• Title/Summary/Keyword: S/A(shock absorber)

검색결과 45건 처리시간 0.022초

충격 흡수기의 동적거동 해석 프로그램을 이용한 각 파라미터가 댐핑력에 미치는 영향 조사 (An Investigation into the Effect of Each Parameter of S/A on the Damping Force Using Dynamic Behaviour Analysis P/G)

  • 박재우;신상윤;주동우;이시복
    • 한국정밀공학회:학술대회논문집
    • /
    • 한국정밀공학회 1996년도 추계학술대회 논문집
    • /
    • pp.371-376
    • /
    • 1996
  • The damping force of shock absorber in an automobile is determined by the components which construct the S/A. In this study we investigate the individual effect of these components on damping force. In addition, opening of important valve doling compression and tension cycle due to up-down reciprocation movement is also researched. Thus we are to strictly control the properties and tolerance of components having important effects on tile damping force and to produce S/A of better quality.

  • PDF

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

  • 김선구;김철;김영만
    • 한국항공우주학회지
    • /
    • 제35권7호
    • /
    • pp.612-618
    • /
    • 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.

경량 피스톤 로드를 위한 마찰용접 적용연구(SM45C/SM45C-Pipe 사용) (A Study on the Friction Welding for Light Piston-Rod(SM45C/SM45C-Pipe))

  • 민병훈;임형택;민택기
    • Journal of Welding and Joining
    • /
    • 제26권2호
    • /
    • pp.55-61
    • /
    • 2008
  • Various research to reduce weight of a car is achieving. This research is tendencious to manufacture solid piston rod of shock absorber as hollow piston rod using friction welding. This study deals with the friction welding of SM45C to SM45C-Pipe that is used in car shock absorber, The friction time was variable conditions under the conditions of spindle revolution of 2,000rpm, friction pressure of 55MPa, upset pressure of 75MPa, and upset time of 2.0seconds. Under these conditions, the microstructure of weld interface, tensile fracture surface and mechanical tests were studied of friction weld, and so the results were as follows. 1. In tensile strength, the hole processing is better than non-hole processing. 2. When the friction time was 1.5seconds under the conditions, the maximum tensile strength of the friction weld happened to be 869MPa, which is 103% of SM45C's tensile strength and 91% of SM45C's Pipe. 3. When the friction time was 2.0seconds under the conditions, the maximum bending strength of the friction weld happened to be 1599MPa, which is 80% of SM45C's bending strength and 118% of SM45C's Pipe.

저속용 피스톤에 가해지는 오일의 속도분포와 정압분포 특성 (A Study on the Features of the Velocity Distribution and the Static Pressure Distribution of Oil on a Low-velocity Piston)

  • 박희재;최재욱;김상도
    • Korean Chemical Engineering Research
    • /
    • 제48권4호
    • /
    • pp.450-456
    • /
    • 2010
  • Shock absorber의 부품인 피스톤을 설계하기 위하여 저속용 피스톤에 가해지는 오일의 속도분포와 정압분포의 특성을 파악하였다. 오리피스를 통과하는 압축속도는 0.0156~0.0642 m/s를 나타났으며, 0.9 mm인 orifice의 속도분포와 정압분포 속도벡터는 속도가 클수록 회전하려는 경향이 커졌다. 0.8 mm인 orifice의 속도분포와 정압분포 속도벡터는 2차적으로 속도가 변하였고 두 번째 압력강하가 발생하였으며, orifice 근처 유선의 분포는 orifice 중심을 기준으로 와류가 발생하였다. 압축실에서 인장실로 통과하는 속도분포는 직경이 작은 orifice에서 속도가 크게 나타났으며, 압축실과 인장실의 압력차가 크면 클수록 피스톤에 작용하는 힘이 크게 나타났다.

Design of Shock Absorber Housing Using Aluminum Vacuum Die Casting Technology

  • Jin, Chul-Kyu;Kang, Chung-Gil
    • 한국산업융합학회 논문집
    • /
    • 제21권1호
    • /
    • pp.1-8
    • /
    • 2018
  • The purpose of this study is to develop a high-strength, high-toughness, thin-walled aluminum shock absorber housing product by applying a high vacuum die casting method to improve internal gas defect and formability. The analysis program dedicated for the casting was used because it was too costly and time-consuming to adopt the gating system design. The final casting plan was designed based on the flow pattern of the material filled into the mold and the result of air pressure and air pocket after the material was completely filled in the mold. Gaty shape was designed as a split type. The runner was designed to have the same shape as the initial inlet curve of the cavity, and the flow of the molten metal was prevented from turbulent flow. The most favorable results were obtained when the injection speed was $V_2=4.0m/s$. Defects on pores were reduced by applying high vacuum level inside the mold.

상용차 운전석의 수동식 가변댐퍼에 대한 동적특성 해석 (Dynamic Characteristics Analysis of A Manually-Controlled Damper for Driver's Seat of Commercial Vehicles)

  • 박재우;백운경;김영호
    • 한국정밀공학회:학술대회논문집
    • /
    • 한국정밀공학회 1995년도 추계학술대회 논문집
    • /
    • pp.518-523
    • /
    • 1995
  • To improve the set comfort of commercial vehicles in various road conditions, it is necessary to design a seat shock absorber which can avoid the vibration zone imposing the discomfort feeling and fatigue on drivers. Through the vibration and dynamic analysis, a shock absorber that has 4 steps of damping ability is developed. Dynamic characteristics analysis of the seat damper is performed considering each valve and oil path for the design purpose.

  • PDF

가변 감쇠를 이용한 충격제어기법의 성능분석 (Performance Investigation of Variable Damping Shock Attenuation Logic)

  • 오현웅
    • 항공우주시스템공학회지
    • /
    • 제7권1호
    • /
    • pp.1-7
    • /
    • 2013
  • Launch vehicles cause several shock events during their lift-off. The excessive shock loads in the several thousands of g's level can results in permanent damage to electronics, optics and other sensitive payload components. The shock can be attenuated by mounting a shock absorber. In this paper, we proposed a semi-active control logic to attenuate the shock so that the input acceleration to main instruments does not exceed the allowable maximum acceleration value. For the performance investigation, two elements model of variable damping and spring stiffness has been used and the analysis results indicate that the proposed semi-active control logic attenuates shock level better than an optimal passive and conventional semi-active on-off control system.

경량화 쇽업소바 피스톤로드에 사용되는 SM45C/SM20C-Pipe의 마찰용접에 관한 연구 (A Study on the Friction Welding of SM45C/SM20C-Pipe which Used in the Light Piston-Rod)

  • 민병훈;최수현;강정식;이형호;민택기
    • 한국공작기계학회논문집
    • /
    • 제17권4호
    • /
    • pp.42-50
    • /
    • 2008
  • Various researches to reduce weight of a vehicle are achieving. One of these researches is tendencious to manufacture the hollow piston rod using friction welding instead of solid one of the vehicle shock absorber. This study deals with the friction welding of SM45C to SM20C-pipe that is used normally in the vehicle shock absorber. The friction time was variable conditions under the conditions of spindle revolution of 2,000rpm, friction pressure of 55MPa, upset pressure of 75MPa, and upset time of 2.0seconds. Under these conditions, the microstructure of weld interface, tensile fracture surface and mechanical tests of friction weld were studied and so the results were as follows. When the friction time was l.5seconds under the conditions, the maximum tensile strength of the friction weld happened to be 837MPa, which is 113% of SM20C's tensile strength and 97% of SM45C's. The optimal welding conditions were n=2,000rpm, $P_1=55MPa$, $P_2=75MPa$, $t_1=1.5sec$, $t_2=2.0sec$ when the total upset length is 1.7mm.

대형 트럭 반능동형 캐빈 공기 현가시스템의 유공압 모델링 및 동특성 해석 (Hydropneumatic Modeling and Dynamic Characteristic Analysis of a Heavy Truck Semi-active Cabin Air Suspension System)

  • 이광헌;정헌술
    • 한국자동차공학회논문집
    • /
    • 제19권2호
    • /
    • pp.57-65
    • /
    • 2011
  • In this paper, a hydropneumatic modeling and dynamic analysis of a heavy truck semi-active cabin air suspension system is presented. Semi-active cabin air suspension system improves driver's ride comfort by controlling the damping characteristics in accordance with driving situation. So it can reduce vibration between truck frame and cabin. Semi-active cabin air suspension system is consist of air spring, leveling valve and CDC shock absorber, and full cabin system are mathematically modelled using AMESim software. Simulation results of components and full cabin system are compared with experimental data of components and test results of a cabin using 6 axis simulation table. It is found that the simulation results are in good agreements with test results, and the hydropneumatic model can be used well to predict dynamic characterics of heavy truck semi-active cabin air suspension system.

Shape and Orifice Optimization of Airbag Systems for UAV Parachute Landing

  • Alizadeh, Masoud;Sedaghat, Ahmad;Kargar, Ebrahim
    • International Journal of Aeronautical and Space Sciences
    • /
    • 제15권3호
    • /
    • pp.335-343
    • /
    • 2014
  • An airbag is an important safety system and is well known as a safety system in cars during an accident. Airbag systems are also used as a shock absorber for UAVs to assist with rapid parachute landings. In this paper, the dynamics and gas dynamics of five airbag shapes, cylindrical, semi-cylindrical, cubic, and two truncated pyramids, were modelled and simulated under conditions of impact acceleration lower than $4m/s^2$ to avoid damage to the UAV. First, the responses of the present modelling were compared and validated against airbag test results under the same conditions. Second, for each airbag shape under the same conditions, the responses in terms of pressure, acceleration, and emerging velocity were investigated. Third, the performance of a pressure relief valve is compared with a fixed-area orifice implemented in the air bag. For each airbag shape under the same conditions, the optimum area of the fixed orifice was determined. By examining the response of pressure and acceleration of the airbag, the optimum shape of the airbag and the venting system is suggested.