• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2007.11a
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• pp.139-143
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• 2007

The overall results of combustion tests performed for a 30 tonf-class full-scale combustion chambers of a liquid rocket engine were described. The combustion chambers have chamber pressure of 53${\sim}$60 bar and propellant mass flow rate of 89 kg/so The combustion chamber is composed of mixing head, SUS baffle, baffle injector, ablative chamber, channel cooling chamber and regenerative cooling chamber. The test results show that the combustion characteristic velocity is in the range of 1673${\sim}$1730 m/sec and the specific impulse of the combustion chamber is in the range of 254${\sim}$263 sec. As the recess number of the injectors increases, the combustion characteristic velocity increases. And as the combustion characteristic velocity increases, the specific impulse of the combustion chamber also increases.

• Journal of the Korean Society of Propulsion Engineers
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• v.14 no.5
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• pp.92-100
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• 2010

Combustion stability rating tests of 75-tonf-class thrust chamber for technology demonstration were carried out at a low pressure. Two kinds of mixing heads were used in this study. One of them has injectors of 631 and the other has injectors of 721. Mixing head with injectors of 631 showed a self-oscillation instability at the chamber pressure of 30 bar. Mixing head with injectors of 721 showed that a high frequency combustion stability was maintained under the same pressure and the same mass flow rate. But mixing head with injectors of 721 generated a self-oscillation instability at the chamber pressure of 20 bar and it was found that stability boundary region was changed due to the configuration of a mixing head from these results.

• Environmental engineer
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• s.28
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• pp.20-22
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• 1988

• Environmental engineer
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• s.156
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• pp.12-19
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• 1999

• Environmental engineer
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• s.27
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• pp.30-33
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• 1988

• Proceedings of the Korea Institute of Fire Science and Engineering Conference
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• 2013.04a
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• pp.128-129
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• 2013

화재 현장에는 소방대원의 생명에 위협이 될 수 있는 다양한 연소가스가 발생하며, 소방대원의 안전에 다양한 연소가스의 농도를 실시간으로 측정하는 것은 매우 중요하다. 현재 무선통신 기술의 발달과 센서 기술의 발전으로 저전력, 소형의 센서를 이용하여 무선으로 화재현장의 온습도조건, 발생가스의 농도, 소방대원의 생체신호를 화재현장의 지휘센터로 보내주는 기술의 개발이 진행되고 있다. 이러한 추세에 맞추어 측정된 가스의 농도를 실시간으로 지휘센터로 송수신하는 기술의 연구가 활발히 진행 중이다. 본 연구는 화재환경에서 주로 발생되는 CO, NO2, NH3를 위주로한 고온의 환경에서 농도를 측정하기 위한 방법에 대한 연구이다.

• Aerospace Engineering and Technology
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• v.4 no.1
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• pp.171-178
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• 2005

An acoustic analysis of a fuel-rich gas generator for the drive of a turbopump in a liquid rocket engine has been performed and the length of a simulating duct has been determined by comparing the resonant frequency of unstable acoustic modes to simulate an actual flight model gas generator. To simulate more realistically, a realistic short-length simulating duct has been determined by considering 1 or 2 wavelength of the unstable modes. Duct-length adjustment to turbopump can be a method to suppress a combustion instability problem by decoupling of acoustic mode and combustion characteristics. This method has been set up and validated with acoustic analysis and hot firing tests.

• Journal of the Korean Institute of Gas
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• v.21 no.1
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• pp.52-58
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• 2017

According to 2015 ministry of public safety and security statistics, product of combustion makes the most victims while fire. for that reason, recent studies about combustion products have been researched actively in domestic and foreign papers. In domestic, study is handling the combustion product effects on human body and flame propagation. Foreign study is conduct about combustion product effects to shelter in offshore and toxic effects on human. because combustion product is toxic and disturb escape by block the view, many research conducted about optimize combustion product removal facilities using dispersion experiments and CFD simulations. In this study, this paper analysed research trend about toxic gas production model while combustion and its removal facilities, it will be the standard of combustion products research.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2008.11a
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• pp.45-48
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• 2008

Micro power generators have been studying to provide high power that micro systems require. Micro power generators need micro combustor. Swiss-roll combustor has been studied about scale, geometry, material. From previous study experiments have shown that swiss-roll combustors require thin walls with low thermal conductivity for maximum performance at small scales. In this work, polyimide combustors with low thermal conductivity and thin thickness are built and tested.

• Proceedings of the KIEE Conference
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• 2011.07a
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• pp.1848-1849
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• 2011

Oxy-PC 발전시스템은 화석 연료를 연소하는 과정에서 발생하는 다량의 이산화탄소를 회수처리 하기위해 고려되고 있는 방법 중 하나이며, 신규 발전 시스템은 물론이며 기존 발전시스템에도 개조 과정을 거쳐 적용이 용이한 장점이 있다. 하지만 현재 국내에 해당 시스템의 적용 사례는 없을 뿐만 아니라 설계 기술의 확보도 부족한 실정이다. 따라서 순산소 연소 시 발생하는 복합적인 문제를 사전에 예측하고 시스템 구현 과정에서 발생되는 시행착오를 최소화하기 위해서는 순산소 연소 공정모델을 반영한 Dynamic Engineering Simulator 개발이 요구된다. 본 논문에서는 Oxy-PC 발전 시스템의 특징을 기존 공기 연소 발전 시스템과 비교하여 설명하고 Oxy-PC 발전 플랜트용 Dynamic Engineering Simulator 개발 절차에 대해 기술한다.