• Title/Summary/Keyword: 단축인장시험

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The Mechanical Properties of CFRC under High Temperature (CFRC 복합재료의 기계적 고온특성)

  • Song, Gwan-Hyeong
    • Korean Journal of Materials Research
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    • v.11 no.4
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    • pp.258-265
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    • 2001
  • Compression and bending test have been conducted to evaluate the mechanical performance of CFRC at several different temperature up to $2000^{\circ}C$ . Tools and several grips for the test at high temperature were designed to obtain mechanical properties of CFRP. A major cause of increasing strength according to increasing the density and the temperature were analyzed. SEM method was utilized to find out the damage and the fracture mechanism. The new simple equation for the L(span length)/h(beam height) of specimens and for the failure criterion on the 4 point bending were proposed.

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Applications of Nanomanipulator in Nanowires (나노메니퓰레이터를 이용한 나노선의 특성평가)

  • Yoon, Sang-Won;Seo, Jong-Hyun;Ahn, Jae-Pyoung;Seong, Tae-Yeon;Lee, Kon-Bae
    • Journal of Powder Materials
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    • v.16 no.2
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    • pp.138-145
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    • 2009
  • The combination of focused ion beam (FIB) and 4 point probe nanomanipulator could make various nano manufacturing and electrical measurements possible. In this study, we manufactured individual ZnO nanowire devices and measured those electrical properties. In addition, tensile experiments of metallic Au and Pd nanowires was performed by the same directional alignment of two nanomanipulators and a nanowire. It was confirmed from I-V curves that Ohmic contact is formed between electrodes and nanomanipulators, which is able to directly measure the electrical properties of a nanowire itself. In the mechanical tensile test, Au and Pd nanowires showed a totally different fracture behavior except the realignment from <110> to <002>. The deformation until the fracture was governed by twin for Au and by slip for Pd nanowires, respectively. The crystallographic relationship and fracture mechanism was discussed by TEM observations.

The Rubber Performance Evaluation for Kick Motor Flexible Seal (킥모터 플렉시블 씰 개발을 위한 고무의 성능 평가)

  • Kim, Byung-Hun;Kwon, Tae-Hoon;Cho, In-Hyun
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.39 no.1
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    • pp.90-95
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    • 2011
  • A Kick Motor, KSLV-I second stage propulsion system, utilizes a flexible seal for pitch and yaw axis controls during combustion. A flexible seal consists of the alternate laminate of rubber and composite reinforcement between forward and aft rings. A Kick Motor nozzle is rotated by the shear deformation of rubber layers. Consequently, the development of rubber, which is appropriate to the usage condition of flexible seal, is very important. A tensile test, QLS test (shear modulus and failure shear stress), and aging test have been carried out to confirm the performance of rubber developed. Test results show that the shear modulus of rubber are 0.4310 ~ 0.4997MPa and the failure shear stress is more than 2.5MPa.

Assessment of Yield Characteristics of Gas Pipeline Materials by Observing Surface-Local Deformation (미소 표면변형 관찰을 통한 가스배관 부재의 항복특성 평가)

  • Lee, Yun-Hee;Baek, Un-Bong;Cheong, In-Hyeon;Nahm, Seung-Hoon;Lee, Sang-Houck
    • Journal of the Korean Institute of Gas
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    • v.12 no.2
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    • pp.92-98
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    • 2008
  • A combination of the instrumented indentation and 3D morphology measurement has been tried in order to perform a real-time property measurement of degraded materials in gas pipelines; three-dimensional indent morphologies were recorded using a reflective laser scanner after a series of insturmented indentations on three metallic specimens. Dimensions of the permanent deformation zone and contact boundary were analyzed from the cross-sectional profile over an remnant indent and used for estimating yield strength and hardness, respectively. Estimated yield strength was comparable with that from uniaxial tensile test and actual hardness implying material pile-up effects was lower than the calculated value from indentation curve by $20{\sim}30%$. It means that this 3D image analysis can explain the material pile-up effects on the contact properties. Additionally, a combined system of indentation and laser sensor was newly designed by modifying a shape of the indentation loading fixture.

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Structure design of regenerative cooling chamber of liquid rocket thrust chamber (액체로켓 연소기 재생냉각 챔버 구조설계)

  • Ryu, Chul-Sung;Choi, Hwan-Seok;Lee, Dong-Ju
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.33 no.12
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    • pp.109-116
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    • 2005
  • Elastic-plastic structural analysis for regenerative cooling chamber of liquid rocket thrust chamber is performed. Uniaxial tension test is also conducted for the copper alloy in order to get material data necessary for the structure analysis. The results of uniaxial tension test reveal that copper alloy become ductile after brazing process and flow stress becomes lower as temperature becomes higher. As a result of structural analysis using the material data, the deformation of cooling channel is more increased by thermal load than by internal pressure of cooling fluid. Therefore, the results of analysis show that structural stability and cooling performance of combustion thrust chamber which is designed to endure mechanical load and minimized a channel thickness are improved by decreased thermal load as possible.

Structural Analysis of Gasket and GDL for Enhanced Performance of PEMFC (고분자 전해질 연료전지 가스켓 및 GDL의 구조 해석)

  • Yoon, Jin-Young;Park, Jungsun
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.36 no.7
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    • pp.642-650
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    • 2008
  • In this paper, structural behavior of Gasket and GDL of a PEMFC stack is studied to improve the performance and to secure the safety. In the Gasket analysis Mooney-Rivlin strain energy function is used to consider hyperelasticity of load and displacement. The material properties is determined by testing specimens of the gasket at uni-axial and equi-biaxial mode and compared with finite element analysis results. By measuring a thickness change, the material property of GDL is determined. The pressure drop of a unit cell is measured along the channel for the clamping force. A cross sectional change of channel base on the experimental data is obtained experimentally and compare with FEM analysis results.

Characterization of Acryl Polymer Concretes for Ultra Thin Overlays (초박층 덧씌우기용 아크릴 폴리머 콘크리트의 특성 연구)

  • Kim, Dae-Young;Kim, Tae-Woo;Lee, Hyun-Jong;Kim, Hyung-Bae
    • International Journal of Highway Engineering
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    • v.12 no.3
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    • pp.1-8
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    • 2010
  • This study is performed to evaluate the physical and mechanical characteristics of an acryl polymer concrete that is developed as an overlay material for cement concrete slabs and pavements. Various laboratory tests including viscosity, flow, compressive strength, flexural strength, tensile strength, linear shrinkage, thermal expansion and thermal compatibility tests are performed. It is observed from the laboratory tests that the acryl polymer concrete developed in this study satisfies all the requirements suggested by ACI guideline. In addition to the laboratory tests, an accelerated performance testing (APT) is conducted to validate the performance of the acryl polymer concrete. During the APT, no significant distresses are observed until 15,903,939 cycles of equivalent single axle loading is applied. Finally, a 10mm thick overlay with the acryl polymer concrete is applied on top of an old deteriorated concrete pavement to evaluate field performance. Right after the field construction, skid resistance, noise and roughness are measured. The skid resistance and noise level have been significantly improved while the roughness is increased. Periodic investigation for the field study section will be conducted to evaluate the long-term performance.

An Experimental Study for Flexural Characteristic of Concrete Beam Reinforced with FRP Rebar under Static and Fatigue (FRP 보강근을 사용한 콘크리트 휨부재의 정적 및 피로특성에 대한 실험적 연구)

  • Sim, Jong-Sung;Park, Sung-Jae;Kang, Tae-Sung;Kwon, Dong-Wook;Lee, Ki-Hong
    • Proceedings of the Korea Concrete Institute Conference
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    • 2008.04a
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    • pp.313-316
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    • 2008
  • Corrosion of steel in the reinforced concrete structures is one of the main reason of degradation. It causes that lifetime of structures is shortened and maintenance cost is increased. And it also causes degradation of structures like bridges which are under repeated load. So, many research have been performed about FRP rebar. But there are few research about FRP rebar under fatigue. This study is to examine flexural characteristic of concrete beam reinforced with FRP(CFRP, GFRP) rebar under static and fatigue for considering the application. The specimens that used in this study are designed by ACI 440.1R-06 and reinforced with CFRP(CR) or GFRP(GR) overly. In the result of static bending test, all specimens were failed at compression phase. In fatigue test, the fatigue stress level was 60%, 70% or 80% of the static bending strength. Most of the specimens seemed to be compressive failure, but CR-60 and CR-70 specimens were failed with rupturing of tension bar.

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Measurement of Mechanical Material Properties of Rubber Compounds Sampled from a Pneumatic Tire (타이어에서 채취한 고무배합물의 기계적 물성 측정)

  • 김용우;김종국
    • Proceedings of the Korean Society of Machine Tool Engineers Conference
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    • 2002.04a
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    • pp.404-409
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    • 2002
  • Pneumatic tires usually contain a variety of rubber compositions, each designed to contribute some particular factor to overall performance. Rubber compounds designed for a specific function will usually be similar but not identical In composition and properties. Since 1970`s finite element analysis of tire has been performed extensively, which requires some energy density functions of rubber components of a tire. The conventional Mooney-Rivlin material model is one of the description that is commonly used in the analysis of tire. In this paper, we report the two material constants of gooney-Rivlin material model for some rubber compounds of a real pneumatic tire, which are obtained through uniaxial tension test.

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Manufacture of 3D Textile Preform and Study on Mechanical Properties of Composites (3D Textile 프리폼 제조 및 복합재료 기계적 특성 연구)

  • Jo, Kwang-Hoon;Klapper, Vinzenz;Kim, Hyeon-Woo;Lee, Jeong-Woon;Han, Joong-Won;Byun, Joon-Hyung;Joe, Chee-Ryong
    • Composites Research
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    • v.32 no.1
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    • pp.65-70
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    • 2019
  • The aircraft composites wing parts are usually integrated with adhesive or fastener. These laminated composites have weak interlaminar strength, which can lead to delamination. In order to compensate the disadvantages of laminated composites, it is possible to improve the strength, durability, shock and fatigue resistance by reinforcing the fiber in the thickness direction. In addition, using a single structure near-net-shape saves the manufacturing time and the number of fasteners, thus can reduce the overall cost of the composite parts. In this study, compression test, tensile test and open-hole tensile test are carried out for three structural architecture of 3D (three-dimensional) textile preforms: orthogonal(ORT), layer-to-layer(LTL) and through-the-thickness(TTT) patterns. Among these, the orthogonal textile composite shows the highest Young's modulus and strength in tensile and compression. The notch sensitivity of the orthogonal textile composite was the smallest as compared with UD (unidirectional) and 2D (two-dimensional) fabric laminates.