• Title/Summary/Keyword: Bushing

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절연시험논고

  • 노은래
    • 전기의세계
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    • v.16 no.2
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    • pp.39-46
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    • 1967
  • 절연시험방법은 여러가지 있으나 이들은 공장에서 또는 특수한 시설을 갖추지 않고는 어려운 경우가 대부분이므로 이에 현장에서 또는 연재 전력을 사용하는 공장및 발변전소가 갖이고 있는 계측기류와 절연시험기(megger)등을 사용하여 발전기 전동기등의 절연의 절연물에 대한 절연도및 cable과 고압 Bushing의 절연도를 결정하므로써 예방설비의 실효를 거두어 전기기기관리의 적정을 기하기 위하여 그 기술과 방법을 고안검토하고져 한다.

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Multistage Cold Forging Process Design of Al6082 Considering Forming Limit (Al6082의 가공한계를 고려한 냉간단조 공정설계)

  • Ann, Ku-Hee;Kang, Jong-Hun;Heo, Su-Jin;Shin, Tae-soo;Cho, Hae-Yong
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.19 no.9
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    • pp.93-99
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    • 2020
  • Recently, as the weight reduction of vehicles has been actively progressed, parts developed using aluminum 60XX series from existing steel materials are increasing. In this paper, the bushing used for the front frame rail, which is one of the parts for fixing engines and other parts in automobiles, was changed to an aluminum material of the Al60XX series, and it was intended to be produced by applying of cold forging method. The bushing is a part that secures the engine frame, and in order to produce it by cold forging, the molding limit is predicted through process design, and a multi-stage process is designed through finite element analysis. In addition, in order to verify the feasibility of the designed forging process, the limits of the multi-step process were verified based on the Cockcroft Latham theory, and the crack and overlap of the actual forging work were predicted and improved.

On the Instantaneous and Average Piston Friction of Swash Plate Type Hydraulic Axial Piston Machines

  • Jeong, Heon-Sul;Kim, Hyoung-Eui
    • Journal of Mechanical Science and Technology
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    • v.18 no.10
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    • pp.1700-1711
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    • 2004
  • Piston friction is one of the important but complicated sources of energy loss of a hydraulic axial piston machine. In this paper, two formulas are derived for estimating instantaneous piston friction force and average piston friction moment loss. The derived formula can be applicable for piston guides with or without bushing as well as for axial piston machines of motoring and pumping operations. Through the formula derivation, a typical curve shape of friction force found from several experimental measurements during one revolution of a machine is clearly explained in this paper that it is mainly due to the equivalent friction coefficient dependent on its angular position. Stribeck curve effect can easily be incorporated into the formula by replacing outer and inner friction coefficients at both edges of a piston with the coefficient given by Manring (1999) considering mixed/boundary lubrication effects. Novel feature of the derived formula is that it is represented only by physical dimensions of a machine, hence it allows to estimate the piston friction force and loss moment of a machine without hardworking experimental test.

Nondestructive Evaluation of the Defects in Composite-sintered Bushes Using Ultrasonics

  • Im, Kwang-Hee;Kim, Ki-Youl;Shin, Ki-Taek;Lee, Han-Hee;Jung, Il-Woong;Kang, To;Cho, Hyun-Joon
    • Journal of the Korean Society of Manufacturing Technology Engineers
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    • v.21 no.6
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    • pp.1013-1017
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    • 2012
  • Advanced composite-sintered bushings are widely utilized in the areas of excavators and injection molding machines as a journal bearing. Since the bearings are mainly used under high loads, service life should be long and the stored oil of inner bushings has to be continually fed into the bearing. The composite-sintered bushings are consisted of the two different materials; outer steel materials and inner porous sintered materials respectively. High temperature diffusion bonding has been applied for holding the both materials of the bushing together. Therefore, it is very important that the bonding reliability has to be assured and evaluated in manufacturing process. Finite element method (FEM) is performed in order to evaluate the minimum allowable flaw sizes that are possibly generated in the composite-sintered bushings. Additionally, the composite-sintered bushings were undergone ultrasonic C-scan tests to find out the size of inherent flaws through artificially simulated UT signal analysis.

A Test Bench with Six Degrees of Freedom of Motion For Development of Small Quadrotor Drones (소형 쿼드로터 드론 개발을 위한 6 자유도 운동 실험 장치)

  • Jin, Jaehyun;Jo, Jin-Hee
    • Journal of Aerospace System Engineering
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    • v.11 no.1
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    • pp.41-46
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    • 2017
  • A new test bench for small multi-rotor type drones has been developed. Six degrees of freedom (DOF) motion is possible due to a ball bushing, wheels, and rotating plates. An FPGA (field programmable gate array) based controller, that supports realtime parallel processing, is used to measure attitude with an accelerometer and a gyro to adjust motor speed. Several tests were performed to check the operational properties of the test bench and the controller. The results show that this test bench is proper for verifying controllers and the control methods of small multi-rotor drones.

The Deterioration Properties and Actual Conditions of Insulation Cover used at 22.9 kV Transformer Bushing (22.9 kV용 변압기 부싱 절연 커버의 실태 조사 및 열화 특성)

  • Choi, Chung-Seog;Kim, Hyang-Kon;Han, Woon-Ki;Lee, Ki-Yeon
    • Fire Science and Engineering
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    • v.20 no.3 s.63
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    • pp.35-41
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    • 2006
  • In this study, we presented the problems in the insulation cover of 22.9kV transformer bushing through investigating actual conditions. After thermal stress applied to the insulation cover, deterioration patterns, thermogravimetric and infrared characteristics were analyzed, and the results were applied to the cause analysis of accidents and judgement of safety. The insulation covers are used to protect exposed terminals of transformer, but they had improper size and length. Therefore, they could not show efficient insulation function. In case that thermal stress of $150^{\circ}C$ was applied to the insulation covers, plastic insulation covers(A, B, D, E) damaged severely, whereas rubber insulation cover(C) showed normal shapes. In the result of thermogravimetric analysis, the thermal gravity of plastic covers(A) decreased about 33.3% at $307.8^{\circ}C\;to\;405.9^{\circ}C$. and he thermal gravity of rubber covers (C) decreased about 53.7% at $258.8^{\circ}C\;to\;32.9^{\circ}C$. In the result of FT-IR analysis, plastic covers showed peaks characteristic of $CH_2,\;CH_3$, C=O and C=C bonds, whereas rubber covers showed peaks characteristic of OH, $CH_2,\;CH_3$, C=O, C=N and C=C bonds.