• Title/Summary/Keyword: impact absorbing

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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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Analysis on the Crashworthiness of the Full Rake Korean Electric Multiple Unit Train (한국형 표준전동차 전체차량의 충돌안전도 해석 연구)

  • 구정서;김동성;조현직;권태수;최성규
    • Journal of the Korean Society for Railway
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    • v.3 no.1
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    • pp.27-33
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    • 2000
  • In this paper, numerically evaluated is the crashworthiness of the new design of the standard Korea Electric Multiple Unit Train(K-EMU)[developed by the Korea Railway Research Institute]. The 4-car consist of K-EMU is analyzed under collision conditions such as normal coupling, heavy shunting, light collision and heavy collision to collide against another stationary one at 5 kph, 10 kph, 25 kph and 32 kph, respectively. Energy absorbing capacity of its draftgear commercially available in the market and to be equipped in K-EMU is evaluated under each collision condition. Analytical results show that draftgear only is not enough to provide necessary energy absorbing capacity. It is therefore concluded that additional energy absorbers like mechanical fuses should be adopted to improve the crashworthiness of K-EMU.

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An Evaluation of Crashworthiness on the KHST using 1D collision dynamics (1차원 충돌 동역학 모델을 이용한 한국형 고속전철의 충돌안전도 평가)

  • 조현직;구정서;윤영한
    • Proceedings of the KSR Conference
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    • 2002.10a
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    • pp.47-53
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    • 2002
  • In this study, the crashworthiness of KHST is evaluated by analysing a nonlinear spring/bar-damper-mass model using 1 dimensional collision dynamics. The numerical results show that KHST can easily absorb kinetic energy at lower impact force and acceleration in heavy collisions, when compared with KTX. Also, in a light collision like a traint-to-train accident at speed under 8 kph, the carbody and components of KHST can be protected without any damage except a energy absorbing tube to be replaced easily. However, KTX may be much damaged in the light collision because there is no energy absorbing tube. In conclusion, the crashworthy performance of KHST has been much improved than that of KTX, although there remains something to be improved for a better performance.

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The Analysis and the Qualification Test Procedures for Oleo-pneumatic Landing Gear (유공압 착륙장치 해석 및 시험평가)

  • Kim, Tae-Uk;Lee, Sang-Wook;Kim, Sung-Chan
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.20 no.2
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    • pp.7-12
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    • 2012
  • A landing gear absorbs the impact energy during the touchdown and it generally consists of an oleo-pneumatic shock absorber and structural components. It should be designed not only to satisfy the static and fatigue strength requirements but to have the sufficient shock absorbing efficiency. The design loads and shock absorbing performance are to be validated by tests, which is required by MIL Spec and FAR, etc. This paper presents the development procedures from the design requirements to the qualification tests and technical points to be considered, with examples of the helicopter landing gear development.

THE EFFECT OF A CHITOSAN COATING OF DENTAL IMPLANT ON THE SHOCK ABSORPTION UNDER IMPACT TEST (키토산으로 표면처리된 인공치아의 충격전달에 관한 연구)

  • Kim, Ki-Hong;Lee, Yong-Chan;Cho, Byoung-Ouck;Choi, Kui-Won;Kwon, Ick-Chan;Bae, Tae-Soo
    • Journal of the Korean Association of Oral and Maxillofacial Surgeons
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    • v.27 no.1
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    • pp.9-14
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    • 2001
  • With the object of providing a temporary artificial periodonal ligament-like membrane around the dental implant, 10 Branemark type implants were coated with commercially available chitosan(Fluka Co., Buchs, Switzerland) which has a molecular weight of 70,000 and 80% deacetylation degree. Once this bioactive hydrophillic polymer(chitosan) contacts with blood or wound fluids, it becomes swollen and penetrates into the adjacent cancellous bone. Thus the interface between implant and surrounding bone is completely filled with chitosan. This tight junction in early healing phase enhances primary stability. The chitosan coated dental implants were implanted into the fresh patella bones from porcine knees, since the thickness of cortical bone is relatively even and their cancellous structure is homogenous. To test the shock absorbing effect, 1mm delta-rogette strain gage was installed behind the implant. The results showed 1. The principal strain peak value directed to the impact of coated implant was 0.064 0.018(p<0.05) and that of uncoated implant was 0.095(0.032 p<0.05). 2. The peak time delay of coated implant was 0.056sec(0.011 p<0.05) and that of uncoated implant was 0.024sec(0.009 p<0.05). It can be reasoned from this results that the chitosan coating has a shock absorbing effect comparable with a temporary artificial periodontal ligament.

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Design of a Variable-Stiffness Type Safety Joint for Service Robots (서비스 로봇용 가변강성 형 안전관절의 설계)

  • Jeong, Jae-Jin;Chang, Seung-Hwan
    • Journal of the Korean Society for Precision Engineering
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    • v.26 no.5
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    • pp.128-134
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    • 2009
  • This paper aims to design a variable-stiffness type economical safety joint for service robots. The safety joint was designed to have a passive shock absorbing mechanism for protecting human from a catastrophic collision under service condition of robots. A simple mechanism composed of two action disks for switching the load transfer, a spring and a screw for pre-load was proposed. In order to evaluate the performance of the safety joint a testing platform which can carry out the static and impact tests was also designed and fabricated. From the test results, the designed safety joint was proved to have a variable load-carrying capacity and about 42% impact absorption capacity with simple manipulation of the control screw.

Weight Reduction of Front Side Member with High Strength Steel (고장력강 적용을 통한 프런트 사이드 멤버의 경량화)

  • 이상곤;최창현;신철수
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2004.10a
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    • pp.1487-1490
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    • 2004
  • In this study, the crash analysis was carried out to evaluate the influence of steel sheet grade and thickness on weight reduction and crash characteristics for front side member which had an important role of absorbing the impact energy during front and side impact. In order to achieve the aim of this study the reverse engineering was applied to obtain 3D model of front side member from BIW for the FE simulation. In the result, the crashworthiness of front side member is considerably improved with steel sheet strength and thickness increase. Also, the weight reduction in automotive parts for the improvement of the fuel efficiency can be easily achieved with applying high strength steel without deterioration of crashworthiness.

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A Study on Optimal Design of Composite Materials using Neural Networks and Genetic Algorithms (신경회로망과 유전자 알고리즘을 이용한 복합재료의 최적설계에 관한 연구)

  • 김민철;주원식;장득열;조석수
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 1997.04a
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    • pp.501-507
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    • 1997
  • Composite material has very excellent mechanical properties including tensile stress and specific strength. Especially impact loads may be expected in many of the engineering applications of it. The suitability of composite material for such applications is determined not only by the usual paramenters, but its impactor energy-absorbing properties. Composite material under impact load has poor mechanical behavior and so needs tailoring its structure. Genetic algorithms(GA) is probabilistic optimization technique by principle of natural genetics and natural selection and neural networks(NN) is useful for prediction operation on the basis of learned data. Therefore, This study presents optimization techniques on the basis of genetic algorithms and neural networks to minimum stiffness design of laminated composite material.

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A study of ballistic impact energy absorbing mechanism of composites (복합재료의 방탄충격에너지 흡수에 관한 연구)

  • 강은영;윤영기;황도인;윤희석
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 1997.10a
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    • pp.773-776
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    • 1997
  • This paper presents an investigation of the energy absorption of composite laminates during ballistic impact. Three components are responsible for the absorption of energy-the tensile failure of fiber, the elastic deformation of the composite, the delamination of composite laminates. The ballistic limit, V/sub 0/, of the laminates is determined using a previous model implemented to determine the energy absorption of the three components listed above. The size of the deformed zone during impact was estimated by an approximate solution for impacts on plates. The carbon/epoxy plates were examined for this research.

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Impact Performance of a Crash Member Filled with Aluminum Foam (알루미늄 폼이 충전된 충돌부재의 충격흡수 성능)

  • Kim, N.H.;Kim, J.H.;Lee, J.K.;Kim, D.
    • Transactions of Materials Processing
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    • v.20 no.8
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    • pp.555-561
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    • 2011
  • The energy absorbing characteristics of crash members in a car collision play an important role in controlling the amount of damage to the passenger compartment. Crash members filled with aluminum foam are expected to have reduced mass while maintaining or even improving the crashworthiness compared to the conventional hollow-beam types. Finite element simulations are carried out in the present work to assess the improvement of crashworthiness by the use of aluminum foam fillers. The numerical results agreed well with experimental measurements. Parametric studies are conducted to analyze the effect of impact velocity, weld strength, and initiator on the crash response.