• 제목/요약/키워드: Shock test

검색결과 974건 처리시간 0.031초

웨이블렛을 이용한 충격신호분석 (Shock Test Signal Analysis using Wavelets)

  • 안호일
    • 한국군사과학기술학회지
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    • 제4권1호
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    • pp.147-154
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    • 2001
  • The underwater explosion shock test is performed for the evaluation of the shock-resistant capability which is a very critical factor considering the survivability of the battle ship. Some measured signals have impulsive noise and gaussian white noise because of the unstable power supply system and the transient movement of cables during the underwater explosion shock test. The advanced shock signal analysis method which remove the noise of measured signal using the threshold policy of the median filter and the orthogonal wavelet coefficients are proposed. It is verified that the signal-to-noise ratio was improved about 30㏈ by the numerical simulation.

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낙하 충격 실험을 통한 자기유변탄성체의 충격 흡수 성능 평가 (The Evaluation of Shock Absorption Performance of Magneto-Rheological Elastomer Through the Drop Impact Test)

  • 정경식;이철희
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2013년도 추계학술대회 논문집
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    • pp.92-93
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    • 2013
  • In this study, Shock Absorption performance of Magneto-rheological elastomer(MRE) is identified through the drop impact test. Magneto-rheological materials are divided into two groups by MR fluid in fluid state and MR elastomer in solid state like rubber. The stiffness characteristics of Magneto-rheological material can be changed as magnetic field is applied. The impact loads in MR elastomer were measured under weight of impactor. Experiment results are shown through the experiments to confirm the effect of shock absorption of MR elastomer. Thus, the MR elastomer can be applied to shock absorber used in area that shock occurs.

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충격파 발생기를 적용한 짧은 초음속 이젝터에 관한 연구 (A Study of short supersonic ejector with shock generators)

  • ;김희동
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2010년도 제35회 추계학술대회논문집
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    • pp.105-110
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    • 2010
  • Supersonic ejectors are simple mechanical components, which generally perform mixing and recompression of two fluid streams. Ejectors have found many applications in engineering. In aerospace engineering, they are used for high altitude testing (HAT) of a propulsion system by reducing the pressure of a test chamber. It is composed of three major sections: a vacuum test chamber, a propulsive nozzle, and a supersonic exhaust diffuser (SED). This paper aims at the improvement in HAT facility by focusing attention on the vertical firing rocket test stand with shock generators. Shock generators are mounted inside the SED for improving the pressure recovery. The results clearly showed that the performance of the ejector-diffuser system was improved with the addition of shock generators. The improvement comes in the form of reduction of the starting pressure ratio and the vertical height of test stand. It is also shown that shock generators are useful in reducing the total pressure loss in the SED.

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격막 파열과 충격파 터널 시험 시간에 대한 수치 연구 (Effect of a Diaphragm Opening Process on Flow Condition in Shock Tunnel)

  • 김세환
    • 한국추진공학회지
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    • 제25권6호
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    • pp.20-28
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    • 2021
  • 극초음속 유동 시험에 활용되고 있는 충격파 터널 등은 원하는 시험 조건을 얻기 위해 격막의 파열 압력비를 맞추어 운용한다. 주로 금속 재질로 이루어진 격막은 정확한 압력비를 맞추기 위해 특정 형태로 가공하거나 강제 파열 장치를 사용하여 개방한다. 격막의 개방 과정은 수백 microsecond 동안 파열과 변형을 통해 이루어지는데, 동일한 압력비에서도 개방 정도와 개방 소요 시간에 따라 시험 조건이 달라질 수 있을 것으로 예상된다. 본 연구에서는 격막의 두께 및 재질 차이를 반영할 수 있는 파열모델을 적용하여 수치 해석을 수행하고 충격파의 형성과 정체 조건의 특성에 대해 살펴보았다. 격막 파열로 인해 생성된 충격파의 속도는 격막 개방 속도에 비례하였으며, 격막의 최종 개폐율 및 소요 시간에 따라 저압관 끝단에 형성되는 정체 압력과 시험 시간에 차이가 나타나는 것을 확인할 수 있었다.

MIL-S-901D 충격시험과 과도응답해석을 이용한 DDAM 특성에 관한 연구 (Study for Characteristics of DDAM using MIL-S-901D Shock Test and Transient Response Analysis)

  • 송오섭;김룡
    • 한국소음진동공학회논문집
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    • 제16권11호
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    • pp.1132-1139
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    • 2006
  • Non-contact underwater explosions against surface ship could cause extensive equipment damage during wartime service. Thus, the need to develop methods for the design of shock resistant equipment structures and systems was strongly established. In analytical methods, DDAM(Dynamic Design and Analysis Method) and transient repsonse method are used for ship shock design. In this paper, to analyze the characteristics of DDAM, medium weight shock test, DDAM and transient response analysis for missile system equipment are performed.

함정용 추진전동기의 내충격성 해석 (Shock Resistance Analysis of a Propulsion Motor for Naval Vessels)

  • 배성욱;홍진숙;정의봉;박영수;빈재구
    • 한국소음진동공학회논문집
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    • 제20권12호
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    • pp.1183-1189
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    • 2010
  • Shock-resistance test for a real equipment for a normal vessel is one of the difficult problem in many cases because of terrible cost and weight. An analysis technique to evaluate the shock resistance in a design stage is necessary, instead In this paper, the process to evaluate the shock resistance of a propulsion motor for naval vessels was presented based on German navy's BV043 regulation. The shock signal to impose the equipment under the test was first evaluated, and was then applied to the structural FE model of the equipment. From the transient FEA, the time history of von-Mises stress was obtained by the mode superposition method. The shock resistance was evaluated using the peak value of the von-Mises stress.

외삽법을 이용한 천리안위성 충격시험 분석 (COMS Shock Test Assessment by Using the Extrapolation Method)

  • 이호형
    • 한국항공우주학회지
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    • 제40권5호
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    • pp.439-445
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    • 2012
  • 천리안위성(COMS)은 발사체에 실려 비행하는 동안 발사체의 단이나 위성덮개가 분리될 때와 위성이 발사체로부터 분리될 때 충격 하중을 받는다. 그리고, 발사체에서 분리 후 태양전지판이 전개 전개될 때, 통신안테나가 전개될 때, 그리고 기상탑재체 라디에이터 덮개가 전개될 때 충격하중을 받게 된다. 이들 충격하중에 대한 위성의 안전 여부를 지상에서 검증하기 위하여 충격 시험이 수행되었다. 본 논문에서는 천리안위성 개발 과정 중에 수행된 충격시험과 시험분석 과정을 소개하고, 해양탑재체(해양관측카메라)의 예를 이용하여 시험 결과에 대한 분석 방법을 소개하였다. 아리안-5 발사체의 경우 위성분리를 위한 조임띠 해제 충격이 위성덮개나 단분리 충격보다 낮다. 본 논문에서는 위성분리 충격시험 결과를 이용하여 발사체로부터 위성이 받는 최대 충격을 고려하기 위한 외삽법 또한 소개되었다.

에폭시계 코팅재의 내산열충격 특성에 관한 연구 (Study on the characteristics of acid resistance and thermal shock for epoxy coatings)

  • 이상열;윤병두
    • 수산해양기술연구
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    • 제43권4호
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    • pp.362-369
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    • 2007
  • This paper was studied on the characteristics of acid resistance and thermal shock for epoxy coatings in the strong acidic environment. The exhaust gas system, such as a air preheater, desulfurization equipment, for industrial boiler is damaged by dew point corrosion. To protect the acid corrosion, the coating using nonmetal was applied. The electrochemical polarization test, acid resistance and thermal shock test for epoxy coatings were carried out. And the acid resistance and thermal shock characteristics, aspect, and electrochemical anti-corrosion characteristics for epoxy coatings in the strong acidic environment were considered. The main results are as followings: As the epoxy glass flake coating by acidic thermal shock was damaged to the crack, blistering and elution etc., the current density of epoxy glass flake coating is high. But the damage of epoxy metal complex coating by acidic thermal shock was not occurred. Therefore the characteristics of acid resistance and thermal shock for epoxy metal complex coating is better than those for epoxy glass flake coating.

시간-주파수 영역에서의 연성 충격 스펙트럼 분석을 통한 하드디스크 드라이브의 충격진동 제어 (현장개발사례: SAMSUNG HDD 'SPINPOINT V40/P40 SERIES') (Shock Vibration Control of Hard-Disk Drive Using Coupled Shock Spectrum Analysis in Time-Frequency Domain)

  • 한윤식;강성우;오동호;황태연;손영
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2001년도 춘계학술대회논문집
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    • pp.1111-1116
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    • 2001
  • A transient T-F(time-frequency) signal processing technique is applied to a tilt drop and a linear shock test rigs for identification of shock characteristics of hard disk drive (HDD). The T-F technique essentially tracks the shock characteristics of pivot point response as well as head slap and lift-off phenomena. From the T-F analysis result, the shock characteristic in HDD is modeled by the two degree of freedom coupled-dynamic system, which consists of actuator arm and suspension. As shock designing tool, the maximax shock response spectrum is employed for prediction of shock performance. Finally, the shock control technique is tested with newly designed actuator arm and suspension. Experimental head slap test result shows that the shock performance is much higher with the new shockproof designed model than the current model

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항공용 마운트의 개발과 시뮬레이션 (The Development & Simulation for the Isolation Mount installed in Aircraft)

  • 전희호;박재민;이승준
    • 한국소음진동공학회논문집
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    • 제20권3호
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    • pp.223-228
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    • 2010
  • The mount which is used in military airplane should be operated in various situations such as vibration, shock and temperature. The recent mounts cost a lot and take much time to replace when they broke down. That's why new mount was produced in domestic by reverse engineering and the product has been proved its performance through environment test regarding vibration and shock. According to simulation of dynamic characteristics on vibration and shock, the result turns out to be similar to the result of the environmental test with an error of within 10 percent. As a result this research, a draft of the military aviation mount designing program is arranged.