• Title/Summary/Keyword: moving core surface heating

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Effects of the mold surface heating methods for the DVD stamper with nano pattern on the transcription of the injection molded parts using COC and PMMA plastics (나노패턴을 갖는 DVD용 스템퍼의 표면가열방식이 COC, PMMA 수지를 이용한 사출성형품의 전사성에 미치는 영향)

  • 김동학;유홍진;김태완
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.5 no.3
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    • pp.218-222
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    • 2004
  • We developed the stamper structured mold with moving core type with nano pattern. Among the factors affecting the quality of injection molding plastic parts, We studied the effects of moving core surface heating method on the transcription of injection molding plastic parts with nano structures. Moving core surface heating has been tested by three different methods. The first was conventional injection molding process without heating moving core surface, the second was halogen lamp radiation heating process and the last was MmSH process using gas flame. As a result of making injection molded parts by using thermoplastic amorphous resins such as COC, PMMA, MmSH method which is the most high temperature of moving core surface showed the best nano pattern transcription of the three methods, but the outcome of conventional injection molding process was not better than others.

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Study on the Performance of Infrared Thermal Imaging Light Source for Detection of Impact Defects in CFRP Composite Sandwich Panels

  • Park, Hee-Sang;Choi, Man-Yong;Kwon, Koo-Ahn;Park, Jeong-Hak;Choi, Won-Jae;Jung, Hyun-Chul
    • Journal of the Korean Society for Nondestructive Testing
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    • v.37 no.2
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    • pp.91-98
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    • 2017
  • Recently, composite materials have been mainly used in the main wings, ailerons, and fuselages of aircraft and rotor blades of helicopters. Composite materials used in rapid moving structures are subject to impact by hail, lightning, and bird strike. Such an impact can destroy fiber tissues in the composite materials as well as deform the composite materials, resulting in various problems such as weakened rigidity of the composite structure and penetration of water into tiny cracks. In this study, experiments were conducted using a 2 kW halogen lamp which is most frequently used as a light source, a 2 kW near-infrared lamp, which is used for heating to a high temperature, and a 6 kW xenon flash lamp which emits a large amount of energy for a moment. CFRP composite sandwich panels using Nomex honeycomb core were used as the specimens. Experiments were carried out under impact damages of 1, 4 and 8 J. It was found that the detection of defects was fast when the xenon flash lamp was used. The detection of damaged regions was excellent when the halogen lamp was used. Furthermore, the near-infrared lamp is an effective technology for showing the surface of a test object.