• 제목/요약/키워드: Shock Absorption Efficiency

검색결과 17건 처리시간 0.021초

ADAMS를 이용한 항공기 전륜착륙장치의 동적거동해석 및 최적설계 (Dynamic Behaviors and Optimal Design of an Aircraft Nose Landing Gear using ADAMS)

  • 김선구;김철;김영만
    • 한국항공우주학회지
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    • 제35권7호
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    • pp.612-618
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    • 2007
  • 본 연구에서는 KT-1 계열 항공기 전륜착륙장치의 동적거동을 분석하고 충격흡수효율을 향상시키기 위한 완충기의 최적설계가 수행되었다. 전륜착륙장치는 ADAMS를 이용하여 2자유도계로 모델링하였으며 운영/환경 조건을 고려한 해석결과는 낙하실험결과와 잘 일치하였다. 또한 최적설계변수를 선정하기 위해 오일밀도, 오리피스 단면적과 같은 완충기 파라미터를 변화시켜 동적거동 및 충격흡수효율에 미치는 영향을 분석하였으며, 해석 결과 완충기 파라미터가 다른 파라미터들보다 큰 영향을 미쳤다. 유용방향탐색법을 사용하여 최적설계를 진행하였고, 최대효율을 나타낼 때 설계변수의 값을 산출하였다. 이러한 방법으로 전륜착륙장치의 최적설계를 통해 충격흡수효율과 동적거동능력을 향상시킬 수 있었다.

낙하충격실험을 통한 고무의 충격흡수성능과 전단계수 평가 (Determination of Shock Absorption Performance and Shear Modulus of Rubbers by Drop Impact Test)

  • 강동환;서무열;김학인;김태원
    • 대한기계학회논문집A
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    • 제33권4호
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    • pp.321-328
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    • 2009
  • Shock absorption performances of various rubbers were investigated by using drop impact test. Several types of rubber such as NR, NBR, EPDM, SR and PUR with three respective levels of shore hardness were used for the test. As in the cases, the absorbed impact energies in rubbers were measured under seven different loads against impact energy between 5-80J. The impact absorption efficiencies of the rubbers then were evaluated by means of both single impact energy condition and summation of all impact energy applied condition. As shown in the results, PUR and EPDM have better shock absorption performances than other rubbers. Further analysis was extended to determine a shear modulus of SR through the finite element implementation with Blatz-Ko model. As can be seen, relatively higher level of absorption energy results in a decreasing shear modulus.

자전거에서 서스펜션 종류에 따른 인체영향 시뮬레이션 (Evaluation of Shock-Absorbing Performance of Three-Different Types of Bicycle Suspension Systems)

  • 정경렬;형준호;김사엽
    • 대한기계학회논문집A
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    • 제34권7호
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    • pp.943-946
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    • 2010
  • 본 연구에서는 소형자전거의 핸들에 적용할 수 있는 전방 서스펜션을 제안하고 시뮬레이션을 통해 충격흡수 성능을 평가하였다. 서스펜션이 없는 경우, 기존의 전방포크서스펜션이 장착된 경우 그리고 제안된 핸들서스펜션이 장착된 경우 등 3가지 서스펜션 종류에 대해 인체모델을 이용한 주행시뮬레이션을 수행하여 각각의 완충성능을 비교평가 하였다. 시뮬레이션 결과 제안된 핸들 서스펜션의 경우 손과 머리에 전달된 가속도가 기존의 전방포크서스펜션이 장착된 경우보다 크게 측정되었지만 서스펜션이 없는 자전거의 경우보다는 현저히 작게 측정되었다. 이 같은 결과는 제안된 핸들 서스펜션이 상당한 완충 성능을 보여주었으며 이는 경량화가 중요한 소형자전거에 적용이 가능할 것으로 보인다.

알루미늄 허니콤의 충격 에너지 흡수 특성 예측 (Prediction to Shock Absorption Energy of an Aluminum Honeycomb)

  • 김현덕;이혁희;황도순;박정선
    • 한국항공우주학회지
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    • 제39권5호
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    • pp.391-399
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    • 2011
  • 본 연구의 목적은 알루미늄 허니콤의 충격에너지 흡수 특성을 예측하는 것이다. 알루미늄 허니콤은 가볍고 에너지 흡수효율이 뛰어나며, 우주환경에서도 사용 가능하여 달착륙선의 충격흡수장치로 사용되고 있다. 충격에너지 흡수용 허니콤의 설계를 위해서는 에너지 흡수 과정에서 일정하게 유지되는 압축강도(crush strength)의 예측이 중요하다. 본 연구에서는 유한요소법을 이용하여 허니콤의 형상 및 충돌속도에 따른 압축강도를 예측하였다. 유한요소해석 프로그램은 Ls-dyna를 이용하였으며, 효율적인 유한요소 해석을 위하여 허니콤의 단위 셀 모델을 선정하였다. 이를 바탕으로 충돌속도 및 허니콤 포일(foil)의 두께 변화, 허니콤의 분기각(branch angle)에 따른 유한요소해석을 수행하여 에너지 흡수 특성을 분석하였다.

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

  • 신정우;이승규;양진열;김성준;황인희;정상준
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2011년도 추계학술대회 논문집
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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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항공기 착륙장치 동하중 해석 (Dynamic Load Analysis of Aircraft Landing Gear)

  • 신정우;김태욱;황인희
    • 한국항공운항학회지
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    • 제16권1호
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    • pp.1-6
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    • 2008
  • Role of landing gear is to absorb energy which is generated by aircraft ground maneuvering and landing. Generally, in order to absorb the impact energy, oleo-pneumatic type shock absorber is used in aircraft landing gear. Oleo-pneumatic type shock absorber has a good energy absorption efficiency and is light in weight because structure of oleo-pneumatic type shock strut is relatively simple. In this study, dynamic load analysis for swinging arm type landing gear was performed to predict landing loads. Modeling of landing gear was conducted with MSC.ADAMS, and dynamic landing loads were analyzed based on ADS-29. Optimum landing loads were generated through adjustment of damping orifice and the analysis results were presented with various aircraft attitude.

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충격 감소 및 중력 보상을 위한 이족보행로봇의 무릎-골반 관절 설계 (Design of Knee-Pelvis Joint in the Biped Robot for Shock Reduction and Gravity Compensation)

  • 김영민;김용태
    • 전기학회논문지
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    • 제64권1호
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    • pp.136-142
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    • 2015
  • In the paper, a design method of knee and pelvis joint in the biped robot is proposed for shock absorption and gravity compensation. Similarly to the human's body, the knee joints of the biped robot support most body weight and get a shock from the landing motion of the foot on the floor. The torque of joint motor is also increased sharply to keep the balance of the robot. Knee and pelvis joints with the spring are designed to compensate the gravity force and reduce the contact shock of the robot. To verify the efficiency of the proposed design method, we develope a biped robot with the joint mechanism using springs. At first, we experiment with the developed robot on the static motions such as the bent-knee posture both without load and with load on the flat ground, and the balance posture on the incline plane. The current of knee joint is measured to analyze the impact force and energy consumption of the joint motors. Also, we observe the motor current of knee and pelvis joints for the walking motion of the biped robot. The current responses of joint motors show that the proposed method has an effect on shock reduction and gravity compensation, and improve the energy efficiency of walking motions for the biped robot.

Assessment of dynamic crushing and energy absorption characteristics of thin-walled cylinders due to axial and oblique impact load

  • Baaskaran, N.;Ponappa, K.;Shankar, S.
    • Steel and Composite Structures
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    • 제28권2호
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    • pp.179-194
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    • 2018
  • Reliable and accurate method of computationally aided design processes of advanced thin walled structures in automotive industries are much essential for the efficient usage of smart materials, that possess higher energy absorption in dynamic compression loading. In this paper, most versatile components i.e., thin walled crash tubes with different geometrical profiles are introduced in view of mitigating the impact of varying cross section in crash behavior and energy absorption characteristics. Apart from the geometrical parameters such as length, diameter and thickness, the non-dimensionalized parameters of average forces which control the plastic bending moment for varying thickness has explored in view of quantifying its impact on the crashworthiness of the structure. The explicit finite element code ABAQUS is utilized to conduct the numerical studies to examine the effect of parametric modifications in crash behavior and energy absorption. Also the simulation results are experimentally validated. It is evident that the circular cross-sectional tubes are preferable as high collision impact shock absorbers due to their ability in withstanding axial and oblique impact loads effectively. Furthermore, the specific energy absorption (SEA), crash force efficiency (CFE), plastic bending moment, peak force responses and its impact for optimally tailoring a design to cater the crashworthiness requirements are investigated. The primary outcome of the study is to provide sufficient information on circular tubes for the use of energy absorbers where impact oblique loading is expected.

ADAMS를 이용한 항공기 착륙장치 지상 충격하중 및 동적거동 해석 (An analysis on the ground impact load and dynamic behavior of the landing gear system using ADAMS)

  • 최섭;이종훈;조기대;정창래
    • 한국항공우주학회지
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    • 제30권4호
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    • pp.114-122
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    • 2002
  • 착륙장치 시스템의 개발은 설계특성상 충격흡수 성능에 대한 설계 파라메터, 최소한의 작동공간, 복잡성 및 중량과 비용 등의 복합적인 관계를 가지고 있다. 특히 항공기 착륙에 따른 지상충격하중 및 동적거동은 착륙장치 자체 구성품 뿐만 아니라 장착구조물의 설계 하중으로 적용되는 중요한 설계분야이다. 본 연구에서는 T-50 착륙장치를 모델로 ADAMS를 이용하여 지상 충격하중 및 동적거동을 해석할 수 있는 프로그램을 개발하였다. 항공기 운용/환경조건을 고려한 충격흡수특성 해석은 다양한 설계경험을 토대로 수행하였다. 설계변수 설정, 완충기에 작용하는 내력정의, 운동방정식을 유도하여 착륙 수직속도, 착륙 자세, 착륙 수평속도, 완충효율, 장착위치 작용하중 등을 고려한 해석결과와 동적거동 특성을 분석하고 제시하였다. 이러한 해석 결과를 바탕으로 향후 새로운 착륙장치 개발시 범용적인 해석이 용이할 뿐만 아니라 지상/비행시험의 문제점 발생시 고장탐구 해결에 활용할 수 있다.

연속회분식 반응조에서 생화학흡착제로서 바이오세라믹의 영향에 관한 연구 (A Study on the Effect of Bioceramics as Biochemosorption Material in Sequencing Batch Reactor)

  • 이승환;이슬람;강미아
    • 상하수도학회지
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    • 제20권3호
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    • pp.367-375
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    • 2006
  • Sequencing Batch Reactor (SBR) is well adopted for community wastewater treatment for its simplicity, performance and various advantageous treatment options. SBR is now drawing attention for its process modification such as coupled with membrane bioreactor, reverse osmosis or applying different media to achieve high removal efficiency. This study focused on the improved efficiency of carbon, nitrogen and phosphorous removal by applying zeolite materials called bioceramics to the SBR. Two laboratory-scale SBR units were operated in the same operating conditions - one with bioceramics called Bioceramic SBR (BCSBR) and the other without bioceramics used as control. Routine monitoring of COD, TP, $NH_3-N$, $NO_3-N$ was performed throughout this study. COD removal was about 80% to 100% and phosphorous removal was about 60% in the process whereas $NH_3-N$ removal efficiency was found to be 99.9% in the BCSBR unit. Addition of bioceramics also improved sludge characteristics such as sludge dewaterability, specific gravity and particle size. BCSBR can withstand high ammonia shock loading leading to the better treatment capacity of high ammonia containing wastewater. The cause of improved removal efficiencies within the biological reactor could be attributed to the biochemosorption mechanisms of bioceramics. Absorption/adsorption or desorption capacity of bioceramics was tested through laboratory experiments.