• Title/Summary/Keyword: 낙하성능시험

Search Result 54, Processing Time 0.031 seconds

Development of Semi-automatic Cabbage Piling System for Tractor Implemented Chinese Cabbage Hervester (트랙터 부착형 배추 수확기용 반자동식 배추 적재시스템 개발)

  • Song, K. S.;Choi, D. Y.;Hwang, H.
    • Journal of Biosystems Engineering
    • /
    • v.27 no.3
    • /
    • pp.211-218
    • /
    • 2002
  • 배추 생산에 있어서 수확, 운반, 적재 작업은 가장 노동이 집약적으로 요구되는 작업들이다. 최근, 여러 종류의 양배추 수화기가 일본과 유럽에서 개발되었다. 하지만 국내에서 재래되는 배추는 크기와 형태에 있어 양배추와는 달라 기 개발 기종의 도입이 어렵다. 또한 수확작업의 생력화 효과는 운반, 정선, 적재 작업과 밀접하게 연계되어 있어 출하시의 작업체계를 고려하여 수화에 따른 수집.반출 시스템을 개발하여야 한다. 수확시의 배추는 중량이 25~45 N 정도로 다 작물에 비하여 무겁고 부피가 크기 때문에 수확작업의 기계화를 위해서는 수확장치와 더불어 연속적으로 수확되는 배추를 적절하게 수집하여 적재하고 반출하는 시스템의 개발이 중요하다. 본 연구에서는 수확작업의 생력화 효과를 높이고 생력화 시스템 비용의 절감을 목적으로 작업자 1인에 의해 작업할 수 있는 반자동 형태의 트랙터 부착형 배추 수집, 적재, 반출시스템 시작기를 개발하였다. 시작기는 배추 이송장치, 적재장치, 팔렛 및 반출장치의 3개 부분과 PLC를 이용한 주 제어기로 구성하였다. 배추 수집용기로는 대략 70개의 배추를 담을 수 있는 크기가 1,050 mm$\times$1.050mm$\times$1,000mm 인 접이식 메쉬 팔렛을 사용하였으며 하단부에 롤러 안내판을 부착하여 적재한 팔렛의 배출이 용이하도록 하였다. 팔렛을 제외한 전체 시작기의 중량은 235 N 이였으며 크기는 3,940mm$\times$520mm$\times$1,630mm 이었다. 본 연구는 수확장치의 기능 및 생력화 효과를 극대화하고 배추의 손상정도를 최소화하는 시스템을 구성하고자 하였다. 이송장치는 트랙터 부착시 횡공간 점유율을 최소화하도록 하였으며 적재장치는 적재시 배추의 손상을 줄이고 배추가 놓이는 자세를 능동적으로 조절할 수 있도록 주름관을 부착하였다. 시작기의 실내시험 결과 이송장치는 0.18 m/s~0.36 m/s의 범위에서 적재장치는 0.4 m/s~2.4 m/s 범위에서 안정적으로 구동하였으며 두 장치를 동시에 구동하여 시험한 결과 이송장치는 0.26 m/s~0.36 m/s, 그리고 적재장치는 0.9 m/s~2.4 m/s 에서 적정하게 안정적으로 구동하였다. 적재장치의 성능에 있어서 1~3단 적재시에는 주름관을 이용하여 적재하고 4~5단 적재시에는 자유낙하에 의한 적재를 수행할 경우 인력에 의한 적재와 거의 동등한 적재량을 보였으며 손상정도는 거의 무시할 정도였다. 트랙터가 0.3 m/s로 주행하는 경우 노지로부터 배추를 뽑아 이송하는 뽑기벨트의 적정속도가 0.46 m/s인 점을 고려할 때 배추 이송 컨베이어는 0.34 m/s 이상의 속도를 유지할 필요가 있었으며 적재 컨베이어는 2 m/s~2.4 m/s의 속도에서 안정적으로 작동하였다. 배추의 주간 거리가 대략 30~40 cm 인 점을 감안하면 적재장치는 초당 1개의 적재성능을 보였다. 실내에서 수행한 시스템의 성능은 배추에 큰 손상없이 전반적으로 성공적으로 구동하였으나 향후 노면이 고르지 못한 포장에서의 성능 시험이 필요하다.

Sand-Box Evaluation for Vibration-Attenuation of Concrete Panels with Recycled Materials (재활용재 혼입콘크리트 패널의 진동감쇠성에 대한 사조실험)

  • 정영수;최우성;조성호
    • Magazine of the Korea Concrete Institute
    • /
    • v.10 no.4
    • /
    • pp.171-182
    • /
    • 1998
  • Vibration-controlled concrete has been developed by using various concrete mixtures, such as latex, rubber powders, plastic resins and polystyrene(styrofoam). As part of the recycling research of obsolete aged tires and plastic materials, various vibration-reducing mixtures are used for 10 concrete panels having above 200 kg/cm$^2$ in uniaxial compressive strength. Plywood box with sand uniformly saturated by the raining device has been used for the analysis of the impact wave, of which data have been transfered by the FFT technique to comparatively investigate damping ratios of 10 concrete panels.According to wave propagation analysis on vibration-controlled concrete for this research, it can be concluded that Latex concrete has relatively larger damping ratios than those for noncontrolled normal concrete in a similar compressive strength

Low Velocity Impact Property of CF/Epoxy Laminate according to Interleaved Structure of Amorphous Halloysite Nanotubes (비정질 할로이사이트 나노입자의 교차적층 구조에 따른 탄소섬유/에폭시 라미네이트의 저속 충격 특성)

  • Ye-Rim Park;Sanjay Kumar;Yun-Hae Kim
    • Composites Research
    • /
    • v.36 no.4
    • /
    • pp.270-274
    • /
    • 2023
  • The stacking configuration of fiber-reinforced polymer (FRP) composites, achieved via the filament winding process, exhibits distinct variations compared to conventional FRP composite stacking arrangements. Consequently, it becomes challenging to ascertain the influence of mechanical properties based on the typical stacking structures. Thus, it becomes imperative to enhance the mechanical behavior and optimize the interleaved structures to improve overall performance. Therefore, this study aims to investigate the impact of incorporating amorphous halloysite nanotubes (A-HNTs) within different layers of five unique layer arrangements on the low-velocity impact properties of interleaved carbon fiber-reinforced polymer (CFRP) structures. The low-velocity impact characteristics of the laminate were validated using a drop weight impact test, wherein the resulting impact damage modes and extent of damage were compared and evaluated under microscopic analysis. Each interleaved structure laminate according to whether nanoparticles are added was compared at impact energies of 10 J and 15 J. In the case of 10 J, the absorption energy showed a similar tendency in each structure. However, at 15 J, the absorption energy varies from structure to structure. Among them, a structure in which nanoparticles are not added exhibits the highest absorption energy. Additionally, various impact fracture modes were observed in each structure through optical microscopy.

Development of Fracture-Type Protector for a Launching Reconnaissance Robot (발사형 정찰로봇을 위한 파단형 보호체 개발)

  • Kang, Bong-Soo;Cho, Yoon-Ho;Choi, Jeong-Nam
    • Transactions of the Korean Society of Mechanical Engineers A
    • /
    • v.36 no.11
    • /
    • pp.1473-1478
    • /
    • 2012
  • This paper presents the development of a fracture-type protector for carrying a reconnaissance robot to a remote target area. Instead of a conventional unlocking mechanism, a separation method based on the fracture of assembled parts was implemented in the proposed lightweight protector in order to improve the feasibility for a real battlefield. Simulations using the finite element model of the protector and the robot were performed to verify the fracture under the given loading conditions, and shock experiments using a drop table were performed to calculate shock transmittance through the protector to the robot. Several field tests for a 100-m flight proved that the proposed scenario (launching, flying, landing, and separation) was achieved successfully.

Improved Control Algorithm Development for Control Element Drive Mechanism Control System (제어봉구동장치제어계통의 개선된 제어 알고리즘 개발)

  • Kim, Byeong-Moon;Lee, Young-Ryul;Han, Jae-Bok;You, Joon
    • Proceedings of the KIEE Conference
    • /
    • 1995.07b
    • /
    • pp.761-765
    • /
    • 1995
  • The old Timing Controller for Control Element Drive Mechanism (CEDM) is designed as an open loop control system because it is difficult to mount sensors within the Control Element Drive Mechanism(CEDM) which is operating under the pressure boundary of the reactor vessel. In this work new method which can be used to detect the CEDM operational conditions without mounting sensors within the CEDM housing is developed in order to resolve problems of the old Timing Controller. By using the developed new method, the new Timing Controller for the CEDM is designed as a closed loop controller which has features of the control rod drop prevention, fine position control and the coil life time extension. The algorithm developed under closed loop control concept resolves most problems occurred in the old Timing Controller and improves the performance and reliability of the system. During designing and testing of the Timing Controller algorithm, the real time CEDM simulator developed here was used. And all functions of the developed algorithm were verified using CEDM simulator with the real data collected from the site. The results show that the Timing Controller performs its intended functions properly.

  • PDF

GPS Array Antenna Installation On The Rear Missile Body (위성항법 배열안테나의 유도탄 동체 후방 배치)

  • Park, Bumsoo;Ahn, Woogeun;Lee, Jangyong;Ko, Duck kon
    • Journal of Advanced Navigation Technology
    • /
    • v.26 no.1
    • /
    • pp.9-14
    • /
    • 2022
  • In this paper we investigate the advantages when the GPS Antenna is installed on the rear missile body. In conventional design the GPS antenna locates on the front part of missile. However it causes degraded GPS positioning performance since the missile body blocks the GPS signals. This paper proposes the GPS array antenna design which locates on the rear part of missile body and has the tilted antenna patches to achieve the maximum area of receiving GPS signals. We simulate LOS region of receiving signals and conducted anechoic chamber test to define the effective signal receiving region. And we conduct field test and flight test to check out the enhancement of signal receiving area.

Evaluation of the Basic Properties of Concrete with Types of Cellulose Fibers (셀룰로오스 섬유 종류에 따른 콘크리트의 기초 물성 평가에 관한 연구)

  • Park, Yong-Kyu;Lee, Joo-Hun;Jeon, In-Ki;Kim, Hyun-Woo;Yoon, Ki-Woon
    • Journal of the Korea Institute of Building Construction
    • /
    • v.11 no.5
    • /
    • pp.419-425
    • /
    • 2011
  • Topping concrete that is not reinforced with rebar to prevent poor tensile performance is vulnerable to cracking. In this study, jute, which is known to be an excellent natural fiber material for strengthening concrete performance, was compared with other cellulose fibers in terms of its capacity to reduce the cracking of concrete. As a result, it was found that compared with concrete using other fibers, concrete using jute fiber showed more than a 50 % reduction of plastic shrinkage crack resistance with the contents of 0.9 kg/$m^3$ and 1.2 kg/$m^3$ for. For impact strength tests, the final destruction of WF and PULP fibers took up to 5 times the number of falls, while jute has 10-18 circuitry, showing excellent ductility properties.

Study on the Shape of Appendage for the Reduction of Motion of Floating Wind Turbine Platforms (부유식 풍력 하부구조물의 운동 저감을 위한 부가물 형상 연구)

  • Dae-Won Seo;Jaehyeon Ahn;Jungkeun Oh
    • Journal of the Korean Society of Marine Environment & Safety
    • /
    • v.28 no.7
    • /
    • pp.1201-1208
    • /
    • 2022
  • In general, to maximize the supply and efficiency of floating offshore wind power generation energy, the motion caused by wave attenuation of the substructure must be reduced. According to previous studies, the motion response was reduced due to the vortex viscosity generated by the damping plate installed in the lower structure among the waves. In this study, a 5 MW semi-submersible OC5 platform and two platforms with attenuation plates were designed, and free decay experiments and numerical calculations were performed to confirm the effect of reducing motion due to vortex viscosity. As a result of the model test, when the heave free decay tests were conducted at drop heights of 30 mm, 40 mm, and 50 mm, compared with the OC5 platform, the platform with two types of damping plates attached had relatively improved motion damping performance. In the model test and numerical calculation results, the damping plate models, KSNU Plate 1 and KSNU Plate 2, were 1.1 times and 1.3 times lower than OC5, respectively, and the KSNU Plate 2 platform showed about two times better damping performance than OC5. This study shows that the area of the damping plate and the vortex viscosity are closely related to the damping rate of the heave motion.

Experimental Ignition Delay Assessment of H2O2 Based Low Toxic Hypergolic Propellants with Variation of Reactive Additive Concentration (반응성 첨가제 농도에 따른 과산화수소 기반 저독성 접촉점화성 추진제의 점화지연 시험평가)

  • Rang, Seongmin;Kim, Kyu-Seop;Kwon, Sejin
    • Journal of Aerospace System Engineering
    • /
    • v.14 no.3
    • /
    • pp.24-31
    • /
    • 2020
  • A study on the H2O2 based low toxic hypergolic propellant was conducted. The fuel candidates were chosen as a mixture of Amine solvent and reactive additive. The analytical performance was calculated via the NASA CEA code and 96% Isp of the NTO/UDMH was confirmed. The ignition delay measurement with drop test was performed and all candidates showed less than 10 ms in the best performance cases. Based on these results, the feasibility of high response H2O2 based low toxic hypergolic propellant was confirmed.

Separation Device Development and Flight Test for Marine Recovery of Scientific Balloon (과학기구 기낭의 해상 회수를 위한 분리장치 개발 및 비행시험)

  • Shim, Gyujin;Kang, Jungpyo;Kim, Hweeho;Yee, Kwanjung
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.47 no.1
    • /
    • pp.49-58
    • /
    • 2019
  • The Scientific balloon is a flight system that could recover an entire platform at the end of the mission. The recovery takes place mainly in low-density populated areas, taking into account for the possible damage to the human life and public safety. In Republic of Korea, on the other hand, marine recovery should be considered due to the dense mountainous terrain and restrictions of the peninsula. In this operating environment, the envelope must be recovered because of severe marine pollution that may occur after the splashdown. Therefore, in this study, the separation device that consists of a location tracker and the waterproof system were developed. The device includes data transmission/reception, separation, and waterproof systems which are manufactured considering the environmental condition of the Korea. The performance of the device and the trajectory of the envelope were verified by conducting a separation test of a 20km platform at a target altitude and the recovery of the zero-pressure balloon.