• Title/Summary/Keyword: 급속 가열

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The Effect of Heating Rate by Ohmic Heating on Rheological Property of Corn Starch Suspension (Ohmic Heating에 의한 가열속도 변화가 옥수수전분의 물성특성에 미치는 영향)

  • Lee, Seok-Hun;Jang, Jae-Kweon;Pyun, Yu-Ryang
    • Korean Journal of Food Science and Technology
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    • v.37 no.3
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    • pp.438-442
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    • 2005
  • Granule swelling is essential phenomenon of starch gelatinization in excess water, and characteristic of heated starch dispersion depends largely on size and distribution of swelled starch granule. Although swelling characteristic of starch granules depends on type of starch, heating rate, and moisture content, influence of heating rate on swelling phenomenon of starch granule has not been fully discussed, because constant heating rate of starch dispersion cannot be obtained by conventional heating method. Ohmic heating, electric-resistant heat generation method, applies alternative current to food materials, through which heating rate can be easily controlled precisely and conveniently at wide range of constant heating rates. Starch dispersion heated at low heating rates below $7.5^{\circ}C/min$ showed Newtonian fluid behavior, whereas showed pseudoplastic behavior at heating rates above $16.4^{\circ}C/min$. Apparent viscosity of starch dispersion increased linearly with increasing heating rate, and yield stress was dramatically increased at heating rates above $16.4^{\circ}C/min$. Average diameter of corn starch granules during ohmic heating was dramatically increased from $30.97\;to\;37.88\;{\mu}m$ by increasing heating rate from $0.6\;to\;16.4^{\circ}C/min$ (raw corn starch: $13.7\;{\mu}m$). Hardness of starch gel prepared with 15% corn starch dispersion after heating to $90^{\circ}C$ at different heating rates decreased gradually with increasing heating rate, then showed nearly constant value from $9.4\;to\;23.2^{\circ}C/min$. Hardness increased with increase of heating rate higher than $23.2^{\circ}C/min$.

Development and Application of the Super High Temperature Thermal Test Equipment (초고온 열하중 부가장치 개발 및 적용)

  • Jun, Joon-Tak;Kang, Hui-Won;Yang, Myung-Seog
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.43 no.1
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    • pp.33-39
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    • 2015
  • This paper describes test result of the Supersonic Wing Structure and the utility of thermal test equipment, which is possible to heat rapidly and continuously above $1,000^{\circ}C$, the durability and reliability of which are improved compared with the existing equipment. Through the test, we could predict the amount of strength reduction of the wing due to aerodynamic heating, caused by exposure of high temperature. Recently the aerodynamic heating temperature of the supersonic flying object is rapidly increased. It is possible to carry out the High Temperature Strength Test on the hypersonic speed flying object with the newly designed thermal test equipment. Because of that, we can upgrade the High Temperature Strength Structure Test technique and test reliability.

Dental Co-Cr alloys fabricated by selective laser melting: A review article (선택적 레이저 용융 방법으로 제작한 치과용 코발트 크롬 합금에 대한 문헌고찰)

  • Kang, Hyeon-Goo
    • The Journal of Korean Academy of Prosthodontics
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    • v.59 no.2
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    • pp.248-260
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    • 2021
  • Cobalt-chromium alloys are used to fabricate various dental prostheses, and have advantages of low cost and excellent mechanical properties compared to other alloys. Recently, selective laser melting, which is an additive manufacturing method, has been used to overcome the disadvantages of the conventional fabrication method. A local rapid heating and cooling process of selective laser melting induces fine microstructures, grain refinement, and reduction of porosities of the alloys. Therefore, it can improve mechanical properties compared to the alloys fabricated by the conventional method. On the other hand, layering process and rapid heating and cooling cause accumulation of a large amount of residual stresses that can adversely affect the mechanical properties. A heat treatment for removing residual stresses through recovery and recrystallization process caused complicated changes in mechanical properties induced by phase transformation, precipitate and homogenization of the microstructures. The purpose of this review was to compare the manufacturing methods of Co-Cr alloys and to investigate the characteristics of Co-Cr alloys fabricated by selective laser melting.

The Trend of Mitigation Devices for Insensitive Munition of Solid Rocket Motor (고체 추진기관 둔감화를 위한 완화장치의 연구 동향)

  • Ryu Byung-Tae;Yoon Ki-Eun;Jung Jin-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2006.05a
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    • pp.77-80
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    • 2006
  • Insensitive Munitions(IM) of solid propulsion system are defined as munitions that fulfil the performance and operational requirements, but will minimize the violence of a reaction when subjected to inadvertant stimuli. It should be clear that the reaction violence of rocket motor subjected to thermal stimuli can be mitigated by reducing confinement prior to propellant reaction. Devices designed to do this by venting the rocket motor case are commonly referred to as mitigation devices. The objective of this paper is to introduce the technical information related to the pyrotechnic mitigation devices for insensitive munition of solid rocket motor.

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Induction Heating Apparatus for Rapid Heating of Flat-Type Metallic Mold in Hot Embossing (미세 패턴 성형용 판형 금형의 급속 가열을 위한 유도가열기구)

  • Hong, S.K.;Lee, S.H.;Heo, Y.M.;Kang, J.J.
    • Transactions of Materials Processing
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    • v.16 no.4 s.94
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    • pp.282-287
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    • 2007
  • Hot embossing, one of Nanoimprint Lithography(NIL) techniques, has been getting attention as an alternative candidate of next generation patterning technologies by the advantages of simplicity and low cost compared to conventional photolithographies. A typical hot embossing usually, however, takes more than ten minutes for one cycle of the process because of a long thermal cycling. Over the last few years a number of studies have been made to reduce the cycle time for hot embossing or similar patterning processes. The target of this research is to develop an induction heating apparatus for heating a metallic micro patterning mold at very high speed with the large-area uniformity of temperature distribution. It was found that a 0.5 mm-thick nickel mold can be heated from $25^{\circ}C\;to\;150^{\circ}C$ within 1.5 seconds with the temperature variation of ${\pm}5^{\circ}C$ in 4-inch diameter area, using the induction heating apparatus.

비정질 실리콘 박막의 주울 가열 유도 결정화 공정 중 발생하는 Arc-Instability 기구 규명 및 방지책

  • Hong, Won-Ui;No, Jae-Sang
    • Proceedings of the Korean Vacuum Society Conference
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    • 2012.02a
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    • pp.375-375
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    • 2012
  • 최근 차세대 평판 디스플레이의 응용에 많은 주목을 받고 있는 AMOLED의 경우 전류구동 방식이기 때문에 a-Si TFT 보다는 LTPS-TFT가 요구되며, 대면적 기판에서의 결정립 크기의 균일도가 매우 중요한 인자이다. 비정질 실리콘 박막 상부 혹은 하부에 도전층을 개재하고, 상기도전층에 전계를 인가하여 그것의 주울 가열에 의해 발생한 고열에 의해 비정질 실리콘 박막을 급속 고온 고상 결정화하는 방법에 관한 기술인 JIC (Joule-heating Induced Crystallization) 결정화 공정은 기판 전체를 한번에 결정화 하는 방법이다. JIC 결정화 공정에 의하여 제조된 JIC poly-Si은 결정립 크기의 균일성이 우수하며 상온에서 수 micro-second내에 결정화를 수행하는 것이 가능하고 공정적인 측면에서도 별도의 열처리 Chamber가 필요하지 않는 장점을 가지고 있다. 그러나 고온 고속 열처리 방법인 JIC 결정화 공정을 수행 하면 Arc에 의하여 시편이 파괴되는 현상이 발견되었다. 본 연구에서는 Arc현상의 원인을 파악하기 위해 전압 인가 조건 및 시편 구조 조건을 변수로 결정화실험을 진행하였다. ARC가 발생하는 Si층과 Electrode 계면을 식각 분리하여 Electrode와 Si층 사이의 계면이 형성되지 않는 조건에서 전계를 인가하는 실험을 통하여 JIC 결정화 공정 중 고온에 도달하게 되면, a-Si층이 변형되어 형성된 poly-Si층이 전도성을 띄게 되고 인가된 전압이 도전층과 Poly-Si 사이에 위치한 $SiO_2$의 절연파괴(Dielectric breakdown)전압보다 높을 경우 전압 인가 방향에 수직으로 $SiO_2$가 절연 파괴되며 면저항 형태의 전도층의 단락이 진행되며 전도층이 완전히 단락되는 순간 Arc가 발생한다는 것을 관찰 할 수 있었다. 본 실험의 연구 결과를 바탕으로 Arc 발생을 방지하는 다양한 구조의 Equi-Potential 방법이 개발되었다.

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A Study on Insensitive Munition Test and Evaluation for Solid Rocket Motor (고체추진기관 둔감시험 평가 기법에 관한 연구)

  • Lee, Do-Hyung;Kim, Chang-Kee;Lee, Hwan-Gyu;Yoo, Ji-Chang
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2010.05a
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    • pp.129-132
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    • 2010
  • The objective of IM rocket motor is to minimize the probability of inadvertent initiation and severity of subsequent collateral damage, hence it is important to define personnel and equipment survivability to a rocket motor accident. The violent response probability associated with shock, impact and thermal effects be minimized. And during production, transportation/storage and stack of rocket motor, sympathetic detonation, giving severe effects of the propagation of adverse reaction on its surroundings, be reduced. Hence Reaction type also based on reaction results of the overpressure, fragment throw and heat flux.

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Quality improvement of retorted frozen seafood by adding sorbitol (솔비톨 첨가에 의한 냉동 해산물의 레토르트 후 품질 향상)

  • Cho, Won-Il;Song, Sang-Hoon
    • Korean Journal of Food Science and Technology
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    • v.49 no.1
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    • pp.85-89
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    • 2017
  • This study was conducted to prevent hardened texture in retorted frozen seafoods such as small octopus, squid, and top shell by adding sorbitol; the strength of mechanical hardness and other qualities were measured. The hardness of the 3 kinds of seafood pretreated with 2-4% (w/w) sorbitol solution decreased by 9-36% compared to the control. The hardness of retorted frozen octopus, squid, and top shell treated with sorbitol solution upon freezing significantly decreased to 1670, 1015, and $521g_f/cm^2$ compared to levels in untreated food of 1841, 1291, and $815g_f/cm^2$ (p<0.05), respectively. Yields based on weight in retorted seafood treated with sorbitol were increased by 2-5% compared to untreated samples. Additionally, the overall preference of texture was 0.4 points higher than that of control samples in descriptive sensory evaluation (p<0.05). The tissue softening of pretreated seafood was based on decreased dewatering due to the formation of small ice crystals during freezing as a result of sorbitol treatment.

Model Identification for Control System Design of a Commercial 12-inch Rapid Thermal Processor (상업용 12인치 급속가열장치의 제어계 설계를 위한 모델인식)

  • Yun, Woohyun;Ji, Sang Hyun;Na, Byung-Cheol;Won, Wangyun;Lee, Kwang Soon
    • Korean Chemical Engineering Research
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    • v.46 no.3
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    • pp.486-491
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    • 2008
  • This paper describes a model identification method that has been applied to a commercial 12-inch RTP (rapid thermal processing) equipment with an ultimate aim to develop a high-performance advanced controller. Seven thermocouples are attached on the wafer surface and twelve tungsten-halogen lamp groups are used to heat up the wafer. To obtain a MIMO balanced state space model, multiple SIMO (single-input multiple-output) identification with highorder ARX models have been conducted and the resulting models have been combined, transformed and reduced to a MIMO balanced state space model through a balanced truncation technique. The identification experiments were designed to minimize the wafer warpage and an output linearization block has been proposed for compensation of the nonlinearity from the radiation-dominant heat transfer. As a result from the identification at around 600, 700, and $800^{\circ}C$, respectively, it was found that $y=T(K)^2$ and the state dimension of 80-100 are most desirable. With this choice the root-mean-square value of the one-step-ahead temperature prediction error was found to be in the range of 0.125-0.135 K.