• Title/Summary/Keyword: defect engineering

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IR Camera Technique Application for Evaluation of Gas Turbine Blades Covering Integrity (가스터빈의 코팅층 건정성 평가를 위한 적외선 열화상 카메라 기법 활용)

  • Kim J.Y.;Yang D.J.;Choi C.J.;Park S.G.;Ahn Y.S.;Jeong G.J.
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2005.10a
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    • pp.192-196
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    • 2005
  • Key part of main equipment in a gas turbine may be likely to be damaged due to operation under high temperature, high pressure, high-speed rotation, etc. Accordingly, the cost for maintenance increases and the damaged parts may cause generation to stop. The number of parts for maintenance also increases, but diagnostics technology fur the maintenance actually does not catch up with the demand. Blades are made of precipitation hardening Ni superalloy IN738 and the like for keeping hot strength. The surface of a blade is thermal-sprayed, using powder with main compositions such as Ni, Cr, Al, etc. in order to inhibit hot oxidation. Conventional regular maintenance of the coating layer of a blade is made by FPI (Fluorescent Penetrant Inspection) and MTP (Magnetic Particle Testing). Such methods, however, are complicated and take long time and also require much cost. In this study, defect diagnostics were tested for the coating layer of an industrial gas turbine blade, using an infraredthermography camera. Since the infrared thermography method can check a temperature distribution on a wide range of area by means of non-contact, it can advantageously save expenses and time as compared to conventional test methods. For the infrared thermography method, however, thermo-load must be applied onto a tested specimen and it is difficult to quantify the measured data. To solve the problems, this essay includes description about producing a specimen of a gas turbine blade (bucket), applying thermo-load onto the produced specimen, photographing thermography images by an infrared thermography camera, analyzing the thermography images, and pre-testing for analyzing defects on the coating layer of the gas turbine blade.

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A numerical simulation of radiative heat transfer coupled with Czochralski flow in cusp magnetic field (복사열전달을 고려한 Cusp 자기장이 있는 초크랄스키 단결정 성장 공정의 유동에 관한 연구)

  • Kim, Tae-Ho;Lee, You-Seop;Chun,Chung-Hwan
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.20 no.3
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    • pp.988-1004
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    • 1996
  • The characteristics of flow and oxygen concentration are numerically studied in Czochralski 8" silicon crystal growing process considering radiative heat transfer. The analysis of net radiative heat flux on all relevant surfaces shows growing crystal affects the heater power. Furthermore, the variation of the radiative heat flux along the crystal surface in the growing direction is confirmed and should be a cause of thermal stress and defect of the crystal. The calculated distributions of temperature and, heat flux along the wall boundaries including melt/crystal interface, free surface and crucible wall indicate that the frequently used assumption of the thermal boundary conditions of insulated crucible bottom and constant temperature at crucible side wall is not suitable to meet the real physical boundary conditions. It is necessary, therefore, to calculate radiative heat transfer simultaneously with the melt flow in order to simulate the real CZ crystal growth. If only natural convection is considered, the oxygen concentration on the melt/crystal interface decreases and becomes uniform by the application of a cusp magnetic filed. The heater power needed also increases with increasing the magnetic field. For the case of counter rotation of the crystal and crucible, the magnetic field suppresses azimutal flow produced by the crucible rotation, which results in the higher oxygen concentration near the interface.

Analysis on Vehicle Fires Caused by Damage of Diesel Particulate Filter (DPF) (매연저감장치 손상에 기인한 차량화재 사고사례 분석)

  • Song, Jae-Yong;Sa, Seung-Hun;Nam, Jung-Woo;Cho, Young-Jin;Kim, Jin-Pyo;Park, Nam-Kyu
    • Fire Science and Engineering
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    • v.26 no.4
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    • pp.70-76
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    • 2012
  • This paper deal with vehicle fire caused by damage of diesel particulate filter (DPF) on diesel passenger vehicles. In order to reduce particulate matters included exhaust gases, a DPF in the exhaust system were installed diesel vehicles. A DPF was broken by excessively trapped particulate matters, regeneration error with a malfunction of ECU and defect of suction system such as swirl valve. If the DPF was broken, hot exhaust gases was released to the bottom of vehicle and released hot exhaust gases lead to occur the fire through combustible materials around the exhaust system. When a fire happened in the diesel vehicle caused by damage of DPF, silicate inorganic compounds were attached to the exhaust ventilation pipe and muffler. The silicate inorganic compounds were created by DPF combustion consisting of raw material ceramics. If the silicate inorganic compounds attached to the tail pipe in the diesel passenger vehicles, its fire cause will be assumed damage of DPF.

SLC-off Image Correlation and Usability Evaluation by Gapfill Function (Gapfill 함수에 의한 SLC off 영상 보정 및 활용성 평가)

  • Park, Joon-Kyu;Kim, Min-Gyu
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.13 no.8
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    • pp.3692-3697
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    • 2012
  • Landsat 7 ETM+ sensor is getting imageries in the SLC-off state since May 31, 2003 due to mechanical defect of SLC(Scan Line Corrector). Therefore additional correction works are required to use these imageries. In this study, Landsat 7 SLC-off imageries were corrected using Gapfill function and compared with Landsat 5 around the same time. Most of pixels in omitted areas due to SLC-off by producing SLC-off imageries and imageries without visual incompatibility could be achieved as there were not unnatural noises. Also, the corrected imageries were performed land cover classification which was compared with the classification result using reference image. To do this, it could be suggested the possibility of SLC-off imagery. Landsat 7 SLC-off corrected imageries will improve the difficult conditions to detect changes of large areas and be used to detect changes of large areas and classify imageries as well as to recover imagery loss arising regionally such as small scale cloud, etc.

Design of electrodes in the Patterned Vertical Aligned Liquid Crystal Cell for high optical performance (수직배향액정셀에서의 광학특성향상을 위한 전극설계)

  • Lee, Wa-Ryong;Kim, Kyung-Mi;Lee, Gi-Dong
    • Journal of the Korea Institute of Information and Communication Engineering
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    • v.11 no.2
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    • pp.344-348
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    • 2007
  • In this paper, we propose the electrode of the Patterned Vertical Aligned (PVA) cell [1] for high transmittance. We use the 'TechWiz LCD' for calculation of the director configuration and optical characteristics to ensure the results of the proposed electrode structure. In general, the transmittance of the PVA cell depends on the shape of the electrode and cell gap. In this work the width of gate line and data line of the improved electrode design is set to be equal to that of the PVA conventional. Instead, we modified the shape of the top and bottom electrode on order to decrease the area of the defect. For verification, we compared the calculated optical transmittance of the PVA cell with the proposed electrode structure to the conventional PVA cell . As a result, we can confirm that the optical loss due to the variation of the retardation the LC cell around electrode can be definitely decreased by the proposed electrode.

Certification Proposal for 3D Printing Technology Integrated Aviation Parts (3D 프린팅 기술 접목 항공부품의 인증 제안)

  • Park, Tae-Jin;Choi, Jeong-Ho
    • Journal of the Korea Convergence Society
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    • v.12 no.12
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    • pp.267-272
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    • 2021
  • This study would like to propose a certification of aviation components manufactured through 3D printing. Currently, many types of 3D printers are being used in various industries. Among them, a lot of research is being done in the aviation sector to manufacture drones and aviation components. However, the current level of 3D printer technology and the application of aviation components using it are lacking in many problems and related airworthiness certification standards. Furthermore, clear certification criteria for conformity and coherence are rarely presented. Therefore, we would like to propose matters related to certification of 3D printed equipment for application as aviation components. It is expected that 3D printing equipment will improve precision, reduce defect rate, sagging problem, and bed leveling problem will be solved in the future, and certification standards will be clearly established. In addition, we hope that the reliability of aviation components applied with 3D printing technology will be improved and the relevant certification standards will be further developed.

Formation Behavior of Anodic Oxide Films on Al 6061 Alloy in Sulfuric Acid Solution (황산 용액에서 Al6061 합금의 아노다이징 피막 형성거동)

  • Moon, Sungmo;Jeong, Kihun;Lim, Sugun
    • Journal of Surface Science and Engineering
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    • v.51 no.6
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    • pp.393-399
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    • 2018
  • Formation behavior of aluminum anodic oxide (AAO) films on Al6061 alloy was studied in view of thickness, morphology and defects in the anodic films in 20 vol.% sulfuric acid solution at a constant current density of $40mA/cm^2$, using voltage-time curve, observation of anodized specimen colors and surface and cross-sectional morphologies of anodic films with anodization time. With increasing anodizing time, voltage for film formation increased exponentially after about 12 min and its increasing rate decreased after 25 min, followed by a rapid decrease of the voltage after about 28 min. Surface color of anodized specimen became darker with increasing anodizing time up to about 20 min, while it appeared to be brighter with increasing anodizing time after 20 min. The darkened and brightened surfaces with anodizing time are attributed to an increase in thickness of porous anodic oxide film and a chemical damage of the films due to heat generated by increased resistance of the film, respectively. Cross-sectional observation of AAO films revealed the formation of defects of crack shape at the metal/oxide interface after 15 min which prevents the growth of AAO films. Width and length of the crack-like defect increased with anodizing time up to 25 min of anodizing, and finally the outer part of AAO films was partly dissolved or detached after 30 min of anodizing, resulting in non-uniform surface structures of the AAO films.

Stick-slip in Chemical Mechanical Polishing Using Multi-Particle Simulation Models (다수의 연마입자를 고려한 CMP 공정의 Stick-Slip 고찰)

  • Jung, Soyoung;Sung, In-Ha
    • Tribology and Lubricants
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    • v.34 no.6
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    • pp.279-283
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    • 2018
  • In this study, we investigate the behavior of abrasive particles and change of the stick-slip pattern according to chemical mechanical polishing (CMP) process parameters when a large number of abrasive particles are fixed on a pad. The CMP process is simulated using the finite element method. In the simulation, the abrasive grains are composed of those used in the actual CMP process. Considering the cohesion of the abrasive grains with the start of the CMP process, abrasive particles with various sizes are fixed onto the pad at different intervals so that stick-slip could occur. In this analysis, we determine that when the abrasive particle size is relatively large, the stick-slip period does not change as the pressure increases while the moving speed is constant. However, if the size of the abrasive grains is relatively small, the amount of deformation of the grains increases due to the elasticity of the pad. Therefore, the stick-slip pattern may not be observed. As the number of abrasive particles increases, the stick-slip period and displacement decrease. This is consistent with the decrease in the von Mises yield stress value on the surface of the wafer as the number of abrasive grains increases. We determine that when the number of the abrasive grains increases, the polishing rate, and characteristics are improved, and scratches are reduced. Moreover, we establish that the period of stick-slip increases and the change of the stick-slip size was not large when the abrasive particle size was relatively small.

Growth of Aluminum Nitride Thin Films by Atomic Layer Deposition and Their Applications: A Review (원자층 증착법을 이용한 AlN 박막의 성장 및 응용 동향)

  • Yun, Hee Ju;Kim, Hogyoung;Choi, Byung Joon
    • Korean Journal of Materials Research
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    • v.29 no.9
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    • pp.567-577
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    • 2019
  • Aluminum nitride (AlN) has versatile and intriguing properties, such as wide direct bandgap, high thermal conductivity, good thermal and chemical stability, and various functionalities. Due to these properties, AlN thin films have been applied in various fields. However, AlN thin films are usually deposited by high temperature processes like chemical vapor deposition. To further enlarge the application of AlN films, atomic layer deposition (ALD) has been studied as a method of AlN thin film deposition at low temperature. In this mini review paper, we summarize the results of recent studies on AlN film grown by thermal and plasma enhanced ALD in terms of processing temperature, precursor type, reactant gas, and plasma source. Thermal ALD can grow AlN thin films at a wafer temperature of $150{\sim}550^{\circ}C$ with alkyl/amine or chloride precursors. Due to the low reactivity with $NH_3$ reactant gas, relatively high growth temperature and narrow window are reported. On the other hand, PEALD has an advantage of low temperature process, while crystallinity and defect level in the film are dependent on the plasma source. Lastly, we also introduce examples of application of ALD-grown AlN films in electronics.

Keratinocyte Migration in a Three-Dimensional In Vitro Wound Healing Model Co-Cultured with Fibroblasts

  • Iyer, Kritika;Chen, Zhuo;Ganapa, Teja;Wu, Benjamin M.;Tawil, Bill;Linsley, Chase S.
    • Tissue Engineering and Regenerative Medicine
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    • v.15 no.6
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    • pp.721-733
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    • 2018
  • BACKGROUND: Because three-dimensional (3D) models more closely mimic native tissues, one of the goals of 3D in vitro tissue models is to aid in the development and toxicity screening of new drug therapies. In this study, a 3D skin wound healing model comprising of a collagen type I construct with fibrin-filled defects was developed. METHODS: Optical imaging was used to measure keratinocyte migration in the presence of fibroblasts over 7 days onto the fibrin-filled defects. Additionally, cell viability and growth of fibroblasts and keratinocytes was measured using the $alamarBlue^{(R)}$ assay and changes in the mechanical stiffness of the 3D construct was monitored using compressive indentation testing. RESULTS: Keratinocyte migration rate was significantly increased in the presence of fibroblasts with the cells reaching the center of the defect as early as day 3 in the co-culture constructs compared to day 7 for the control keratinocyte monoculture constructs. Additionally, constructs with the greatest rate of keratinocyte migration had reduced cell growth. When fibroblasts were cultured alone in the wound healing construct, there was a 1.3 to 3.4-fold increase in cell growth and a 1.2 to 1.4-fold increase in cell growth for keratinocyte monocultures. However, co-culture constructs exhibited no significant growth over 7 days. Finally, mechanical testing showed that fibroblasts and keratinocytes had varying effects on matrix stiffness with fibroblasts degrading the constructs while keratinocytes increased the construct's stiffness. CONCLUSION: This 3D in vitro wound healing model is a step towards developing a mimetic construct that recapitulates the complex microenvironment of healing wounds and could aid in the early studies of novel therapeutics that promote migration and proliferation of epithelial cells.