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2000년도 추계학술대회논문집
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    • pp.581-586
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    • 2000
  • Explosively activated pyro-technic device is used to release exhausted rocket booster or payloads at prescribed times in the rocket's flight. It creates pyro-shock environment that rocket or payload components must survive. With the shock spectra acquired from flight data, laboratory test should be performed before flight to check whether all of component can sustain the shock environment. The pyro-shock environment simulation was created by the resonance fixture response to a projectile impact. Desired shock spectra is realized by adjusting the natural frequency of resonance plate and the velocity of impact hammer. This paper describes the development process of Pyro-shock testing machine, which is designed and tested by Korean engineers, to verify components of Korean Sounding Rocket(KSR-3) and the other Korean space vehicle. Both analytical and experimental techniques are introduced in this paper.

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