• Title/Summary/Keyword: Controlled blasting

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A Study on the Heat Treatment Technology for Reduction of Oxidation Scales (산화피막 저감을 위한 열처리 기술에 관한 연구)

  • Koo, Hee Jun;Chung, Chan Kyo
    • Clean Technology
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    • v.4 no.2
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    • pp.41-53
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    • 1998
  • Most of flame furnace with uncontrolled atmosphere forms oxidation scales in the surface during heat treatment. In this case, shot blasting and pickling are commonly used for reduction of oxidation scales. These processes have many disadvantages, such as long process time, high operating cost and environmental problems due to polishing dust, etc. Hence, this study aimed to develop the advanced heat treating equipment which could make a controlled atmosphere using a heatresisting structure into the flame furnace. The analysis result with SEM, EPMA, and EDX revealed that the amount of scales formed is much less than that with the conventional flame furnace. A brightness of the sample treated with the advanced process is similar compared to the treatment with vacuum furnace. In the present work, it was recommended that the inside structure of the furnace and gas line system could made up of SBB410 and STS310, respectively. The operating cost with the advanced heat treatment system could be reduced annually by forty million won. As a result of this study, it may be possible to reduce the oxidation scales. The fundamental information obtained in this study will be useful not only for improving the heat treatment process(reduction of shot blast and cleaning process), but for promoting the manufacture of bright products.

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Influence of surface treatment on the insertion pattern of self-drilling orthodontic mini-implants (표면처리가 교정용 미니 임플랜트의 식립수직력과 토크에 미치는 영향)

  • Kim, Sang-Cheol;Kim, Ho-Young;Lee, Sang-Jae;Kim, Cheol-Moon
    • The korean journal of orthodontics
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    • v.41 no.4
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    • pp.268-279
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    • 2011
  • Objective: The purpose of this study was to compare self-drilling orthodontic mini-implants of different surfaces, namely, machined (untreated), etched (acid-etched), RBM (treated with resorbable blasting media) and hybrid (RBM + machined), with respect to the following criteria: physical appearance of the surface, measurement of surface roughness, and insertion pattern. Methods: Self-drilling orthodontic mini-implants (Osstem implant, Seoul, Korea) with the abovementioned surfaces were obtained. Surface roughness was measured by using a scanning electron microscope and surface-roughness-testing machine, and torque patterns and vertical loadings were measured during continuous insertion of mini-implants into artificial bone (polyurethane foam) by using a torque tester of the driving-motor type (speed, 12 rpm). Results: The mini-implants with the RBM, hybrid, and acid-etched surfaces had slightly increased maximum insertion torque at the final stage ($p$ < 0.05). Implants with the RBM surface had the highest vertical load for insertion ($p$ < 0.05). Testing for surface roughness revealed that the implants with the RBM and hybrid surfaces had higher Ra values than the others ($p$ < 0.05). Scanning electron microscopy showed that the implants with the RBM surface had the roughest surface. Conclusions: Surface-treated, self-drilling orthodontic mini-implants may be clinically acceptable, if controlled appropriately.

EFFECTS OF SURFACE ROUGHNESS AND MULTILAYER COATING ON THE CORROSION RESISTANCE OF Ti-6Al-4V ALLOY

  • Ko, Yeong-Mu;Choe, Han-Cheol
    • Proceedings of the Korean Institute of Surface Engineering Conference
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    • 2003.10a
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    • pp.134-135
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    • 2003
  • The dental implant materials required good mechanical properties, such as fatigue strength, combined with a high resistance to corrosion. For increasing fatigue resistance and delaying onset of stress corrosion cracking, shot peening has been used for > 50 years to extend service life of metal components. However, there is no information on the electrochemical behavior of shot peened and hydroxyapatite(HA) coated Ti-6Al-4V alloys. To increase fatigue strength, good corrosion resistance, and biocompatibility, the electrochemical characteristics of Ti/TiN/HA coated and shot peened Ti-6Al-4V alloys by electron beam physical vapor deposition(EB-PVD) have been researched by various electrochemical method in 0.9%NaCl. Ti-6Al-4V alloys were prepared under the condition of hydrogen and vacuum arc furnace. The produced materials were quenched at 1000$^{\circ}C$ under high purity dried Ar atmosphere and were hold at 500$^{\circ}C$ for 2 hrs to achieve the fatigue strength(1140㎫) of materials. Ti-6Al-4V alloys were prepared under the condition of hydrogen and vacuum arc furnace. Shot peening(SP) and sand blasting treatment was carried out for 1, 5, and 10min. On the surface of Ti-6Al-4V alloys using the steel balls of 0.5mm and alumina sand of 40$\mu\textrm{m}$ size. Ti/TiN/HA multilayer coatings were carried out by using electron-beam deposition method(EB-PVD) as shown Fig. 1. Bulk Ti, powder TiN and hydroxyapatite were used as the source of the deposition materials. Electrons were accelerated by high voltage of 4.2kV with 80 - 120mA on the deposition materials at 350$^{\circ}C$ in 2.0 X 10-6 torr vacuum. Ti/TiN/HA multilayer coated surfaces and layers were investigated by SEM and XRD. A saturated calomel electrode as a reference electrode, and high density carbon electrode as a counter electrode, were set according to ASTM GS-87. The potentials were controlled at a scan rate of 100 mV/min. by a potentiostat (EG&G Co.273A) connected to a computer system. Electrochemical tests were used to investigate the electrochemical characteristics of Ti/TiN/HA coated and shot peened materials in 0.9% NaCl solution at 36.5$^{\circ}C$. After each electrochemical measurement, the corrosion surface of each sample was investigated by SEM.

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Progress of Composite Fabrication Technologies with the Use of Machinery

  • Choi, Byung-Keun;Kim, Yun-Hae;Ha, Jin-Cheol;Lee, Jin-Woo;Park, Jun-Mu;Park, Soo-Jeong;Moon, Kyung-Man;Chung, Won-Jee;Kim, Man-Soo
    • International Journal of Ocean System Engineering
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    • v.2 no.3
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    • pp.185-194
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    • 2012
  • A Macroscopic combination of two or more distinct materials is commonly referred to as a "Composite Material", having been designed mechanically and chemically superior in function and characteristic than its individual constituent materials. Composite materials are used not only for aerospace and military, but also heavily used in boat/ship building and general composite industries which we are seeing increasingly more. Regardless of the various applications for composite materials, the industry is still limited and requires better fabrication technology and methodology in order to expand and grow. An example of this is that the majority of fabrication facilities nearby still use an antiquated wet lay-up process where fabrication still requires manual hand labor in a 3D environment impeding productivity of composite product design advancement. As an expert in the advanced composites field, I have developed fabrication skills with the use of machinery based on my past composite experience. In autumn 2011, the Korea government confirmed to fund my project. It is the development of a composite sanding machine. I began development of this semi-robotic prototype beginning in 2009. It has possibilities of replacing or augmenting the exhaustive and difficult jobs performed by human hands, such as sanding, grinding, blasting, and polishing in most often, very awkward conditions, and is also will boost productivity, improve surface quality, cut abrasive costs, eliminate vibration injuries, and protect workers from exposure to dust and airborne contamination. Ease of control and operation of the equipment in or outside of the sanding room is a key benefit to end-users. It will prove to be much more economical than normal robotics and minimize errors that commonly occur in factories. The key components and their technologies are a 360 degree rotational shoulder and a wrist that is controlled under PLC controller and joystick manual mode. Development on both of the key modules is complete and are now operational. The Korean government fund boosted my development and I expect to complete full scale development no later than 3rd quarter 2012. Even with the advantages of composite materials, there is still the need to repair or to maintain composite products with a higher level of technology. I have learned many composite repair skills on composite airframe since many composite fabrication skills including repair, requires training for non aerospace applications. The wind energy market is now requiring much larger blades in order to generate more electrical energy for wind farms. One single blade is commonly 50 meters or longer now. When a wind blade becomes damaged from external forces, on-site repair is required on the columns even under strong wind and freezing temperature conditions. In order to correctly obtain polymerization, the repair must be performed on the damaged area within a very limited time. The use of pre-impregnated glass fabric and heating silicone pad and a hot bonder acting precise heating control are surely required.