• Title/Summary/Keyword: composite manufacturing process

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Manufacturing Technique of Suspension Insulator far Distribution Lines Using Composite materials (배전급 고분자 현수애자의 제조기술 개발)

  • 홍진영;김영성;지응서;김영찬;백주흠;김동욱
    • Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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    • 1996.11a
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    • pp.306-310
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    • 1996
  • In this paper a series of developing process for an insulator which can be employed in overhead distribution lines, using polymeric composite materials, is introduced. In order to design an insulator for heavily polluted area, weathershed of alternating type was adopted, which could have longer leakage distance. Modified EVA was used as surface material which has good electrical and mechanical characteristics as well as superior chemical stability. FRP core was covered with above surface material through heat shrinking process. By standardization of each process, higher productivity and lower production cost could be ensured. The developed insulator has been put under various tests including long-term field test and artificial aging test and satisfactory results were obtained.

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Research of the Composite Spun Yarn Manufacturing Process using Silicon Carbide and Para Aramid Fiber (SiC/p-Aramid 복합방적사 제조기술 연구)

  • Kim, Booksung;Ryu, Huijun
    • Textile Coloration and Finishing
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    • v.33 no.4
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    • pp.309-316
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    • 2021
  • Due to the rigid nature of the silicon carbide fiber(SiC), fiber damage occurs from the friction during the carding process. This damage not only lowers the spun yarn yield, but also lowers the heat resistance of the spun yarn, so that ultra-high heat resistant yarn cannot be manufactured. Therefore, in the carding process where the most friction between fiber and machine(wire, etc.) occurs, some factors were modified and tested, and as a result of measuring the change in physical properties, fiber damage decreased due to the wire angle or wire density, resulting in improved yield. The test method used to measure the yield of SiC fiber was the carbonization method, and the content of SiC fibers was calculated using the remaining amount after carbonization. Carbonization test was performed at air condition, 700℃, and for 2 hours. Analysis by SEM-EDX showed that the carbide was consistent with the composition of the SiC fiber.

SILICON DIOXIDE FILMS FOR INTERMETAL DIELECTRIC APPLICATIONS DEPOSITED BY AN ECR HIGH DENSITY PLASMA SYSTEM

  • Denison, D.R.;Harshbarger, W.R.
    • Journal of the Korean Vacuum Society
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    • v.4 no.S1
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    • pp.130-137
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    • 1995
  • Deopsition of thermal quality SiO2 using a high density plasma ECR CVD process has been demonstrated to give void and seam free gap fill of high aspect ratio metallization structures with a simple oxygen-silane chemistry. This is achieved by continuous sputter etching of the film during the deposition process. A two-step process is utilized to deposit a composite layer for higher manufacturing efficiency. The first step, which has a deposition rate of approximately 0.5 $\mu$m/min., is used to provide complete gap fill between the metal lines. The second step, which has a deposition rate of up to 1.5 $\mu$m/min., is used to deposit a total thickness of 2.0$\mu$m for the intermetal dielectric film. The topography of this composite film is very compatible with subsequent chemicl mechanical polishing(CMP) planarization processing.

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Prediction of Temperature and Degree of Cure of Carbon Fiber Composites Considering Thermal Chemical Reaction (화학 반응열을 고려한 탄소 섬유 복합재 온도와 경화도 예측)

  • Jae-Woo Yu;Wie-Dae Kim
    • Composites Research
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    • v.36 no.5
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    • pp.315-320
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    • 2023
  • In the manufacturing process of thermosetting carbon fiber composite materials using an autoclave, the internal temperature changes according to the set temperature cycle. This temperature change causes the resin in the composite material to cure. Heat is generated through the chemical reaction of the resin, which can result in a difference between the temperature inside the autoclave and the temperature of the composite material. Previous research assumed that the temperatures of the composite material and the autoclave were the same and analyzed to predict the residual stress and thermal deformation after manufacturing. However, these stresses and deformations depend on the temperature and degree of cure of the composite material. Therefore, this study verifies a thermal-chemical model analysis technique that takes into account the heat generated by the chemical reaction of the resin to accurately calculate the temperature and degree of cure. Additionally, case studies were conducted for different thicknesses to investigate whether this model exhibits similar trends across varying thicknesses.

Effects of Parameters on Abrasion-Resistant Layer of Composite Structure Formed by Evaporation Pattern Casting (소실모형주조법에 의한 내마모 복합조직층 형성에 미치는 공정인자의 영향)

  • Choi, Chang-Young;Mo, Nam-Gyu;Kim, Gun-ho;Yoon, Jong-Cheon;Jung, Yu-Hyun;Kim, Dong-Hyuk;Choi, Yong-Jin;Lee, In-Kyu;Cho, Yong-Jae
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.17 no.2
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    • pp.89-94
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    • 2018
  • Due to industrial advancement and environmental concerns, there is a demand for light-weight material parts with high-performance characteristics. In order to meet this demand, various studies have been conducted on developing high-performance castings to achieve composite features by coating only specific parts that require high performance, with dissimilar joining, rather than coating the entire material part. This study analyzed the possibility of forming a local composite layer on an aluminum alloy through evaporation pattern casting, and the effects of parameters on the aluminum alloy.

The Characteristics and its Development Trends of Thermoplastic Propellants (열가소성 추진제의 특성 및 발전 전망)

  • Kim, Kyung-Moo;Kim, In-Chul
    • Journal of the Korean Society of Propulsion Engineers
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    • v.15 no.3
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    • pp.47-57
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    • 2011
  • All solid rocket propellants are divided in two basic classes according to chemical state: homogeneous(double base) and heterogeneous (composite). Today, composite propellants are extensively used as power sources covering the range from gas generators and small rocket systems to large launch vehicles in space programs. The development of composite rocket propellants in the past was mainly directed to thermoset polymers. But, the thermoset composite propellants have the complication in formulation and fabricating process to adapt to rocket system requirements. In contrast to the thermoset propellant, the PVC plastisols composite propellants have the advantages in the view of loss in manufacturing process, low cost of raw material, and stability of the handling process even though moderate ballistic and mechanical properties. It is predicted that the application field of this class will be used more widely than any other classes.

A Study on Injection Mold Design Using Approximation Optimization (근사 최적화 방법을 이용한 사출금형 설계에 관한 연구)

  • Byon, Sung-Kwang;Choi, Ha-Young
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.19 no.6
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    • pp.55-60
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    • 2020
  • The injection molding technique is a processing method widely used for the production of plastic parts. In this study, the gate position, gate size, packing time, and melt temperature were optimized to minimize both the stress and deformation that occur during the injection molding process of medical suction device components. We used a central composite design and Latin hypercube sampling to acquire the data and adopted the response surface method as an approximation method. The efficiency of the optimization of the injection molding problem was determined by comparing the results of a genetic algorithm, sequential quadratic programming, and a non-dominant classification genetic algorithm.

Minimization of Warpage in Injection-molded Parts By Optimal Design of U-type Ribs (U자형 리브의 최적설계에 의한 사출제품의 휨 최소화)

  • Park, Jong-Cheon;Kim, Kwang-Ho;Kim, Kyung-Mo;Koo, Bon-Heung
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.7 no.1
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    • pp.53-61
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    • 2008
  • In this research, the layout and geometry of U-type ribs in the part, including significant process conditions, are automatically optimized to reduce part warpage with robustness in consideration. The optimization procedure are based on an iterative redesign methodology integrated with computer aided injection molding simulation, Taguchi's Design of Experiment(DOE), and a direct search-based optimization method. The robustness of a design alternative is efficiently measured by introducing composite noise factor and Taguchi's signal-to-noise ratio. As a solution search methodology, the modified design space reduction method based on orthogonal arrays is employed to exploit an optimal robust design alternative. To illustrate the proposed methodology, a case study is performed on simulation results, where an optimal robust design alternative is obtained with a moderate number of iterations.

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Development of Blade Surface Modeling System Using Point Data (점 데이터를 이용한 블레이드 곡면 모델링 시스템 개발)

  • Kim, Yeoung-Il
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.18 no.10
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    • pp.110-115
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    • 2019
  • Stationary and rotating blades can be found in a steam turbine generator and the airfoil shapes of these blades can be defined by point data from an aerodynamic design system. The main design process of blades is composed of two steps: first, the blade surface is modeled with the point data; and then, the section data is generated which contains composite curves with line segments and arcs for CAE of the blade. The surface is modeled by a curve-net defined by the point data, which may be extended to obtain the section data to model the blade. This paper presents methods for automating the above-mentioned steps, which have been implemented in the commercial CAD/CAM system, Unigraphics, with API functions written in C-language. Finally, the proposed methods have been applied to model the blade of a steam turbine generator.

The effect of silica composite properties on DLP-stereolithography based 3D printing (실리카 복합소재의 물성에 따른 DLP 3D printing 적용 연구)

  • Lee, Jin-Wook;Nahm, Sahn;Hwang, Kwang-Taek;Kim, Jin-Ho;Kim, Ung-Soo;Han, Kyu-Sung
    • Journal of the Korean Crystal Growth and Crystal Technology
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    • v.29 no.2
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    • pp.54-60
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    • 2019
  • Recently, various composite materials for additive manufacturing are interested to expand the application field of 3D printing. 3D printing technique was mainly developed using polymer, and ceramic materials for 3D printing are still in the early stage of research due to the requirement of high solid content and post treatment process. In this study, silica particles with various diameters were surface treated with silane coupling agent, and synthesized as silica composite with photopolymer to apply DLP 3D printing process. DLP is an additive manufacturing technology, which has high accuracy and applicability of various composite materials. The rheological behavior of silica composite was analyzed with various solid contents. After DLP 3D printing was performed using silica composites, the printing accuracy of the 3D printed specimen was less than about 3 % to compare with digital data and he bending strength was 34.3 MPa at the solid content of 80 wt%.