• Title/Summary/Keyword: 내열 알루미늄

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알루미늄도금강판의 표면 및 계면특성

  • Jeong, Yong-Seok;Heo, Seon-Hwa;Lee, Gyu-Yong
    • Proceedings of the Korean Vacuum Society Conference
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    • 2011.02a
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    • pp.503-503
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    • 2011
  • 알루미늄 도금강판은 Al-10%Si의 Type 1과 100%Al의 Type2로 구분되어 진다. 그러나, 국내에서는 Type1만이 생산되고 있으며, Zn이 주요성분이 되는 도금강판대비 내열성이 우수하여, 고온기기나 자동차용 배기계 등에 상용되고 있다. 이러한 알루미늄 도금강판의 특성은 표면조직이나, 소재에 도금층과 반응하여 형성된 계면합금층의 특성에 따라, 내열성, 가공성, 내식성 등의 물성에 큰 영향을 미친다. 특히, 합금층은 매우 취성이 강하여 도금층의 박리 등을 유발할수 있으며, 고온에서는 합금층이 성장하여, 내열성 등 물성에 영향을 미친다. 그러나, 이러한 합금층의 결정구조나 조직에 대해서도 연구자간의 분석결과가 일치하지 않으며, 합금층의 고온에서의 거동에 대해서도 잘 이해되지 않고 있다. 본 연구에서는 이러한 합금층에 대한 문헌조사 및 내열실험을 통하여 합금층거동을 분석하고자 하였으며, 또한, 이상적인 도금구조를 갖는 건식도금 샘플을 제작하여 합금층의 내열특성을 상호 비교하였다. 본 발표에서는 이러한 결과를 제시한고자 한다.

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입자포집장치를 이용한 산화알루미늄 입자의 포집 및 분석

  • 이도형;윤명원;배주찬;윤덕진;김명철
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 1999.04a
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    • pp.18-18
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    • 1999
  • 추진제의 비추력 및 밀도 등을 효과적으로 증진시키기 위해 알루미늄 분말의 함량을 높인 고 알루미늄 추진제가 로켓모터에 널리 사용되고 있다. 추진제 내 알루미늄 성분은 연소과정의 이상유동으로 인하여 로켓의 성능 및 내열설계에 많은 영향을 미칠 수 있다. 즉, 산화알루미늄 입자가 노즐 벽면에 달라붙어 추력의 손실을 가져오기도 하고 노즐 입구에 침적되어 내열재의 삭마가 과다해져 최악의 경우 모터의 파손을 일으켜 임무수행에 실패를 초래할 수도 있다.

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Effects of Aluminum Oxide Particles on the Erosion of Nozzle Liner for Solid Rocket Motors (고체 추진기관에서 산화알루미늄 입자가 노즐 내열재의 삭마에 미치는 영향)

  • 황기영;임유진;함희철
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.34 no.8
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    • pp.95-103
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    • 2006
  • The compositions, the gas properties in motor chamber and the aluminum oxide (Al2O3) particle size for two kinds of solid propellants with approximately 20% aluminum powder have been investigated. The SEM photographs of $Al_2O_3$ taken from nozzle entrance liner show that the aluminized PCP propellant with 47% volumetric fraction AP/HNIW and bimodal oxidizer 200-5 ${\mu}m$ can offer greater possibility for increasing aluminum agglomeration than the aluminized HTPB propellant with 64% volumetric fraction AP and trimodal oxidizer 400-200-6 ${\mu}m$. The nozzle entrance liner of solid rocket motor with the PCP propellant shows greater erosion at 4 circumferential sections in line with grain slots due to the impingement of large particles, but that with the HTPB propellant shows uniform erosion with circumferential angle.

Effects of Solid Propellant Cases on the Thermal Response of Nozzle Liner (노즐 내열재 열반응에 미치는 고체 추진제 연소가스의 영향)

  • Hwang, Ki-Young;Yim, Yoo-Jin;Ham, Hee-Cheol;Kang, Yoon-Goo;Bae, Joo-Chan
    • Journal of the Korean Society of Propulsion Engineers
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    • v.11 no.2
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    • pp.26-36
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    • 2007
  • The thermal response characteristics of nozzle liner for a solid rocket motor applying highly aluminized PCP or HTPB propellant with slotted tube grain have been investigated. The SEM photographs of aluminum oxide particles taken from nozzle liner show that the PCP propellant with the finer and less contents of oxidizer can offer greater possibility for increasing aluminum agglomeration than the HTPB propellant. The PCP propellant shows locally greater mechanical erosion at 4 circumferential areas of the nozzle entrance in line with grain slot due to the impingement of large particles, but the HTPB propellant shows greater thermochemical ablation at the nozzle blast tube, the throat insert and the exit cone because of relatively much more mole fraction of $H_2O\;and\;CO_2$ in combustion gases.

Study on the Flame Retardation and Thermal Resistance for CPE Rubber Material Added Etching By-product of Aluminum (알루미늄 엣칭부산물을 첨가한 CPE 고무재료의 난연성 및 내열성 연구)

  • Kim, Kyung Hwan;Lee, Chang Seop
    • Journal of the Korean Chemical Society
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    • v.45 no.4
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    • pp.341-350
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    • 2001
  • Aluminum Hydroxide was employed as a thermal retardent and flame retardent for Chloropolyethylene (CPE) rubbery materials which is the construction material of automotive oil cooler hose. and then cure characteristics, physical properties, thermal resistance and flame retardation of compounded rubber were investigated, and optimum mixing conditions of rubber and flame retarding agent were deduced from the experimental results. CPE rubber material which has excellent properties of chemical corrosion resistance and cold resistance and inexpensive in price was used to prepare rubber specimen. The by-product of ething, produced from the process of surface treatment of aluminum was processed to aluminum hydroxide via crushing and purification, which is characterized by XRD, PSA, SEM and ICP-AES techniques in terms of phase, size, distribution, morphology and components of particles and then mixed to CPE rubber materials in the range of 0~80 phr. Hardness, tensile strength, elongation and thermal properties of compounded rubber specimens were tested. The optimum mixing ratio of rubber to additives to give maximum effect on thermal resistance and flame retardation, within the range of tolerable specification for rubber materials, was determined to be 40 phr. The flame retardation of CPE rubber materials was found to be increased by 5 times at this mixing ratio.

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High Temperature Fatigue Behavior of A356 and A319 Heat Resistant Aluminum Alloys (A356 및 A319 내열 알루미늄 합금의 고온 피로 변형 거동)

  • Park, Jong-Soo;Sung, Si-Young;Han, Bum-Suck;Jung, Chang-Yeol;Lee, Kee-Ahn
    • Proceedings of the Korean Society for Technology of Plasticity Conference
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    • 2009.10a
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    • pp.467-469
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    • 2009
  • In this study, fatigue samples were prepared from cylinder head parts that are actually used in domestic (A) and foreign (B) automobiles; high-temperature, high-cycle, and low-cycle fatigue characteristics were then evaluated and compared. A study on the correlation between the microstructural factor and high temperature fatigue characteristic was attempted. The chemical compositions of the heat resistant aluminum alloys above represented A356 (A) and A319 (B), respectively. The result of the tensile strength test on material B at $250^{\circ}C$ was higher by 30.8MPa compared to material A. On the other hand, elongation was 8.5% higher for material A. At $130{\circ}C$, material B exhibited high fatigue life given high cycle fatigue under high stress, whereas material A showed high fatigue life when stress was lowered. With regard to the low-cycle fatigue result ($250^{\circ}C$) showing higher fatigue life as ductility is increased, material A demonstrated higher fatigue life. Through the observation of the differences in microstructure and the fatigue fracture surface, an attempt to explain the high-temperature fatigue deformation behavior of the materials was made.

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가공 송전용 신전선의 개발동향

  • 이수홍;한광현;김신철
    • 전기의세계
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    • v.45 no.1
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    • pp.10-15
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    • 1996
  • 가공송전망 고전압화는 세계적으로는 1,000KV까지 검토되고 있으며 우리나라에서도 765KV를 시험 운전추진중에 있다. 송전선의 전류용량 증대방법으로서는 도체크기의 대형화, 다도체화 뿐만 아니라 경 알루미늄을 도체로 사용한 종래의 ACSR을 대체할 수 있는, 초내열 알루미늄선을 사용하여 허용전류를 증가시킨 STACIR의 채택이 확대되고 있다. 증용양화 송전선의 본격적 도입과 함께 송전선로 운영시에 발생하는 공해성, 환경저해성을 촤소화시키는 환경조화선로및 지역별 특성에 맞는 특수기능 전선에도 그 관심이 고조되고 있는바 도체재료와 구조에 대한 꾸준한 기술 개발로 송전선의 고신뢰화, 다기능화가 지속적으로 진행되고 있다. 우리나라의 경우도 1960년대에 ACRS이 가설된 이후 늘어나는 전력수요에 부응하기 위하여 1995년 STACIR의 154KV 의정부-동두천 송전선로 구간에 가설운전을 시작으로 신송전로의 시대에 진입했다고 볼 수 있다.

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Experimental study on the hydrophilic performance of pre-coated aluminum foil (알루미늄 호일의 친수코팅 성능 개선에 관한 실험적 연구)

  • 김영생;길용현;박환영;윤백;김자수소;김병열
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.11 no.6
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    • pp.725-732
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    • 1999
  • It is usual to use hydrophilic-coated aluminum foil for evaporator fin of air-conditioners to reduce air flow resistance caused by the water droplets condensed on the fin surface. The major effect of a hydrophilic coating is to reduce the contact angle of the condensate and prevent bridging of the condensate between the adjacent fins. The performance of hydrophilic coating generally tends to be degraded as it is used since the coating material is washed down by the condensate. In the present work, several types of hydrophilic coatings were evaluated in terms of durability of hydrophilicity, corrosion resistance and heat resistance. Results showed that an improved hydrophilic coating of resin type presented superb qualify in terms of durability and corrosion resistance while having almost the same level of qualify in heat resistance compared with the others.

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