• Title/Summary/Keyword: 인장시험시편

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Effects of Microcapsules on Mechanical Properties and Thermal Stability of Microcapsule Embedded Polymeric Resins (마이크로캡슐이 폴리머 수지의 기계적 특성 및 열안정성에 미치는 영향)

  • Yoon, Sung Ho;Kim, Min Sik;Jang, Se Yong
    • Composites Research
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    • v.28 no.5
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    • pp.316-321
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    • 2015
  • This study investigated the effects of microcapsules on mechanical properties and thermal stability of the composite material containing self-healing microcapsules. To this end, tensile specimens and flexural specimens containing melamine-urea-formaldehyde (M-U-F) shell walled microcapsules with diameters of $70{\sim}130{\mu}m$ were manufactured. Varying amount of microcapsules in the specimens was considered: 0 wt%, 0.5 wt%, and 1.0 wt%. The tensile and flexural tests were conducted to evaluate mechanical properties of the specimens containing the microcapsules and the thermogravimetric analysis test was performed to evaluate the thermal stability of the specimens containing the microcapsules. The results show that the tensile strength of the specimens was sensitive to the amount of the microcapsules compared to the tensile modulus even though the tensile modulus of the specimens was not significantly affected by the amount of the microcapsules. However, reduction of the tensile strength was not linearly proportional to the amount of microcapsules; similar results were observed in the flexural test. The weight changes of the specimens containing the microcapsules, as a function of temperature, were similar to those specimens without microcapsules. The thermal stability of the specimens was not affected significantly by the microcapsules embedded in the specimens.

Mechanical Properties of 3D Printed Composite Material on Various Thermal Environment (다양한 온도 환경에 따른 3D 프린트 복합재료의 기계적 물성 평가)

  • Sang-Hun Kang;Do-Hyeon Kim;Hyoung-Seock Seo
    • Composites Research
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    • v.36 no.3
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    • pp.193-198
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    • 2023
  • Currently, there are many discussions about composite materials and 3D printed composite material to weight reduction of ships. A test was conducted to confirm the applicability of the 3D printed composite material to ships and offshore structures by linking the 3D printing technology with excellent productivity and the composite material with corrosion resistance and lightweight characteristics in salt water environments. In order to apply the 3D printed composite material used in this paper to ships and offshore structures, the temperature environmental effects that can be exposed in the marine environment should be considered. Therefore, the tensile test was conducted with specimen of Carbon + Onyx, Carbon + Nylon, HSHT glass + Onyx, HSHT glass + Nylon material in low temperature (-50℃), room temperature (20℃), and high temperature (50℃) environments that can be exposed to the marine environment. As a result of the tensile test, the carbon + onyx specimen showed the highest tensile strength and the HSHT glass + onyx specimen showed the highest tensile strain. In addition, by analyzing the tested specimens, the failure mode of the 3D printed composite material specimens exposed to various temperature environments was analyzed.

Moisture Absorption and Strengths of Composite Skins cured on the Close Heated Mold (폐쇄형 가열 금형에서 경화된 복합재 외피의 수분흡수 및 강도특성)

  • Kyung-Su Kim;Hyeon-Seok Choe;Byeong-Su Kwak;Jin-Hwe Kweon
    • Composites Research
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    • v.37 no.2
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    • pp.126-131
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    • 2024
  • The moisture absorption rate and structural strength changes of oven-cured composite skin based on closed molds were studied. Moisture absorption was performed on specimens with and without filler applied. The specimens were exposed to moisture for up to 231 days. Tensile and compression tests were conducted with and without filler application. As a result of the test, the moisture absorption rates of the tensile and compressive specimens without filler were 2.4 and 0.3% higher, respectively, than those with the filler applied. The tensile and compressive strengths of the specimen without filler applied were average 305 MPa and 139 MPa, respectively, and the tensile and compressive strengths of the specimen with filler applied were 313 MPa and 166 MPa, respectively, appeared high.

Study on Tensile Properties of Polyamide 12 produced by Laser-based Additive Manufacturing Process (레이저 적층제조기술로 제작한 폴리아미드 12 시편의 인장특성 연구)

  • Kim, Moosun
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.20 no.11
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    • pp.217-223
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    • 2019
  • The application of 3D printing technology is expanding due to the production of the complex-shape parts and the one-step manufacturing process. Moreover, various technical solutions in 3D printing are emerging through continuous research and development. Representative technologies include SLS technology, in which a desired area is sintered and laminated by irradiating a powder-type material with a laser. In addition, high-performance engineering plastic parts are being manufactured in increasing numbers. In this study, tensile specimens were fabricated from polyamide 12, a widely available polymer, and the glass bead-reinforced polyamide 12. The specimen-build orientation was divided into 0°, 45°, and 90° on the fabrication platform, and the tensile test temperature was -25℃, 25℃, and 60℃. The test results showed that the tensile modulus of both materials decreases as the build orientation becomes closer to 90°. In addition, the tensile strength of glass bead-reinforced PA12 showed more dependence on the build orientation than PA12. In addition, the tensile modulus and tensile strength decreased with increasing test temperature.

Compression Test of Subelement and Tension Test of Hoop Ring for Stiffness Evaluation of Conical Composite Lattice Structures (콘형 복합재 격자 구조의 강성 평가를 위한 Subelement의 압축 시험 및 후프 링의 인장 시험)

  • Jeon, Min-Hyeok;Kong, Seung-Taek;No, Hae-Ri;Kim, In-Gul;Lee, Sang-Woo
    • Composites Research
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    • v.33 no.3
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    • pp.169-175
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    • 2020
  • The compression and tension test were performed to evaluate the stiffnesses of the conical composite lattice structures and results of test were compared with finite element analysis results. Because of difficulty to perform simple tension and compression test due to conical shape, suitable specimens and jig for test were made. Subelements extracted from the structure were prepared for compression test. Compression test of subelement was performed and compressive strains in fiber direction were measured. Compressive stiffness of the helical rib was verified by finite element analysis results. For stiffness of hoop rib, hoop ring specimens were extracted from the structure. Tension test of hoop ring specimen was performed to apply bending deformation to hoop rib. Stiffness of hoop rib was verified by finite element model considering various fiber volume fraction in thickness direction.

조사재시험시설 핫셀에서의 원자로 감시시편 시험기술개발

  • 안상복;이기순;박대규;주용선;김병철
    • Proceedings of the Korean Nuclear Society Conference
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    • 1998.05b
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    • pp.111-117
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    • 1998
  • 원자로 압력용기는 운전기간 동안 중성자 조사에 따른 재료의 기계적 성질이 변화되므로, 용기의 건전성 유지여부를 평가하기 위하여 조사시편을 이용한 주기적인 감시시험이 요구된다. 그러나 감시시편은 방사성 물질로서 일반 환경조건에서 시험이 불가능하다. 따라서 국내의 자력기술로 완공된 조사재시험시설의 핫셀 내에서 감시시험의 주요항목인 온도감시자, 충격, 인장, 파괴인성, 그리고 성분분석 등에 대한 시험을 수행하기 위하여 관련된 규정에 합하도록 장비 및 시험 평가기술을 개발하였다.

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Aluminum autobody technology for the '90 (90년대의 Al 차체 기술)

  • 박석완;권순용;조원석
    • Journal of the korean Society of Automotive Engineers
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    • v.15 no.1
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    • pp.3-8
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    • 1993
  • 본 고에서는 차체제작의 첫단계인 프레스 성형시 문제가 되는 알루미늄 합금판재의 성형성에 대하여 기술한다. 차체용 Al합금판의 성형성을 인장시험, 헤밍시험, 스트레치 포오밍 시험 등으로 조사해 보았다. 냉연강판과 비교하여 현재의 차체용 Al합금판은 강도와 연신율 면에서 열세임에 틀림이 없으나, 앞으로 냉여강판에 버금가는 Al합금판이 나오리라 예상한다. 1. 시편의 종류. 2. 결정립 조직. 3. 집합 조직. 4. 상온 인장시험. 5. 고온 인장시험. 6. 헤밍시험(Hemming test). 7. 스트레치 포오밍 시험(Stretch forming test)

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Tensile Strength of Composite Laminate Repaired Using Heat-blanket and a Novel Pressurization System (히트블랑켓과 새롭게 개발된 가압장치를 이용해 수리한 복합재 적층판의 인장강도 연구)

  • Chae, Song-Su;Lee, Gwang-Eun;Ahn, Hyonsu;Choi, Jin-Ho;Kweon, Jin-Hwe
    • Composites Research
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    • v.31 no.1
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    • pp.1-7
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    • 2018
  • In the case of a conventional composite patch repair using a heat blanket, the adhesive is pressurized using only a vacuum bag. In this study, however, a pressurization system has been developed to apply additional air pressure on the vacuum bag. In order to verify the performance of the developed system, the composite laminates were repaired with scarf patches and then tested under tensile load to be compared with the strength of the defect-free laminate. Tensile tests were also conducted on specimens with the same configuration but bonded in an autoclave. As a result of the test, the tensile strengths of the specimens repaired using the heat blanket with vacuum only without external pressure, the specimens repaired with additional pressure by the developed system, and the specimens repaired with the same external pressure in an autoclave, showed the strength recovery ratios of 74.9, 81.0, and 78.2%, respectively. The results of the tensile test after moisture saturation and the dried fatigue test also showed that the strength recovery ratios of the specimens repaired under the external pressure of 1 atm using the developed system are slightly higher than that of specimens bonded in autoclave.

압입시험 기법을 이용한 인장물성 평가

  • Kim, Sung-Hoon;An, Jung-Hoon;Choi, Yeol;Jeon, Eun-Chae;Kwon, Dong-Il
    • Proceedings of the Korean Institute of Industrial Safety Conference
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    • 2000.11a
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    • pp.3-8
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    • 2000
  • 현재 재료의 기계적 특성을 평가하기 위한 가장 표준화된 방법은 일축인장시험이다. 일축인장시험은 다양한 기계적 물성을 제공하나, 일정 크기 이상의 시편을 요구하므로 실제 산업현장에서 사용되고 있는 구조물의 안전성 평가에 이용하기 어렵다. 이러한 단 점을 개선할 수 있는 시험법으로 최신압입시험법이 제안되었다.(중략)

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Test Method on Interlaminar Tensile Properties of Carbon Fabric Reinforced Phenolic Composites (카본-페놀 직물복합재료의 층간인장물성 측정기법)

  • Lee Ji-Hyung;Kim Hyoung-Geun;Lee Hyung-Sik;Park Young-Che;Ju Se-Kyun
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2006.05a
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    • pp.81-85
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    • 2006
  • Through-the-thickness properties of thick-walled cylindrical composites are required to determine structural performances because interlaminar tensile stress is primarily responsible for structural failure of the composites during their curing process. It is necessary for evaluating the tensile properties to find individual test methods to find appropriate methods because there are no recognised international standards(test methods and test specifications) available for generating reliable tensile properties in the direction. This paper has performed an experimental Study to measure that properties of carbon fabric/phenolic composites are produced by domestic company. Several test methods using an aluminum specimen were compared and evaluated. The best method, found out, was adopted to measure transverse through-the-thickness properties of composite materials. The results show that strain trends on four faces of composite specimen are the same.

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