• Title/Summary/Keyword: 열선 절단

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Development of Multi-functional Hotwire Cutting System using EPS-foam (발포 폴리스티렌 폼을 이용한 다기능 열선절단장치 개발)

  • 이상호;김효찬;양동열;박승교;김찬국
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2004.10a
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    • pp.1414-1417
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    • 2004
  • A thick-layered RP process, transfer-type variable lamination manufacturing using expandable polystyrene foam (VLMST) has been developed to have the advantageous characteristics such as high building speed, low cost for introduction and maintenance of VLM-ST apparatus, and little staircase surface irregularities of parts. However, VLM-ST has difficulty fabricating an axisymmetric shape and a large-sized freeform shape because of the limited sloping angles and small build size. The objective of this paper is to develop a multi-functional hotwire cutting system using EPS-foam (MHC). MHC employs a four-axis synchronized hotwire cutter with the structure of two XY movable heads and a turntable. In order to examine the applicability of the developed MHC apparatus, an axisymmetric shape, a polyhedral shape and a large-sized freeform shape were fabricated on the apparatus.

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Effects of Cutting Angle on Kerf width and Edge Shape in the Hotwire Cutting of EPS Foam for the Case of Single-Sloped Cutting for VLM-s Process (VLM-s 공정을 위한 EPS 폼의 단순 경사 열선 절단시 절단 경사각이 절단폭과 모서리 형상에 미치는 영향)

  • 안동규;양동열
    • Journal of Welding and Joining
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    • v.21 no.5
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    • pp.525-533
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    • 2003
  • The dimensional accuracy and global roughness between successive layers of VLM-s, which is a new rapid prototyping process using hotwire cutter and EPS foam, depend significantly on the operating parameters of hotwire cutter. In the present study, the effect of cutting angle on the kerf width and edge shape in hotwire cutting of EPS foam for the case of single-sloped cutting with one cutting angle was investigated. Through single-sloped cutting tests, the modified relationship between kerf width and effective heat input, considering the effect of the cutting angle, and the relationship between the melted area and the cutting angle were obtained. In order to investigate the effect of cutting angles on the thermal field in EPS foam, transient heat transfer analyses using single-sloped volumetric heat flux model and locally-conformed mesh were performed. Through the comparison between experimental and numerical results, it was shown that the proposed analysis model is needed to estimate the three-dimensional temperature distribution of the EPS foam for the case of single-sloped hotwire cutting.

Thermal Vacuum Test and Thermal Analysis for a Qualification Model of Cube-satellite STEP Cube Lab. (큐브위성 STEP Cube Lab.의 임무 탑재체 인증모델의 열진공시험 및 열모델 보정을 통한 궤도 열해석)

  • Kang, Soo-Jin;Ha, Heon-Woo;Han, Sung-Hyun;Seo, Joung-Ki;Oh, Hyun-Ung
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.44 no.2
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    • pp.156-164
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    • 2016
  • Qualification model(QM) of main payloads including concentrating photovoltaic system using fresnel lens, heating wire cutting type shockless holding and release mechanism, and MEMS-based solid propellant thruster have been developed for the STEP Cube Lab.(Cube Laboratory for Space Technology Experimental Project), which is a pico-class satellite for verification of core space technologies. In this study, we have verified structural safety and functionality of the developed payloads under a qualification temperature range through the QM thermal vacuum test. Additionally, a reliability of thermal model of the payloads has been confirmed by performing a thermal correlation based on the thermal balance test results.

Preliminary System Design of STEP Cube Lab. for Verification of Fundamental Space Technology (우주기반기술 검증용 극초소형 위성 STEP Cube Lab.의 시스템 개념설계)

  • Kwon, Sung-Cheol;Jung, Hyun-Mo;Ha, Heon-Woo;Han, Sung-Hyun;Lee, Myung-Jae;Jeon, Su-Hyeon;Park, Tae-Young;Kang, Su-Jin;Chae, Bong-Gun;Jang, Su-Eun;Oh, Hyun-Ung;Han, Sang-Hyuk;Choi, Gi-Hyuk
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.42 no.5
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    • pp.430-436
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    • 2014
  • The mission objective of STEP Cube Lab. (Cube Laboratory for Space Technology Experimental Project) classified as a pico-class satellite is to verify the technical effectiveness of payloads such as variable emittance radiator, SMA washer, oscillating heat pipe and MEMS based solid propellant thruster researched at domestic universities. In addition, the MEMS concentrating photovoltaic power system and the non-explosive holding and separation mechanism with the advantages of high constraint force and low shock level will be developed as the primary payloads for on-orbit verification. In this study, the feasibility of the mission actualization has been confirmed by the preliminary system design.