• 제목/요약/키워드: Ring Flange

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Cuticle Micromorphology of Korean Gymnosperms I. Cycadaceae, Ginkgoaceae, Taxaceae and Cephalotaxaceae

  • Sung Soo Whang
    • Journal of Plant Biology
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    • v.38 no.2
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    • pp.181-193
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    • 1995
  • Cuticle micromorphology of four families of Korean gymnosperms, Cycadaceae, Ginkgoaceae, Taxaceae, and Cephalotaxaceae, were studied with scanning electron microscopy. The outer and inner features of abaxial and adaxial cuticles were described in details; the absent or present of Florin ring, orifice, trichome, and plug and their shape, the shape and periclinal and anticlinal wall sculpture of epidermal cells, the shape of cuticular flange of epidermal cell, guard cell, and subsidiary cell, the number of stomatal bands and rows, and stomatal apparatus including the shape of polar extension, number of subsidiary cells, the sculpture of guard cell and subsidiary cell. Most of these features have not been sufficiently substantiated by the previous reprots. Furthermore, all the species investigated showed distinctive cuticle morphology with morphological and taxonomical informations.

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A Study on Pylon Cable Anchor System in Cable-Stayed Railway Bridge (철도용 사장교의 주탑 케이블 정착부에 관한 연구)

  • Han, Sung-Gwan;Gong, Byung-Seung
    • Proceedings of the KSR Conference
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    • 2006.11b
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    • pp.565-580
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    • 2006
  • Set in constant increase and period current of lively technical development of railroad use and construction of cable stayed bridge railway bridge, one of bridge form of most suitable that think side police officer and the material enemy of bridge that use long rail, is increasing laying stress on the foreign countries. Main tower fixing department of this cable stayed bridge is consisted of main tower flange that support bearing plate, bay ring plate bearing plate, support end rib and diaphragm etc, as stress transmission mechanic that tensility of cable socket into normal force of main tower, and is used this time. These structural elements is very complex the structure and direction of load delivered from socket specially calbe particularly be different, and need FEM analysis that use Thick Shell element for suitable arrangement of mutual stress flowing grasping and absence that follow hereupon because all of the each support plate angle that suport this differ.

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Evaluation of Boundary Conditions for Structural Analysis of Wheel Bearing Units (Wheel Bearing Unit의 구조해석을 위한 경계조건 설정에 관한 연구)

  • 김기훈;유영면;임종순;현준수
    • Transactions of the Korean Society of Automotive Engineers
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    • v.8 no.6
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    • pp.230-237
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    • 2000
  • The wheel bearing in vehicles has been improved to unit module by joining a bearing to a hub in order to achieve weight reduction and easy assembly. Currently, the contact force between a raceway and balls of a bearing is applied as the external force in order to analyse the structure of the unit type bearings. In this paper, simplified boundary conditions are discussed for structure analysis of wheel bearing unit. From the procedure, the contact conditions of balls and race in wheel bearing unit are considered as equivalent non-linear spring elements. The end node of a spring element is constrained in displacement. And the external force of boundary conditions is applied at the contact point between tire and road. For the evaluation of this analysis, its results for the force of spring elements are compared with contact forces of calculated results. and also maximum equivalent stresses of analysis are compared with results of test at the flange of inner ring. The analysis results with proposed boundary conditions are more accurate than results from analysis which is generally used.

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Failure Examples Study for Tribological Characteristics of Drive Shaft and Axle System in Vehicles (자동차 드라이브 샤프트와 액슬 시스템의 트라이볼로지적인 특성에 관한 고장사례 고찰)

  • Lee, Il Kwon;Moon, Hak Hoon;Youm, Kwang Wook
    • Tribology and Lubricants
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    • v.29 no.6
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    • pp.397-402
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    • 2013
  • This study examined the tribological characteristics of the drive shaft and axle system in vehicles. The first drive shaft example contained end play for a CV joint that transferred part of the transmission power to the wheel. The joint part of the drive shaft was deformed because of reduced durability due to wear. Thus, vibrations caused the body to shake and become unbalanced when the drive shaft transferred the power. The second example was the cross-section of a shaft that connected the slip-connection of the propeller shaft on the input side to the yoke flange of the output side; the durability was reduced because of corrosion. End play caused by wear between the bearing and cross-section shaft appeared to cause shaking. In the third example, a grease leak reduced lubrication and thus caused damage to the hub bearing and inside the knuckle. The failure was produced by sticking. The fourth example had noise produced by the gear and gear transfer. This was due to the backlash of the pinion and few ring gears for the differential gear. Therefore, drive shaft and axle systems must be thoroughly checked and managed to minimize and reduce failure phenomena.

Microstructural Evolution of the Al 7175 alloy forgings (알루미늄 7175합금의 단조재의 미세조직 발달)

  • 이용연;임성택;손영일;이경훈;은일상
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 1997.11a
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    • pp.27-27
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    • 1997
  • 최근 미사일 추진기관 및 기체 구조재로 사용되는 알루미늄 7175 합금의 형상의 변화와 제조공정 변화에 따른 미세조직 변화에 대하여 고찰하였다. 구조체는 사용처에 따라 Flange Type 또는 Ring Type 등으로 형상이 다양하므로 단조 조건과 제품의 위치에 따라 균일한 물성을 획득하기는 매우 어려운 숙제이다. 본 연구에서는 균일한 물성을 얻기 위한 여러 가지 제조 공정의 변화를 모색하였으며, 제조된 단조재의 미세조직을 통하여 물성과의 연관성을 검토하였다. 적용된 공정은 통상의 열간 단조공정, 아 결정립 미세화공정, 재 결정립 미세화 공정 등이며 단조재의 형상과 동일 부품에서도 부위에 따라 변형량이 다르므로 미세조직의 변화가 다르게 나타났다. 아결정립과 재결정립 미세화 공정은 제품의 형상에 따라 내·외부 결정립이 크기가 크게 변화되었다. 이는 내·외부에 재료에 축적되는 에너지의 양과 외적으로 가해지는 기계적 에너지 및 열적 에너지가 다르기 때문이며, 변형량이 큰 부분의 미세 석출물의 크기가 변형량이 적은 부분의 석출물보다 크게 감소됨은 준안정상이 기계적 에너지가 변형열에 의한 열에너지로 변환됨에 따라 상석출에 영향을 미친 것으로 판단된다. 이와 같은 결과는 미세 조직 제어가 알루미늄합금 단조재의 공정설계의 중요한 인자임을 재 확인시켜 주는 것으로 재료의 신뢰성이 필수적으로 요구되는 추진기관의 중요 부품에 적극 고려해야 할 요소라 할 수 있다.

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Design Optimization of CRDM Motor Housing

  • Lee, Jae Seon;Lee, Gyu Mahn;Kim, Jong Wook
    • Journal of Magnetics
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    • v.21 no.4
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    • pp.586-592
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    • 2016
  • The magnetic-jack type CRDM withdraws or inserts a control rod assembly from/to the reactor core to control the core reactivity. The CRDM housings form not only the path of the electromagnetic field but also the pressure boundary of a nuclear reactor, and a periodic in-service inspection should be carried out if there are welded or flange jointed parts on the pressure boundary. The in-service inspection is a time-consuming process during the reactor refueling, and moreover it is difficult to perform the inspection over the reactor head. A magnetic motor housing is applied for the current SMART CRDM and has several welding joints, however a nonmagnetic motor housing with fewer or no welding joints may improve the operational efficiency of the nuclear reactor by avoiding or simplifying the in-service inspection process. Prior to the development, the magnetic field transfer efficiency of the nonmagnetic housing was required to be assessed. It was verified and optimized by the electromagnetic analysis of the lifting force estimation. Magnetic flux rings were adopted to improve the efficiency. In this paper, the design and optimization process of a nonmagnetic motor housing with the magnetic flux rings for the SMART CRDM are introduced and the analyses results are discussed.

Improvement of Flight Safety by Horizontal Stabilizer Design Improvement of Rotorcraft (회전익 항공기 수평 안정판의 설계 개선을 통한 비행 안전성 향상)

  • Lee, Yoon-Woo;Kim, Dae-Han;Jang, Min-Wook;Hyun, Young-Jin;Lee, Sook
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.20 no.6
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    • pp.134-141
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    • 2019
  • This paper is a study on design improvement of rotorcraft horizontal stabilizer. The rotorcraft horizontal stabilizer stabilizes the behavior of the pitch, yaw, etc. from the aircraft. Because of this role, horizontal stabilizers are a major component (Flight Safety Part) that affects flight safety on rotorcraft. However, when the rotorcraft was operated in domestic, cracks were found in the inner structure of the horizontal stabilizer and design improvement was needed. In this paper, we identified the two causes of the horizontal stabilizer crack defects through fracture analysis and structural analysis. The first is the tightening torque when the bolt is tightened, and the second is the lead-lag behavior of aircraft. In order to improve these two causes, bolt fastening method, flange structure and thickness were changed and composite ring was applied. In order to verify the design improvement, the structural analysis was performed and the structural strength was improved. Also Fatigue analysis of the internal structure (Rib 1) was performed and it was confirmed that the requirements were satisfied.