• Title/Summary/Keyword: Thermal Margin

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Results of Thermal Conductivity Measurement of NiCr Coatings for the Thrust Chamber of a LRE (액체로켓엔진 연소기 적용 니켈크롬도금의 열전도도 측정결과)

  • Lim, Byoung-Jik;Choi, Hwan-Seok
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.11a
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    • pp.805-806
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    • 2011
  • Thermal conductivities of a Ni-Cr coating applied for the protection of a thrust chamber operating under the condition of high pressure and high temperature were measured. Results showed that the data used in heat transfer calculation has a 20~25% margin compared with data measured.

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The Effect of Manipulating Package Construct and Leadframe Materials on Fracture Potential of Plastically Encapsulated Microelectronic Packages During Thermal Cycling

  • Lee, Seong-Min
    • Transactions on Electrical and Electronic Materials
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    • v.2 no.3
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    • pp.28-32
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    • 2001
  • It was studied in the present work how the thermal cycling performance of LOC (lead on chip) packages depends on the package construct or leadframe materials. First, package body thickness and Au wire diameter were manipulated for the selection of proper package design. Secondly, two different types of leadframe materials (i.e. copper and 52%Fe-48%Ni alloy) were tested to determine the better material for improved reliability margin of plastically encapsulated microelectronic packages. This work shows that manipulating package body thickness was more effective than an increase of Au wire from 23$\mu\textrm{m}$ to 33$\mu\textrm{m}$ for the prevention of wire debonding failure. Further, this work indicates that the LOC packages including the copper leadframes can be more susceptible to thermal cycling reliability degradation due to chip cracking than those including the alloy leadframes.

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HAUSAT-2 STM(Structural-Thermal Model) Development and Launch Environment Test Result Analyses (HAUSAT-2 위성 STM 개발 및 발사환경시험 분석)

  • Chang, Jin-Soo;Hwang, Ki-Lyong;Chang, Young-Keun
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.33 no.11
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    • pp.95-105
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    • 2005
  • The HAUSAT-2 nanosatellite which is scheduled to launch in 2008 is being developed by SSRL(Space System Research Lab.). The HAUSAT-2 STM(Structural-Thermal Model) was developed as the first system model to verify structural and thermal design margin. The qualification level vibration and thermal tests have been conducted on STM. This paper addresses the comparison of structural analysis and test results of HAUSAT-2 STM. It was shown that the natural frequency of HAUSAT-2 STM satisfies the stiffness requirements without structural damage in the random vibration test. The assembly and integration validity were also checked out through STM.

Optimum Design of Junctionless MOSFET Based on Silicon Nanowire Structure and Analysis on Basic RF Characteristics (실리콘 나노 와이어 기반의 무접합 MOSFET의 최적 설계 및 기본적인 고주파 특성 분석)

  • Cha, Seong-Jae;Kim, Kyung-Rok;Park, Byung-Gook;Rang, In-Man
    • Journal of the Institute of Electronics Engineers of Korea SD
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    • v.47 no.10
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    • pp.14-22
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    • 2010
  • The source/channel/drain regions are formed by ion implantation with different dopant types of $n^+/p^{(+)}/n^+$ in the fabrication of the conventional n-type metal-oxide-semiconductor field effect transistor(NMOSFET). In implementing the ultra-small devices with channel length of sub-30 nm, in order to achieve the designed effective channel length accurately, low thermal budget should be considered in the fabrication processes for minimizing the lateral diffusion of dopants although the implanted ions should be activated as completely as possible for higher on-current level. Junctionless (JL) MOSFETs fully capable of the the conventional NMOSFET operations without p-type channel for enlarging the process margin are under researches. In this paper, the optimum design of the JL MOSFET based on silicon nanowire (SNW) structure is carried out by 3-D device simulation and the basic radio frequency (RF) characteristics such as conductance, maximum oscillation frequency($f_{max}$), current gain cut-off frequency($f_T$) for the optimized device. The channel length was 30 run and the design variables were the channel doping concentration and SNW radius. For the optimally designed JL SNW NMOSFET, $f_T$ and $f_{max}$ high as 367.5 GHz and 602.5 GHz could be obtained, respectively, at the operating bias condition $V_{GS}$ = $V_{DS}$ = 1.0 V).

A System for Thermal Distortion Analysis of Hull Structures by Solar Radiation (선체의 태양복사 열변형 해석을 위한 전처리시스템)

  • Ha, Yunsok;Lee, Donghoon
    • Journal of the Society of Naval Architects of Korea
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    • v.53 no.4
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    • pp.275-281
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    • 2016
  • One of the most important things for quality to meet ship-production schedule is an accuracy control. A ship is assembled by welding through whole production process, so it is important that loss by correction will not happen as much as possible by using some engineering skills like reverse design, reverse setting and margin for thermal shrinkage. These efforts are a quite effective in fabrication stages, but not in erection stages. If a ship block which consists of common steel is exposed to directional solar radiation, its dimensional accuracy will change high as time by its thermal expansion coefficient. Therefore, the measuring work would be often done at dawn or evening even with having a very accurate device. In this study, an FE analysis method is developed to solve this problem. It can change measured data affected by solar thermal distortion to ones not, even though ship-block is measured at an arbitrary time. It will use the time when measuring, the direction of block and the weather record by satellites. It is confirmed by a comparison between measured data of a ship-block and the result by suggested analysis method. Furthermore, a pre-processing system is also developed for fast application of the suggested analysis method.

Thermal Design on the Backplane of GPS Antenna of Low Earth Orbit Satellite (지구저궤도위성 GPS 안테나 후판 열설계)

  • Hyun, Bum-Seok;Lee, Jang-Joon
    • Aerospace Engineering and Technology
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    • v.10 no.1
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    • pp.136-140
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    • 2011
  • In this study, thermal model for backplane of GPS antenna in Low Earth Orbit Satellite is updated and orbit thermal analysis is performed. The analysis is focused on the safehold mode of satellite. During the safehold mode, the solar panel is constantly looking to the Sun, and there is not a mission maneuvering. Therefore, antenna backplane receives the maximum heat influx considering the End-Of-Life condition. To maintain the temperature of antenna within allowable limits, radiating tape is applied and its area is determined. Besides, to verify the lowest temperature of the antenna, cold case with Begin-Of-Life analysis is also performed.

Loss of Coolant Accident Analysis During Shutdown Operation of YGN Units 3/4

  • Bang, Young-Seok;Kim, Kap;Seul, Kwang-Won;Kim, Hho-Jung
    • Nuclear Engineering and Technology
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    • v.31 no.1
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    • pp.17-28
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    • 1999
  • A thermal-hydraulic analysis is conducted on the loss-of-coolant-accident (LOCA) during shutdown operation of YGN Units 3/4. Based on the review of plant-specific characteristics of YGN Units 3/4 in design and operation, a set of analysis cases is determined, and predicted by the RELAP5/MOD3.2 code during LOCA in the hot-standby mode. The evaluated thermal-hydraulic phenomena are blowdown, break flow, inventory distribution, natural circulation, and core thermal response. The difference in thermal-hydraulic behavior of LOCA at shutolown condition from that of LOCA at full power is identified as depressurization rate, the delay in peak natural circulation timing and the loop seal clearing (LSC) timing. In addition, the effect of high pressure safety injection (HPSI) on plant response is also evaluated. The break spectrum analysis shows that the critical break size can be between 1% to 2% of cold leg area, and that the available operator action time for the Sl actuation and the margin in the peak clad temperature (PCT) could be reduced when considering uncertainties of the present RELAP5 calculation.

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Investigation on damage assessment of fiber-reinforced prestressed concrete containment under temperature and subsequent internal pressure

  • Zhi Zheng;Yong Wang;Shuai Huang;Xiaolan Pan;Chunyang Su;Ye Sun
    • Nuclear Engineering and Technology
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    • v.55 no.6
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    • pp.2053-2068
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    • 2023
  • Following a loss of coolant accident (LOCA), prestressing concrete containment vessels (PCCVs) may experience high thermal load as well as internal pressure. The high temperature stress would increase the risk of premature damage to the containment, which reduces the safety margin during the increasing internal pressure. However, current investigations cannot clearly address the issues of thermal-pressure coupling effect on damage propagation and thus safety of the containment. Thus, this paper offers three simple and powerful damage parameters to differentiate the severity of damage of the containment. Moreover, despite of the temperature action severely threatening the pressure performance of the containment, the research regarding the improvement of the resistant performance of the containment is quite scarce. Therefore, in this paper, a comprehensive comparison of damage propagation and mechanism between conventional and fiber-reinforced concrete (FRC) containments is performed. The effects of fiber characteristics parameters on damage propagation of structures following the LOCA are also specifically revealed. It is found that the proposed damage indices can properly indicate state of damage in the containment body and the addition of fiber can be used to obviously mitigate the damage propagation in PCCV considering the thermal-pressure coupling.

Experimental Investigation of Forced Air Cooled Plate Fin Heat Sinks (강제 공냉 평판형 핀 방열판에 대한 실험적 고찰)

  • Kim, Tae-Yeop
    • The Transactions of the Korean Institute of Power Electronics
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    • v.24 no.6
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    • pp.428-437
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    • 2019
  • Analytical thermal models based on average convection heat transfer are frequently used for the design and selection of forced air-cooled plate fin heat sinks. In this paper, a convection heat transfer model within a ±10% margin of error was presented through experimental investigation. Five types of heat sinks with inlet widths of 1.7-6.8 mm were tested at 50-160 W heat sources to derive and verify the model. Causes of error between the experiment and analytical thermal model were analyzed and listed to design the heat sink. Using proposed method and the lists to be considered in the paper, a quick and accurate heat sink design of the power-conversion system is expected.

A study on characteristics of crystallization according to changes of top structure with phase change memory cell of $Ge_2Sb_2Te_5$ ($Ge_2Sb_2Te_5$ 상변화 소자의 상부구조 변화에 따른 결정화 특성 연구)

  • Lee, Jae-Min;Shin, Kyung;Choi, Hyuck;Chung, Hong-Bay
    • Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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    • 2005.11a
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    • pp.80-81
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    • 2005
  • Chalcogenide phase change memory has high performance to be next generation memory, because it is a nonvolatile memory processing high programming speed, low programming voltage, high sensing margin, low consumption and long cycle duration. We have developed a sample of PRAM with thermal protected layer. We have investigated the phase transition behaviors in function of process factor including thermal protect layer. As a result, we have observed that set voltage and duration of protect layer are more improved than no protect layer.

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