• Title/Summary/Keyword: 재생냉각유로

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추력 30톤급 연소기의 냉각 성능

  • Cho, Won-Kook;Lee, Soo-Yong;Cho, Gwang-Rae
    • Aerospace Engineering and Technology
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    • v.3 no.1
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    • pp.197-204
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    • 2004
  • A design of regenerative cooling system of 30 ton level thrust combustion chamber for ground test has been performed. The 1-D design code has been validated by comparing with the heat flux of the NAL calorimeter for high chamber pressure and water-cooling performance of the ECC engine of MOBIS. The present design code has been confirmed to predict accurately the heat flux and water-cooling performance for high chamber pressure condition. The maximum hot-gas-side wall temperature is predicted to be about 720 K without thermal barrier coating and the coolant-side wall temperature is less than the coking temperature of RP-1. The coolant temperature rises nearly 100 K with thermal barrier coating when Jet-A1 is used as coolant.

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The Structural Design for Combustor Chamber of Liquid Rocket Engine (액체로켓엔진 연소기 챔버 구조 설계)

  • Chung Yong-Hyun;Ryu Chul-Sung
    • Journal of the Korean Society of Propulsion Engineers
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    • v.8 no.4
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    • pp.36-42
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    • 2004
  • The Properties of material, C18200 which is used for development of high performance liquid rocket engine combustor chamber were obtained by tension tests. The specimen for regenerative combustor was designed by structural analysis using that Properties. After the designed specimen was manufactured by the same manufacturing process of regenerative combustor. the yielding stress and yielding strain were obtained by strength tests. The properties of C18200 was degraded very much after brazing. The estimation of yielding pressure by structural analysis was almost same as that of strength test. The collector Part was yielded and failed previously than that of cooling channel part during strength test.

Cooling Performance Analysis of a Sub-scale Calorimeter (축소형 칼로리미터의 냉각성능 해석)

  • 조원국;문윤완
    • Journal of the Korean Society of Propulsion Engineers
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    • v.7 no.3
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    • pp.8-14
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    • 2003
  • A cooling performance analysis has been made in the 8-channel calorimeter based on sub-scale KSR-III engine. Three-dimensional heat transfer analysis in cooling channels has been performed using the heat flux distribution through the chamber wall predicted from axi-symmetric compressible flow inside the combustion chamber. The heat flux distribution is verified against the published literature. Presented for the development and operation of the calorimeter are the coolant pressure drop, coolant temperature rise and the maximum chamber wall temperature. Required coolant flow rate is determined for given chamber pressure. Cooling performance is also predicted for temperature dependant coolant properties.

A Case Study on the Design of Kerosene-LOx Liquid-Propellant Rocket Engines for Performance Enhancement (케로신-액체산소 액체로켓엔진의 성능향상 설계안 사례 조사)

  • Lee, Seon-Mi;Moon, In-Sang;Lee, Soo-Young
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2011.04a
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    • pp.12-15
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    • 2011
  • The most widely used kerosene-LOx liquid-propellant rocket engines in these days have a similar engine schematic to those of the past because of the development cost and the reliability. The efficiency of engines could be increased by the factors such as a cooling method, engine cycles, shape of cooling channels, additional coolant and so on. In this article, it is described that some design ideas for performance enhancement by exchange kerosene with LOx of a coolant.

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Performance Evaluation of Plate Membrane Humidifier for PEMFC (고분자전해질연료전지용 판형막가습기 성능 평가)

  • Kho, Back Kyun;Park, JongCheol;Lim, Jongkoo;Kwon, Ki Wook;Shin, Hyun Khil;Hur, Tae Uk;Cho, Sungbaek
    • 한국신재생에너지학회:학술대회논문집
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    • 2010.11a
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    • pp.88.2-88.2
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    • 2010
  • 고분자전해질연료전지(PEMFC)의 성능은 고분자막의 이온전도도에 따라 큰 영향을 받으며 가습조건에 따라 연료의 수화정도에 비례하여 증가하는 경향을 보인다. 현재 고분자막을 가습하는 방법에는 여러 가지가 있는데, PEMFC에 많이 사용되고 있는 Bubbler 형태의 가습장치는 고온이 필요하며 가습 효율이 수동적인 단점을 가지고 있다. 이에 비해서 막을 이용한 가습방법은 스택의 냉각시스템을 이용하여 가습 시, 별도의 에너지가 필요하지 않다. 이에 본 연구에서는 비교적 저온에서도 가습 효율이 증대하고 시스템 간소화의 장점을 가진 막가습기를 제작하여 고분자전해질 연료전지에서 열 및 습도조절에 대한 효율성을 비교 연구하였다. 막가습기에 사용된 가습막의 두께에 따른 가습도 변화 및 유로 구조에 따른 압력강화를 관찰하였으며 막가습기를 판형 모듈 형태로 제작하여 고분자전해질연료전지에 적용하여 성능을 평가하였다.

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Assessment of Practical Use of Recycling Oil from the Pyrolysis of Mixed Waste Plastics (혼합폐플라스틱의 열분해를 통한 회수오일의 이용가능성 평가)

  • Phae Chae-Gun;Kim Young-shin;Jo Chang-Ho
    • Journal of Energy Engineering
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    • v.14 no.2 s.42
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    • pp.159-166
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    • 2005
  • In Korea, although the generation of waste plastic has been increasing, the rate of recycling is considerably low and moreover, there is no suitable method for the treatment of waste plastics. However, pyrolysis, which is appropriate for the treatment of highly polymerized compounds, such as plastics, has recently gained much interest. In this study, a property of the products from the pyrolysis of mixed waste plastics, with a possible practical use for the recycling oil produced, were assessed. First of all, in order to investigate the pyrolysis characteristic of waste plastics, TGA (Thermogravimetric analysis) and DCS (Differential Scanning Calorimetry) were performed on a number of different plastics, including PP, LDPE, HDPE, PET and PS, as well as others. According to the result, it appeared that PP was the most efficiently pyrolyzed by changing the temperature, followed by LDPE, HDPE, PET, PS and the other plastics, in that order. From the results, the optimum conditions f3r pyrolysis were set up, and the different waste plastics pyrolyzed. The recycling oil produced from the flammable gases generated during the pyrolysis was com-pared with fuel oil by an analysis using the petroleum quality inspection method on KS(Korea industrial Standard). The results of the analysis showed the recycling oil was of a similar standard to fuel oil, with the exception of the ignition point, with a quality somewhere between that of paraffin oil and diesel fuel. With respect to these results, the quality of the recycling oil produced by the pyrolysis of waste plastics was suf-ficient for use as fuel oil.