• Title/Summary/Keyword: Shock Test

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Research of the Scramjet Engine Performance Test Technique at T4 Free Piston Shock Tunnel in University of Queensland, Australia (호주 UQ의 T4 Free Piston Shock Tunnel에서의 스크램제트 엔진 성능시험 기법 연구)

  • Lee, Yang-Ji;Kang, Sang-Hun;Yang, Soo-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2007.11a
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    • pp.267-270
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    • 2007
  • Korea Aerospace Research Institute(KARI) made a scramjet engine test contract with the University of Queensland in October 2006. The experiments were conducted at Mach 7.6, Altitude 31.2 km condition in the T4 free piston-driven shock tunnel in June 2007. In this paper, the short introduction and data processing technique of the T4 free piston-driven shock tunnel will be explained.

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Shock Waveform Synthesis Methods for Shock Response Spectrum over Short Time Interval, Digital Filter for Obtaining Shock Response History and Applications Thereof (충격응답 스펙트럼이 나타나는 시간들의 차이가 짧은 충격파형의 합성방법 및 충격응답 내역을 구하는 디지털 필터)

  • Yoon, Eul-Jae
    • Journal of the Korea Institute of Military Science and Technology
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    • v.8 no.3 s.22
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    • pp.73-82
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    • 2005
  • This paper describes shock waveform synthesis methods for a shock response spectnlm over a short time interval with which intereference between parts within a test item is increased to perform a sufficient shock test for damage or malfunction which may be caused by the interference between parts, and a digital filter for obtaining a shock response history required for the shock waveform synthesis and a digital inverse filter for restoration by inversely using the digital filter. The time at which the maximax value occurs in the response history is detected in order to establish a delay time which is one of the parameters in the wavelet, on the condition that the natural frequency of SDOF system with a Q (quality factor) of 10 equals to the wavelet frequency of the zero delay wavelet input. A shock response spectrum over a short time interval and an abrupt change in the acceleration for an instant are illustrated as features of the synthesized waveform.

The Comparative Analysis on Mechanical Property Test of Carbon Nanotube-based Shock Absorbers (탄소나노튜브를 기반으로 하는 충격흡수제의 물리적 특성 비교분석)

  • Kim, Jong-Woo;Chae, Woen-Sik
    • Korean Journal of Applied Biomechanics
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    • v.22 no.2
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    • pp.237-242
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    • 2012
  • The purpose of this study was (a) to develop carbon nanotube-based shock absorbers for reducing potentially harmful impact forces and excessive foot pronation, and (b) to briefly determine how the effects of carbon nanotube-based shock absorbers on biomechanical variance during drop landing. A university student(age: 24.0 yrs, height: 176.2 cm, weight: 679.5 N) who has no musculoskeletal disorder was recruited as the subject. Hardness, specific gravity, tensile strength, elongation, 100% modulus, tear strength, split tear strength, compression set, resilience, vertical GRF, and loading rate were determined for each material. For each dependent variable, a descriptive statistics was used for different conditions. The property test results showed that tensile strength, tear strength, split tear strength, compression set, and resilience in carbon nanotube-based shock absorbers were greater than general Ethylene Vinyl Acetate(EVA). These indicated that resistance against variable strength in developed carbon nanotube-based shock absorbers were greater than general EVA. In vertical GRF of CNTC was less than those of EVA during drop landing and loading rate of CNTC was greater than EVA. It seems that the use of CNT can be a effective way of reducing and controlling shock from impact.

A Denoising Method for the Transient Response Signal (과도응답신호의 잡음제거기법)

  • Ho-Il Ahn
    • Journal of the Society of Naval Architects of Korea
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    • v.38 no.3
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    • pp.117-122
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    • 2001
  • The shock test of shipboard equipments is performed for the evaluation of the shock-resistant. capability by analyzing the maximum acceleration, the effective time duration and the shock response spectrum, etc. But some measured signals have impulsive noise and gaussian white noise because of the ambient noise, the acquisition equipment error and the transient movement of cables during the shock test. The improved transient signal analysis method which removes the noise of measured signal using the threshold policy of the median filter and the orthogonal wavelet coefficients is proposed. It was verified that the signal-to-noise ratio was improved about 30dB by the numerical simulation. And the shock response spectrum was extracted using the denoised shock response signal which was applied by this proposed method.

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The Testing Methods of the Fire and the Electric Shock on the Electric Pad Using the House (가정용 전기매트에 대한 화재 및 감전 시험법에 관한 연구)

  • Jang, In-Hyeok;Lee, Chang-Hoon;Lee, Young-Joo;Lim, Houng-Woo
    • Journal of Applied Reliability
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    • v.14 no.3
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    • pp.169-175
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    • 2014
  • In this paper, the evaluating test methods of the fire and the electric shock on the Electric pad using the house is proposed. We analyzed electric pad using magnetic shielded type hot wire because electric pad using the magnetic shielded type hot wire generally be used in the home. We analyzed FMEA in order to analyze the mechanism of the fire and the electric shock of the electric pad and designed testing methods (Durability tests on the environment, Mechanical durability tests, Electrical durability tests) obtained through the two-step QFD and tested. We verified the evaluating test methods of the fire and the electric shock on the Electric pad using the house through the analysis of the test results.

Review of Shock Test Standards for Unifying Specification of Naval Equipments (함정탑재장비 규격통일화를 위한 충격시험기준 고찰)

  • Kim, Young-Ju;Kim, Joon-Won
    • Proceedings of the Korean Society of Marine Engineers Conference
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    • 2005.11a
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    • pp.214-215
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    • 2005
  • Naval equipments are installed and used for naval vessel with different environmental conditions comparing to the commercial vessel, for example, high engine power per ship displacement size, severe vibration and shock due to high running speed and explosion from naval gun's bombardment and underwater weapons. Therefore, those equipments must be installed on shipboard with small spaces, high ambient temperature around engine room and which are required be fabricated with high resistances of vibration, shock and heat resources. But in case of commercial vessel, the performances of their recent equipments naval have been improved continuously due to the technology development of domestic shipbuilding and shipboard equipment industries, together with the related fundamental industries i.e, metal, steel and electronic industries, to an international level since 1970. With these results, it became possible to unify the specifications of shipboard equipments for the commercial and military vessels(Dual-Use). In this study, vibration and shock test standards for the commercial and military vessels will be compared and reviewed technically.

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The Testing Methods of The Fire and The Electric Shock on the LED Lamps Supply (LED 램프용 안정기에 대한 화재 및 감전 시험법에 관한 연구)

  • Jang, In-Hyeok;Na, Hyun-Jun;Lee, Chang-Hoon;Kim, Myung-Soo;Oh, Geun-Tae;Lim, Houng-Woo
    • Journal of Applied Reliability
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    • v.15 no.3
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    • pp.163-169
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    • 2015
  • In this paper, the evaluating test methods of the fire and the electric shock on the led lamp supply using the house is proposed. We analyzed FMEA in order to analyze the mechanism of the fire and the electric shock of the led lamp supply and designed durability tests on the environment ($85^{\circ}C$, 85% R.H.) and obtained through the two-step QFD and tested. We verified the evaluating test methods of the fire and the electric shock on the led lamp supply using the house through the analysis of the test results.

Simulation and Design of High-Speed Hydraulic Velocity Generator in Shock Test Machine (충격시험장치 고속유압 속도발생기 해석 및 설계)

  • Kim, Tae Hyeong;Shul, Chang Won;Kim, Yoon Jae;Yang, Myung Seog;Lee, Gyu Sub
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.38 no.6
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    • pp.663-668
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    • 2014
  • Mechanical and electrical devices in various forms are used in many different fields. These can be exposed to external environmental factors such as shock. Therefore, a shock test machine is commonly used to test these devices and evaluate their shock resistance. In this test, the break-down or permanent deformation and malfunction of inner parts due to a high stress or acceleration can be evaluated. As part of a shock test machine, a velocity generator is needed to create shocks between objects. In this study, a hydraulic velocity generator was conceptually designed and an AMESim model was developed to simulate the velocity under different conditions. Simulation results using this model were compared with the test results from a reduced-size velocity generator, and we designed a velocity generator that fits the target payload and velocity using the simulation results.

Transient testing from LV / SC coupled analysis by new shock synthesis

  • Girard, Alain;Cavro, Etienne;Dupuis, Paul-Eric
    • Advances in aircraft and spacecraft science
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    • v.5 no.2
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    • pp.177-186
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    • 2018
  • This paper deals with the idea to replace the usual high-level sine sweep test on shaker at system level, very severe, by a low level one completed by a transient test in the same configuration, in order to be more representative of the real environment, thus limiting over testing and improving the payload comfort. The problem of the transient test specification is first discussed. The proposed solution is to derive from LV/SC coupled analyses a shock response spectrum corresponding to two damping ratios. Then, the question of adequate shock synthesis is tackled. A new method with a given spectrum is considered for better potential and accuracy than the usual wavelets. A campaign on the Intespace bi-shaker devoted to system level showed its capability to perform the resulting test with one spectrum. First investigations to extend this approach to two spectra are in progress.

Drop Test for the UAV Landing Gear Performance Verification (무인정찰기 착륙장치 성능입증을 위한 낙하시험)

  • Shin, Jeong-Woo;Lee, Seung-Gyu;Yang, Jin-Yeol;Kim, Sung-Joon;Hwang, In-Hee;Chung, Sang-Joon
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2011.10a
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    • pp.250-254
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    • 2011
  • Main role of landing gear is to absorb the energy which is generated by aircraft lanidng and ground maneuvering. Generally, in order to absorb the impact energy during landing, oleo-pneumatic type shock absorber is used for aircraft landing gear. Oleo-pneumatic type shock absorber has a good energy absorbing efficiency and is light in weight because its structure is relatively simple. For the landing gear development, it is necessary to conduct drop test in order to verify shock absorbing performance. In the drop test, first, gas spring curve verification tests are conducted. Then, limit and reserve energy absorption drop tests are performed based on the STANAG 4671. The drop tests results with performance analysis results are presented.

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