• Title/Summary/Keyword: Thermal Protection System

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Application of SFCL on Bus Tie for Parallel Operation of Power Main Transformers in a Fuel Cell Power Systems

  • Chai, Hui-Seok;Kang, Byoung-Wook;Kim, Jin-Seok;Kim, Jae-Chul
    • Journal of Electrical Engineering and Technology
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    • v.10 no.6
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    • pp.2256-2261
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    • 2015
  • In the power plant using high temperature fuel cells such as Molten Carbonate Fuel Cell(MCFC), and Solid Oxide Fuel Cell(SOFC), the generated electric power per area of power generation facilities is much higher than any other renewable energy sources. - High temperature fuel cell systems are capable of operating at MW rated power output. - It also has a feature that is short for length of the line for connecting the interior of the generation facilities. In normal condition, these points are advantages for voltage drops or power losses. However, in abnormal condition such as fault occurrence in electrical system, the fault currents are increased, because of the small impedance of the short length of power cable. Commonly, to minimize the thermal-mechanical stresses on the stack and increase the systems reliability, we divided the power plant configuration to several banks for parallel operation. However, when a fault occurs in the parallel operation system of power main transformer, the fault currents might exceed the interruption capacity of protective devices. In fact, although the internal voltage level of the fuel cell power plant is the voltage level of distribution systems, we should install the circuit breakers for transmission systems due to fault current. To resolve these problems, the SFCL has been studied as one of the noticeable devices. Therefore, we analyzed the effect of application of the SFCL on bus tie in a fuel cell power plants system using PSCAD/EMTDC.

Analysis of Effects of Lightning on PAV Using Computational Simulation and a Proposal to Establish Certification Guidance (전산 시뮬레이션을 통한 PAV 낙뢰 영향성 분석 및 인증기술에 관한 연구)

  • Park, Se-Woong;Kim, Yun-Gon;Kang, Yong-Seong;Myong, Rho-Shin
    • Journal of Aerospace System Engineering
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    • v.13 no.6
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    • pp.60-69
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    • 2019
  • Companies around the world are actively developing Personal Air Vehicle (PAV) to solve the serious social problem of traffic jams. Airworthiness certification for PAV is required, since it is a manned vehicle. As with aircraft, the critical threat to the safe operation of PAV is lightning strike with strong thermal load and magnetic fields. Lightning certification issue also remains important for PAV, since there are still insufficient development of PAV-related lightning certification technologies, guidelines, and requirements. In this study, the SAE Aerospace Recommended Practice (ARP), an international standard certification guideline recognized by the Federal Aviation Administration (FAA), was analyzed. In addition, the guideline of lightning certification was applied to a PAV. The impact of lightning on PAV was also analyzed through computational software. Finally, the basis for the establishment of the PAV lightning certification guidance was presented.

The Performance Characteristics of Anti-Surge Devices for High Head Cooling Water Systems in 1,000 MW Thermal Power plants (고수두 1,000 MW 석탄화력발전소 냉각수계통 수격방지장치의 성능특성)

  • Kim, Keun-Pil;Yoo, Hoseon
    • Plant Journal
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    • v.15 no.4
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    • pp.36-42
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    • 2019
  • In recent, according to the tightening of environment regulation policy, the height of the site of the power plant is increased and the length of the cooling water pipe is increased. This has a serious impact on the stability of the plant. This study analyzes the transient phenomenon using LIQT 7.2, an unsteady state one-dimensional analysis software, to secure the stability of 1,000 MW high-capacity coal-fired power plant cooling water system with high head. To prevent water hammer, The effects on performance characteristics were predicted by individual and combination application. The surge pressure of the cooling water which occurs when the pump was stopped without installing the anti-surge devices was the largest at the pump outlet side. The most effective and simple way to reduce surge pressure in these cooling water systems is to combine a vacuum breaker with a hydraulic non-return valve, which is an essential device for pump protection.

A Study on Surface Properties of Ablative Materials from 0.4MW Arc-Heated Wind Tunnel Test (0.4MW 아크 가열 풍동 시험을 통한 삭마 재료의 표면 특성 연구)

  • Kim, Nam Jo;Oh, Philyong;Shin, Eui Sup
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.43 no.12
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    • pp.1048-1053
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    • 2015
  • Ablative materials in a thermal protection system for atmospheric re-entry suffers from the most severe heat fluxes and temperatures, which induces surface recession in the thickness direction. In this paper, a 0.4MW arc-heated wind tunnel is operated to test for ablative materials, and a non-contact three-dimensional surface measuring system is used to evaluate the different surface characteristics of them. In particular, by postprocessing the three-dimensional image data, the surface roughness and recession of ablative materials can be calculated before and after the wind tunnel test. Moreover, the surface properties are analyzed quantitatively by comparing volume and mass losses of the test specimens.

Technical Review and Analysis of Ramjet/Scramjet Technology I. Ramjet Engine (Liquid Ramjet, Ducted Rocket) (램제트/스크램제트의 기술동향과 소요기술 분석 I. 램제트 엔진(액체램제트, 덕티드로켓))

  • Sung Hong-Gye;Yoon Hyun-Gull
    • Journal of the Korean Society of Propulsion Engineers
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    • v.10 no.1
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    • pp.72-86
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    • 2006
  • A technical review of current ramjet propulsion is presented. In addition to summarize the current status of ramjet technology, new key techniques like Boosting technique easily adapting total impulse of booster, flame stabilization technique with minimized ramjet combuster length, variable nozzle-inner-surface technique realizing wide flight-envelop, and thermal protection technique for long operating time are identified. Actually various Ramjet propulsion technology has been matured and expanding to both military and combined cycle application. Yet many opportunities remain to be challenged by future generations of explorers to utilize s typical ramjet propulsion system for multi-purpose(multi-platform and multi-target) missiles, for example, American JSSCM and Russian Yakhont missiles, improving both reliability of techniques and downsizing development cost of new propulsion system.

Electrically conductive nano adhesive bonding: Futuristic approach for satellites and electromagnetic interference shielding

  • Ganesh, M. Gokul;Lavenya, K.;Kirubashini, K.A.;Ajeesh, G.;Bhowmik, Shantanu;Epaarachchi, Jayantha Ananda;Yuan, Xiaowen
    • Advances in aircraft and spacecraft science
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    • v.4 no.6
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    • pp.729-744
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    • 2017
  • This investigation highlights rationale of electrically conductive nano adhesives for its essential application for Electromagnetic Interference (EMI) Shielding in satellites and Lightning Strike Protection in aircrafts. Carbon Nano Fibres (CNF) were functionalized by electroless process using Tollen's reagent and by Plasma Enhanced Chemical Vapour Deposition (PECVD) process by depositing silver on CNF. Different weight percentage of CNF and silver coated CNF were reinforced into the epoxy resin hardener system. Scanning Electron Microscopy (SEM) micrographs clearly show the presence of CNF in the epoxy matrix, thus giving enough evidence to show that dispersion is uniform. Transmission Electron Microscopy (TEM) studies reveal that there is uniform deposition of silver on CNF resulting in significant improvement in interfacial adhesion with epoxy matrix. There is a considerable increase in thermal stability of the conductive nano adhesive demonstrated by Differential Scanning Calorimetry (DSC) and Thermogravimetric Analysis (TGA). Four probe conductivity meters clearly shows a substantial increase in the electrical conductivity of silver coated CNF-epoxy composite compared to non-coated CNF-epoxy composite. Tensile test results clearly show that there is a significant increase in the tensile strength of silver coated CNF-composites compared to non-coated CNF-epoxy composites. Consequently, this technology is highly desirable for satellites and EMI Shielding and will open a new dimension in space research.

Aerodynamic control capability of a wing-flap in hypersonic, rarefied regime: Part II

  • Zuppardi, Gennaro;Vangone, Daniele
    • Advances in aircraft and spacecraft science
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    • v.4 no.5
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    • pp.503-514
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    • 2017
  • The attitude control of an aircraft is usually fulfilled by means of thrusters at high altitudes. Therefore, the possibility of using also aerodynamic surfaces would produce the advantage of reducing the amount of fuel for the thrusters to be loaded on board. For this purpose, Zuppardi already considered some aerodynamic problems linked to the use of a wing flap in a previous paper. A NACA 0010 airfoil with a trailing edge flap of 35% of the chord, in the range of angle of attack 0-40 deg and flap deflections up to 30 deg was investigated. Computer tests were carried out in hypersonic, rarefied flow by a direct simulation Monte Carlo code at the altitudes of 65 and 85 km of Earth Atmosphere. The present work continues this subject, considering the same airfoil and free stream conditions but two flap extensions of 45% and 25% of the chord and two flap deflections of 15 and 30 deg. The main purpose is to compare the influence of the flap dimension with that of the flap deflection. The present analysis is carried out in terms of: 1) percentage variation of the global aerodynamic coefficients with respect to the no-flap configuration, 2) increment of pressure and heat flux on the airfoil lower surface due to the Shock Wave-Shock Wave Interaction (SWSWI) with respect to the same quantities with no SWSWI or in no-flap configuration, 3) flap hinge moment. Issues 2) and 3) are important for the design of the mechanical and thermal protection system and of the flap actuator, respectively. Under the above mentioned test and geometrical conditions, the flap deflection is aerodynamically more effective than the flap extension, because it involves higher variation of the aerodynamic coefficients. However, tests verify that a smaller deflection angle involves the advantage of a smaller increment of pressure and heat flux on the airfoil lower surface, due to SWSWI, as well as a smaller hinge moment.

Frost resistance of porous concrete assuming actual environment (實環境を考慮したポーラスコンクリートの耐凍害性の評価(실제 환경을 고려한 다공질 콘크리트의 내동해성(耐凍害性) 평가))

  • NAKAMURA, Takuro;HORIGUCHI, Takashi;SHIMURA, Kazunori;SUGAWARA, Takashi
    • Proceedings of the Korean Institute of Building Construction Conference
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    • 2008.11a
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    • pp.227-233
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    • 2008
  • Porous concrete has large continuous voids of 20-30 % by volume, and this concrete is attractive as environmental material in Japan i.e. permeable road pavement, river bank protection with vegetation and green roof system which influence thermal environment. It is necessary to confirm the frost resistance when constructing porous concrete structure in cold region. However applicable test method and evaluation criterion of porous concrete has not defined yet. Therefore, the object of this study is to investigate the frost resistance of porous concrete and this investigation attempts to address this concern by comparing 4 kinds of specified freezing and thawing tests methods (JIS A1148 procedure A/B and RILEM CIF/CDF test) in consideration of actual environment. RILEM freeze-thaw tests are different from JIS A1148 freeze-thaw tests, which are widely adopted for evaluating the frost resistance of conventional concrete in Japan, in water absorption, cooling rate, length of freezing and thawing period, and number of freezing and thawing cycles. RILEM CIF test measures internal damage and is primarily applicable for pure frost attack. CDF test is appropriate for freeze-thaw and de-icing salt attack. JIS A1148 procedure A/B showed extremely low frost resistance of porous concrete if the large continuous voids were filled with water and the ice expansion in the large continuous voids set in during cooling. Frost resistance of porous concrete was improved by mixing coarse aggregate (G7) which particle size is smaller and fine aggregate in JIS freezing and thawing tests. RILEM CIF/CDF test showed that freeze-thaw and de-icing resistance of porous concrete was seems to be superior in that of conventional concrete.

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Research on Overheat Protection Techniques of Connection Parts of MCCB by Poor Contact (MCCB 단자 접속부의 접촉불량에 의한 과열사고 방지기법에 관한 연구)

  • Kim, Dong-Woo;Lee, Ki-Yeon;Moon, Hyun-Wook;Kim, Hyang-Kon;Cho, Chung-Seog
    • Fire Science and Engineering
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    • v.22 no.4
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    • pp.54-60
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    • 2008
  • In this study, damage characteristics of MCCB and terminal block due to poor contact were analyzed, and various poor contact detection techniques were suggested. Firstly, the detection techniques using thermocouple and infrared thermal camera were analyzed respectively. Also, thermo-cap during poor contact detected abnormal status effectively by changing its color, and the detection system using an odor detector and odor capsules was analyzed. Lastly, poor contact detection screw was made using characteristics of fusible alloy, and we applied the poor contact detection screw to terminal block. The above methods could prevent electrical fire caused by poor contact effectively if they are used properly.

Lifespan Extending Effects of Helianthus tuberosus Linne in C. elegans (예쁜꼬마선충을 이용한 돼지감자의 수명 연장 효능)

  • Lee, Byung Ju;Yoon, Young Jin;Oh, Jong Woo;Park, Zi Won;Lee, Hyun Joo;Kim, Yong Sung;Cha, Dong Seok;Kwon, Jin;Oh, Chan Ho;Jeon, Hoon
    • Korean Journal of Pharmacognosy
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    • v.47 no.3
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    • pp.280-286
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    • 2016
  • Helianthus tuberosus Linne (Compositae) has been widely used as a folk remedy to treat various ailments including fever, bleeding, fracture and contusion. This study was designed to elucidate the lifespan extending activities MeOH extract of the tubers of Helianthus tuberosus Linne (MHT) using Caenorhabditis elegans (C. elegans) model system. In the current study, we found that the lifespan of worms was significantly extended by MHT supplement, dose-dependently. MHT also provided robust protection against various stress environments such as osmotic, thermal and oxidative condition. In addition, elevated antioxidant enzyme activities by MHT resulted in attenuation of intracellular reactive oxygen spices (ROS) levels, suggesting antioxidant capacity of MHT might be associated with longevity properties. Herein, we showed that altered food intake and growth of worms were also involved in the MHT activity. Furthermore, MHT increased body movement in aged worms, indicating possible role for MHT in healthspan.