• Title/Summary/Keyword: Hydrospace Noise

Search Result 4, Processing Time 0.018 seconds

An Experimental Study on Ground Vibration Equations by Underwater Blasting at Construction Site (수중발파 현장에서의 진동추정식에 관한 실험적 연구)

  • Park, Yeon-Soo;Kang, Sung-Hoo;Jeon, Yang-Bae;Gong, Gang-Joo;Park, Sun-Joon
    • Transactions of the Korean Society for Noise and Vibration Engineering
    • /
    • v.16 no.7 s.112
    • /
    • pp.777-783
    • /
    • 2006
  • In this study, quantitative ground vibration values and damping coefficient produced by underwater blasting were measured and analyzed. Also, hydrospace noise in aquafarm and noise in atmosphere as well as ground vibrations were measured, and maximum values of these results were 86,8 dB(A), 147,8dB(A), 0.244 cm/s, respectively, With these results, vibration influence about snakehead (channa argus) and structures were examined. the damage of those was proved that is not. Equations of vibration ($V_{50%}=1.507SD^{-0.536},\;V_{95%}=2,171SD^{-0.536}$) and hydrospace noise ($SL=293.2SD^{-0.164}$) were presented from quantitative experiment results. respectively. The results of the study may be applied for the evaluation of the influence on aquafarm as a basic data before having main underwater blasting at construction sites.

Flow-Chart for Influence Estimation of Underwater Blasting (수중발파의 영향평가를 위한 Flow-Chart)

  • Park, Sun-Joon;Park, Yeon-Soo
    • Journal of the Korea institute for structural maintenance and inspection
    • /
    • v.12 no.5
    • /
    • pp.47-54
    • /
    • 2008
  • In this study, ground vibration values and damping coefficient produced by underwater blasting were measured and analyzed. Equations of vibration, $V=K(SD)^{-0.536}$, were presented from quantitative experiment results. The K Values are classified with 1.507, 2.005 and 2.939 respectively at 50%, 90% and 95% reliability. Also, hydrospace noise in aquafarm and noise in atmosphere as well as ground vibrations were measured, and maximum values of these results were 86.8dB(A), 147.8dB(A), 0.244cm/s, respectively. Equations of hydrospace noise, $SL=293.2SD^{-0.164}$, was presented from quantitative experiment results. Also, the flow-chart for influence estimation and underwater blast design was presented from these results. The results of the study may be applied for the evaluation of the influence on aquafarm as a basic data before having main underwater blasting at construction sites.

Effects of Inplane Modes in SEA on Structure-Borne Noise Transmission in Ship Structures

  • Kim, Jae-S.;Kim, Hyun-S.;Kang, Hyun-J.;Kim, Sang-R.
    • Journal of Hydrospace Technology
    • /
    • v.2 no.1
    • /
    • pp.18-26
    • /
    • 1996
  • It is normal practice to consider bending wave modes only, when one applies SEA (Statistical Energy Analysis) to ship structures because of complexities in SEA modeling and evaluation of coupling loss factors for inplane modes. According to the result of Tratch[1], the inplane wave modes becomes important for the analysis of a foundation structure as the distance from the source and receiver increases. In this paper, the effect of inplane wave modes on structure-borne noise propagation in ship structures is presented. It is shown that the inplane wave could increase the noise level more than 10 dB compared with the results without inplane wave modes at high frequency bands for compartments far from the source location.

  • PDF

Failure Detection Filter for the Sensor and Actuator Failure in the Auto-Pilot System

  • Suh, Sang-Hyun
    • Journal of Hydrospace Technology
    • /
    • v.1 no.1
    • /
    • pp.75-88
    • /
    • 1995
  • Auto-Pilot System uses heading angle information via the position sensor and the rudder device to control the ship's direction. Most of the control logics are composed of the state estimation and control algorithms assuming that the measurement device and the actuator have no fault except the measurement noise. But such asumptions could bring the danger in real situation. For example, if the heading angle measuring device is out of order the control action based on those false position information could bring serious safety problem. In this study, the control system including improved method for processing the position information is applied to the Auto-Pilot System. To show the difference between general state estimator and F.D.F., BJDFs for the sensor and the actuator failure detection are designed and the performance are tested. And it is shown that bias error in sensor could be detected by state-augmented estimator. So the residual confined in the 2-dimension in the presence of the sensor failure could be unidirectional in output space and bias sensor error is much easier to be detected.

  • PDF