• 제목/요약/키워드: air gun, impact test

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임팩트 테스트를 이용한 초고속 회전체용 공기 포일 베어링의 동특성 계수 측정 (Measurement of Dynamic Coefficients of Air Foil Bearing for High Speed Rotor by Using Impact Test)

  • 박철훈;최상규;함상용
    • 한국유체기계학회 논문집
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    • 제14권1호
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    • pp.5-10
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    • 2011
  • MTG(Micro turbine generator) operating at 400,000 rpm is under development and the impact test rig to measure the dynamic stiffness and damping coefficient of air foil bearing for high speed rotor is presented in this study. The stiffness and damping coefficient of air foil bearing depending on the rotational speed can be measured easily and effectively by using the simple configuration of impact test rig which is composed of air gun, gap sensors and high speed motor. The estimation results of stiffness and dampling coefficient using least square estimation method is presented as well.

차세대 소형위성 1호 충격시험 계측/분석 프로그램 개발 (Development of Shock Test Measurement/Analysis Program for NEXTSat-1)

  • 성태현;진재현;김상균
    • 항공우주시스템공학회지
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    • 제10권2호
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    • pp.34-40
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    • 2016
  • A satellite is exposed to various impact environment until orbit entry. It is particularly undergoing the biggest impact by pyro shock, which is generated when the launch vehicle stages are separated or the satellite is separated from the launch vehicle. In this paper, due to the fact that the pyro shock is prerequisite for performing the test and verification on the ground, we developed an air-gun type shock tester for NEXTSat-1 shock test at the KAIST SaTReC along with the development of program introduced by LabVIEW software. The program operated in shock tester is consist of data measurement and analysis with the convenient implementation of user interface and its easy modification of the code.

Friability 시험에 의한 둔감화약의 기계적 충격 감도 평가 연구 (A study on friability test to assess the mechanical impact sensitivity of insensitive explosives)

  • 박정수;박희덕;김성호;이정관
    • 한국군사과학기술학회지
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    • 제4권1호
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    • pp.20-29
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    • 2001
  • We recently developed a friability test procedure, which will be used as one of substance tests for Extremely Insensitive Detonating Substances(EIDSs) in Test Series 7 of the United Nations. This test was intended to assess the susceptibility of insensitive explosives to the break-up as high strain rate and subsequent ignition characteristics of the deformed material. We designed an air gun system using the hydro code simulation. The projectile velocities of the gun were in good agreement with those predicted by the hydro code with an inert material. Three different types of explosives, melt castable Comp B, castable plastic bonded explosives(PBXs), and pressable PBXs were tested during the development of the test procedure. Two tastable PBXs, i.e. DXD-09 and DXD-10, which are currently under development as candidate formulations of EIDS were classified as EIDS, since test results with these formulations were far better than the criterion of the UN Test Series 7.

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Analysis of the residual strengths and failure mechanisms in laminated composites under impact loading

  • Park, K.C.;Kim, M.S.
    • 한국정밀공학회지
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    • 제11권3호
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    • pp.105-121
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    • 1994
  • In this paper, we proposed the two-parameter model for predicting the residual strength in CFRP laminated composites subjected to high velocity impact and developed and formulated it based upon Cparino's by using the ratio of impact and the normalized residual strength. Critical indentation was obtained by the statical indentation tests. Impact tests were carried out through air-gun type impact equipment with the velocities varied 30-100m/sec. Projectiles were steel balls with 5 and 7mm in diameter. Test material was carbon/epoxy. The specimens were composed of [ .+-. 45 .deg. /0 .deg. /90 .deg. ]$\_$2/ and [ .+-. 45 .deg. ]$\_$4/stacking sequences and had 0.75$\^$T/*0.26$\^$W/*100$\^$L/(mm) dimension. Results from the proposed model were in good agreement with the test data. And failure mechanism due to high velocity impact is given here to examine the initation and deveolpment of damage by fractography and ultrasonic image system. The effects of the 0 .deg. -direction ply position and the amount to damage area on the residual strength are considered here.

중고속 충돌 실험을 위한 전자기력 발사장치의 설계와 제작 (Design and Development of Electromagnetic Launcher for Low-High Velocity Impact Test)

  • 김홍교;노학곤;강범수;김정
    • 대한기계학회논문집A
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    • 제40권10호
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    • pp.857-864
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    • 2016
  • 항공산업의 발달로 하늘에는 많은 비행기, UAV, 드론이 비행하고 있다. 비행기와 UAV는 빠른 속도로 비행하며 드론의 프로펠러는 빠른 속도로 회전하고 있다. 이렇게 빠른 속도의 비행체간의 충돌은 비행기 운항과 승객의 안전성을 위협하고, 지상에 있는 인명과 재산에 피해를 줄 수 있다. 비행체의 운항속도는 음속(340m/s) 내외이며, 프로펠러의 회전 속도는 그 보다 작은 속도 영역이다. 현재까지의 충돌 실험은 공기의 힘을 이용한 방식으로 충돌 속도를 얻었고, 공기 팽창에 따른 넓은 공간을 필요로 한다. 하지만 전자기력 발사장치는 그보다 작은 공간에서 충분한 속도를 얻을 수 있다.(~500m/s) 본 논문에서는 전자기력 발사장치의 설계와 이에 따른 제작에 관한 방법을 제시하고자 한다.

정적압입 관통 실험을 이용한 복합재 적층판의 고속충격 탄도한계속도 예측 (Prediction of Ballistic Limit for Composite Laminates Subjected to High-velocity Impact Using Static Perforation Test)

  • 유원영;김인걸;이석제;김종헌
    • Composites Research
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    • 제26권1호
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    • pp.21-28
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    • 2013
  • 본 논문에서는 유효 면적의 제한이 있는 복합재 적층판의 탄도한계속도를 예측하였다. 탄도한계속도를 예측하기 위해 정적압입 관통실험과 고속충격 실험 그리고 준실험식을 이용하였다. 정적압입 관통실험을 통해 하중-변위 데이터를 취득하고 이를 이용해서 관통에너지를 측정하였다. 고속충격 실험을 통해 실제 관통 속도 및 관통 에너지를 측정하였다. 정적압입 관통실험과 고속충격 실험을 통해 구한 에너지를 이용해 준실험식을 만들고, 준실험식과 고속충돌 실험결과와 비교해 보았다. 위 방법을 이용해 탄도한계속도를 예측하였고 정적압입 관통 실험과 준실험식에 의한 탄도한계속도 예측의 타당성을 확인하였다.

수동식 부항기의 기계적 안정성과 성능의 실험적 비교연구 (Comparative Study on Cupping Apparatuses for Medical Use by Mechanical Stability and Functional Test)

  • 소문기;송윤경;임형호
    • 한방재활의학과학회지
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    • 제18권2호
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    • pp.157-167
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    • 2008
  • Objectives : It is sure that standardization of medical instruments is very important and necessary. Cupping therapy is one of the traditional oriental medical method, and it is necessary to set up a standard of cupping therapy and instruments. Methods : We select 3 major cupping instrument makers according to a questionnaire survey of 2001 oriental medical doctors. Dae Gun is A maker, Han Sol is B maker, Dong Bang is C maker. And with these air pumps we make experiments on stability by an inner impact test and a falling test. With these cups we check stability by an inner impact test and a disinfection test. And to know function of these instruments we test a negative pressure and maintain attached cups until 5 to 10minutes. Results : All results of experiments(impacted test, disinfection test, falling test) on stability of cups and air pumps are suitable for medical instrument. And the efficiency of 3 major makers shows various results. Negative pressure of B group is the highest, C group is the second, A group is the lowest. Pressure maintenance test shows A and C group is comparatively up to the experimental standard(<10%), B group is comparatively below the experimental standard(<10%). Conclusions : Results show stability of cups and air pumps is suitable for medical instruments. And negative pressure of cupping and maintenance of pressure show various results. So it is necessary to set up a standard negative pressure of cupping and maintenance of pressure.

탄소섬유복합재료의 충격 손상에 따른 파괴 인성과 AE 특성 (Fracture Toughness and AE Behavior of Impact-Damaged CFRP)

  • 이상국;남기우;오세규
    • 비파괴검사학회지
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    • 제17권2호
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    • pp.81-88
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    • 1997
  • 탄소섬유강화복합재료(CFRP) 적층판에 비교적 낮은 에너지의 충격을 주어, 충격에 의해서 손상된 적층판을 사용하여 인장강도, 파괴 인성 및 AE 신호 특성에 미치는 충격 손상의 영향에 대하여 검토하였다. 충격손상재의 인장강도, 파괴 인성 및 AE-event count는 충격 속도와 박리 면적의 증가에 따라서 감소함을 알 수 있었다. 그리고 충격시험시에 발생한 박리 면적은 충격 속도와 비례하였다. 또한 적층 방법에 따른 손상재의 강도비와 파괴 인성비가 달라짐이 확인되어 복합재료의 내충격 설계시 손상량과 손상재의 파괴 인성 및 강도에 대한 정량적 평가를 AE 신호로부터 해석할 수 있음이 확인되었다.

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CFRP적층재의 잔류피로굽힘강도애 미치는 열습의 영향 (Influence of Hygrothermals on Residual Fatigue Bending Strength of CFRP Composite Laminates)

  • 박노식;임광희;양인영
    • 한국안전학회지
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    • 제12권2호
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    • pp.27-36
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    • 1997
  • This paper evaluates the static and fatigue bending strengths of CFRP (carbon fiber reinforced plastic) laminates subjected to hygrothermals. The specimens which had different stacking composition, orthotropic and quasi-isotropic laminated plates, were prepared for this experiment. A steel ball launched by the air gun collides against CFRP laminates to generate impact damages, and the 3-point fatigue bending test is carried out by using the impacted laminates to investigate the influence of hygrothermals on the effect on the residual bending fatigue strength of CFRP laminates.

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