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Damage Detection in Composite Laminates using Tapping Sound (태핑음을 이용한 복합적층판의 손상검출)

  • Kim, Sung-Joon;Hong, Chang-Ho
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.37 no.11
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    • pp.1089-1095
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    • 2009
  • The radiated sound pressure induced by tapping test is obtained by solving the Rayleigh integral equation. For structurally radiated sound, the sound field is directly coupled to the structural motion. Therefore the impact response should be analyzed. In this paper, the delamination model is used to analyze the impact response of delaminated composite laminates. And efficient spring-mass model has been proposed to model hammer shaped impactor. Predicted sound pressure histories are compared with test data. The influence of damage on the sound pressure and impacted force history of laminates were investigated. The results show that both radiated sound pressure and impact force history are strongly influenced by delamination on laminates. As a result, it is shown that the presented sound based tapping method was found to be reliable for detecting the damage in composite laminate.

Behaviors of Laminated Composite Folded Structures According to Ratio of Folded Length (곡절 길이비에 따른 복합적층 절판 구조물의 거동)

  • Yoo Yong-Min;Yhim Sung-Soon;Chang Suk-Yoon
    • Journal of the Computational Structural Engineering Institute of Korea
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    • v.19 no.3 s.73
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    • pp.223-231
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    • 2006
  • This study deals with behavior characteristics of laminated composite folded structures according to ratio of folded length based on a higher-order shear deformation theory. Well-known mixed finite element method using Lagrangian and Hermite shape interpolation functions is a little complex and have some difficulties applying to a triangular element. However, a higher-order shear deformation theory using only Lagrangian shape interpolation functions avoids those problems. In this paper, a drilling degree of freedom is appended for more accurate analysis and computational simplicity of folded plates. There are ten degrees of freedom per node, and four nodes per element. Journal on folded plates for effects of length variations is not expressed. Many results in this study are carried out according to ratio of folded length. The rational design is possible through analyses of complex and unpredictable laminated composite folded structures.

Detection of High-Velocity Impact Damage in Composite Laminates Using PVDF Sensor Signals (고분자 압전 필름 센서를 이용한 복합재 적층판의 고속 충격 손상 탐지)

  • Kim Jin-Won;Kim In-Gul
    • Composites Research
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    • v.18 no.6
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    • pp.26-33
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    • 2005
  • The mechanical properties of composite materials may severely degrade in the presence of damage. Especially, the high-velocity impact such as bird strike, a hailstorm, and a small piece of tire or stone during high taxing, can cause considerable damage to the structures and sub-system in spite of a very small mass. However, it is not easy to detect the damage in composite plates using a single technique or any conventional methods. In this paper, the PVDF(polyvinylidene fluoride) film sensors were used for monitoring high-velocity impact damage initiation and propagation in composite laminates. The WT(wavelet transform) and STFT(short time Fourier transform) are used to decompose the sensor signals. A ultrasonic C-scan and a digital microscope are also used to examine the extent of the damage in each case. This research shows how various sensing techniques, PVDF sensor in particular, can be used to characterize high-velocity impact damage in advanced composite.

Sound Insulation Performance of Honeycomb Composite Panel for a Tilting Train (틸팅 열차용 허니콤 복합 적층재의 차음성능)

  • Kim, Seock-Hyun;Seo, Tae-Gun
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.34 no.12
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    • pp.1931-1936
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    • 2010
  • In Korean tilting trains, honeycomb composite panels are used for high speed and light weight. The side wall of a tilting train consists of an aluminum honeycomb coated with carbon-fiber-reinforced epoxy skin and a nomex honeycomb panel as the main structure, with glass wool inserted between the panels. In this study, based on ASTM E2249-02, we measure the intensity sound transmission loss (TL) of the honeycomb composite panels. Using mass law deviation (MLD), we estimate the sound insulation performance of the honeycomb composite panels in terms of their weight and explore the feasibility of substituting a conventional corrugated steel panel. The transmission-loss data of the honeycomb composite panels obtained in the study will be used to establish noise-reduction measures for train compartments.

A Performance Analysis and Experiments on Plastic Film/Paper Humidifying Elements Consisting of Horizontal Air Channels and Vertical Water Channels (수평 공기 채널과 수직 물 채널로 구성된 플라스틱 필름/종이 가습 소자의 성능)

  • Kim, Nae-Hyun
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.40 no.1
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    • pp.55-63
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    • 2016
  • New materials and shapes for a humidifying element were developed which outperformed the widely used crisscross glass wool Glasdek media design. The new material consists of 50% cellulose and 50% PET. The parallel channel configuration was devised to reduce excessive pressure loss caused by the reduced height (from 7.0 mm to 5.0 mm) of the crisscross configuration. For the same crisscross configuration, the humidification efficiency of the cellulose/PET element was 26% higher than that of the glass wool element. For the same cellulose/PET material, humidification efficiency of the parallel channel configuration was 14% higher than that of the crisscross configuration. As for the pressure drops, the cellulose/PET element was 2-52% higher than those of the glass wool element. For the same cellulose/PET material, the pressure drop of the parallel channel configuration was 14% higher than that of the crisscross configuration. Data were compared against the predictions from existing correlations and those by the proposed model.

Structural Characteristics on InAs Quantum Dots multi-stacked on GaAs(100) Substrates

  • Roh, Cheong-Hyun;Park, Young-Ju;Kim, Eun-Kyu;Shim, Kwang-Bo
    • Journal of the Microelectronics and Packaging Society
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    • v.7 no.1
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    • pp.25-28
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    • 2000
  • The InAs self-assembled quantun dots (SAQDS) were grown on a GaAs(100) substrate using a molecular beam epitaxy (MBE) technique. The InAs QDs were multi-stacked to have various layer structures of 1, 3, 6, 10, 15 and 20 layers, where the thickness of the GaAs spacer and InAs QD layer were 20 monolayers (MLs) and 2 MLs, respectively. The nanostructured feature was characterized by photoluminescence (PL) and scanning transmission electron microscopy (STEM). It was found that the highest PL intensity was obtained from the specimen with 6 stacking layers and the energy of the PL peak was split with increasing the number of stacking layers. The STEM investigation exhibited that the quantum dots in the 6 stacking layer structure were well aligned in vertical columns without any deflect generation, whereas the volcano-like deflects were formed vertically along the growth direction over 10 periods of InAs stacking layers.

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Carbon Fiber Tow Spreading Technology and Mechanical Properties of Laminate Composites (탄소섬유 펼침 기술 및 이를 적용한 적층 복합재료의 기계적 특성)

  • Park, Sung Min;Kim, Myung Soon;Choi, Yoon Sung;Lee, Eun Soo;Yoo, Ho Wook;Chon, Jin Sung
    • Composites Research
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    • v.28 no.5
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    • pp.249-253
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    • 2015
  • This paper reports a study on a method for achieving lightweight thermoplastic laminate composites referred to as tow spreading technology. Thickness of an unspread 12 K carbon fiber tow is reduced by increasing the tow width from 7 mm to 20 mm. The polypropylene (PP) film was used to stabilize and impregnate the spread tow, covering it into a partially consolidated prepreg: 12 K carbon fiber spread tow/PP. Laminates were fabricated from the spread tow prepreg and control laminate composites were produced from unspread tow prepreg consisting of 12 K carbon fiber and PP. The void content, tensile and flexural properties of the composite laminates were investigated. Consequently, the spread tow laminate composite exhibited lower void content and improved mechanical properties.

Three Dimensional Layering Algorithm for 3-D Metal Printing Using 5-axis (3 차원 금속 프린팅을 위한 다중 3 차원 적층 알고리듬(3DL))

  • Ryu, Sua;Jee, Haeseong
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.38 no.8
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    • pp.881-886
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    • 2014
  • The purpose of three-dimensional (3-D) metal printing using 5-axis is to deposit metal powder by changing the orientation of the deposited structure to be built for the overhang or undercut feature on part geometry. This requires a complicated preprocess functionality of providing three dimensionally sliced layers to cover the required part geometry. This study addresses the overhang/undercut problem in 3-D metal printing and discusses a possible solution of providing 3-D layers to be built using the DMT(R) machine.

진공 플라즈마 용사코팅시 분말 이송가스 유량이 적층효율에 미치는 영향

  • Jeong, Yeong-Hun;Nam, Uk-Hui;Byeon, Eung-Seon
    • Proceedings of the Korean Vacuum Society Conference
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    • 2014.02a
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    • pp.161-161
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    • 2014
  • 열플라즈마는 주로 아크 방전에 의해 발생시킨 전자, 이온, 중성입자(원자 및 분자)로 구성된 부분 이온화된 기체로, 국소열평형상태를 유지하여 구성입자가 모두 수천에서 수만도에 이르는 같은 온도를 갖는 고속의 제트 화염 형태를 이루고 있다. 이렇게 고온, 고열용량, 고속, 다량의 활성입자를 갖는 열플라즈마의 특성을 이용하여, 종래 기술에서는 얻을 수 없는 다양하고 효율적인 산업적 이용이 활발히 진행되고 있다. 용사코팅은 노즐 출구를 통해서 외부로 방출되는 열 플라즈마 화염을 이용하는 것으로 이 화염의 와류 특성으로 인하여 외기의 가스가 화염내부로 침투하는 특성을 가진다. 이러한 현상은 열원의 냉각효과 외에도 외기를 구성하는 기체 분자의 내부 유입을 의미하는 것으로 대기 상태에서 공정이 이루어진다면 열원 내로 유입되는 대기 내의 산소가 모재 표면과 반응하여 산화가 진행된다. 이러한 산화과정은 용사 코팅의 품질을 저하시키는 요인이 되므로, W, Ti 등과 같은 반응성이 높은 재료의 코팅은 산화과정을 방지하기 위하여 진공에서 코팅을 하여야만 한다. 진공 플라즈마용사코팅은 진공 또는 저압의 불활성 분위기 중에서 열플라즈마 화염에 용사재료를 투입하여 플라즈마 화염 내부에서 순간적으로 이를 용융시킨 후 고속으로 분출, 모재에 적층시키는 코팅공정이다. 이때 분말상의 용사재료를 고속으로 화염 중심에 투입하여 최대 에너지 전달이 이루어지도록 하는 것이 적층효율 및 코팅품질을 향상에 필수적이다. 하지만 플라즈마 화염 내부를 고속으로 이동하는 입자의 온도와 속도 및 궤적을 측정하여 제어하는 것은 매우 어렵기 때문에, 통상 형성된 코팅의 구조와 두께로부터 경험적으로 파라미터를 결정하는 것이 일반적이다. 본 연구에서는 초고속 레이저 카메라와 이미지 분석용 소프트웨어를 이용하여 플라즈마 화염내의 비행입자 궤적을 추적하고, 이를 통해 분말 이송가스의 유량이 코팅 효율 및 미세구조에 미치는 영향을 조사하였다. 플라즈마 화염은 중심부가 가장 높은 온도와 속도를 가지고 있기 때문에, 분말 이송가스의 유량이 적을 경우 투입된 분말은 단지 플라즈마 화염의 상부 경계면을 지나는 궤적을 갖게된다. 이로 인해 분말의 용융이 충분히 이루어지지 않아 적층 효율이 낮고 미용융 입자 및 기공이 많은 미세구조를 보였다. 이송가스 유량을 증가시키게 되면, 분말의 궤적은 플라즈마 화염의 중심부를 지나게 되어 적층 효율이 증가하고 미세구조 또한 개선되었다. 하지만 이송가스 유량이 지나치게 클 경우, 투입된 분말 입자는 플라즈마 화염을 조기에 관통하게 되어 비행궤적은 온도와 속도가 낮은 영역에 형성되었다.

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The Effect of Fabrication Process Parameters on the Microstructures of Intermetallic/Metal Laminated Composite by Self-propagating High-temperature Synthesis (자전고온반응에 의한 금속간화합물/금속 적층복합재료의 제조공정변수가 미세조직에 미치는 영향)

  • 김희연;정동석;홍순형
    • Composites Research
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    • v.16 no.3
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    • pp.68-74
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    • 2003
  • In this paper, intermetallic/metal laminated composites have been successfully produced that utilizes SHS reactions between Ni and Al elemental metal foils. The reaction between Ni and Al started from the nucleation and growth of NiA1$_3$ and was followed by the diffusional growth of Ni$_2$A1$_3$ between Ni and NiA1$_3$. The SHS reaction was thermodynamically analyzed through the final volume fraction of the non-reacted Al related with the initial thickness ratio of Ni:Al and prior heat treatment. Thermally aging these 1aminates resulted in formation of a functionally gradient series of intermetallic phases. Microstructure showed that the intermetallic volume percent was 82, 59.5, 40% in the 1:1, 2:1, 4:1 thickness ratio specimen. Main phases of the intermetallic were NiAl and Ni$_3$Al having higher strength at room and high temperatures.