• 제목/요약/키워드: natural gas cooling

검색결과 97건 처리시간 0.029초

천연가스냉방의 경제성 분석 연구 (A Study on Economic Analysis of Natural Gas Cooling)

  • 김기호
    • 한국가스학회지
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    • 제17권1호
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    • pp.42-48
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    • 2013
  • 한반도의 지구 온난화는 세계에서 가장 빠른 속도로 진행되고 있고, 이상기후 현상도 날로 심화되고 있다. 따라서 하절기의 혹서와 동절기의 혹한으로 인한 전력수요가 급증함에 따라 우리나라의 전력 수급상황은 매우 어려운 상황에 있다. 현재 천연가스는 현존하는 화석연료 중 온실가스 배출이 가장 적어서 공급이 확산되고 있다. 천연가스냉방은 전력피크 완화는 물론, 발전소 추가 건설비용의 절감, 천연가스 저장설비의 효율적 운영 및 분산형 전원으로서의 역할수행도 가능한 장점이 있다. 따라서 본 연구는 전력 부하관리의 대안으로서 천연가스냉방의 경제성을 분석하였다.

자연대류를 고려한 전류도입선의 최적설계 (Optimal design of Current lead considering Natural convection)

  • 손봉준;설승윤
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2003년도 추계학술대회
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    • pp.103-108
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    • 2003
  • In this paper, the current lead for superconducting device is studied by numerical method. The current lead is cooled by surrounded $N_{2}$ gas by natural convection. The heat conduction equation for current lead and boundary layer equation for $N_{2}$ gas must be solved simultaneously. The boundary layer equation for $N_{2}$ gas is highly nonlinear for varied temperature of current lead. So the linearization method is adopted for simplicity. Numerical results using natural convection cooling are compared with the conventional cooling methods such as conduction cooling and vapor cooling methods. The main difference of natural convection cooing is the non-zero temperature gradient at the top of current lead for the minimum heat dissipation into superconducting devices. For the optimized conduction-cooling and vapor-cooling current leads, the temperature gradient at the top of current lead is zero. Also, the heat flow at the cold end is much smaller than conduction cooling case.

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Evaluation on the Characteristics of Liquefied Natural Gas as a Fuel of Liquid Rocket Engine

  • Namkoung, Hyuck-joon;Han, Poong-Gyoo;Kim, Kyoung-Ho
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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    • pp.148-154
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    • 2004
  • As a rocket propellent of hydrocarbon fuels, the characteristics of liquefied natural gas was evaluated with the viewpoint of the constituents and content, the cooling performance as a coolant, and characteristic velocity and specific impulse as parameters of the engine performance. Content of methane was a principal factor to determine the characteristics as a rocket propellant and more than 90 % of it was needed as a fuel and coolant in the regenerative cooled liquid rocket engine. Some constituents of the liquefied natural gas can be frozen by the pre-cooling of the pipe lines, therefore they can be a factor disturbing the normal working of engine. In case the content of methane is around 90% in the liquefied natural gas, a normalized stoichiometric O/F mixture ratio of 0.75 is suggested for a nominal operation condition to get the maximum specific impulse and characteristic velocity.

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SF6 가스를 충전한 변압기의 자연순환 냉각시스템의 성능시뮬레이션 (Performance Simulation of Natural Circulating Cooling System of SF6 Gas Charged Transformer)

  • 최영돈;허창수;김진봉
    • 설비공학논문집
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    • 제6권1호
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    • pp.54-65
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    • 1994
  • Performance of naturally circulating cooling system of $SF_6$ gas charged transformer was simulated and the variations of gas flow rate, maximum coil temperature, gas temperature and cooling air temperature were investigated with respect to the height of radiator, interplates distance and heat generation rate at core. The results show that the height of radiator most significantly affects the performance of natural circulating cooling system of transformer.

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가스터빈 내부 냉각계통 발화에 의한 고온부품 손상의 현상학적 고찰 (A Phenomenological Review on the Damage of Hot Gas Parts caused by Explosion of Gas Turbine Cooling System)

  • 유원주;이승현
    • 대한안전경영과학회지
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    • 제12권2호
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    • pp.75-82
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    • 2010
  • Gas turbines for power generating operate in a very high temperature condition and use natural gas for fuel. For this reason, many cases of damage happen at hot gas parts which are severely affected by high temperature gas and many cases of explosion occur by fuel gas. So a lot of efforts should be made to prevent hot gas parts damage and gas explosion accidents. Though there are many damage cases and explosion accidents, it is very difficult to find out the root causes of hot gas parts damage caused by gas explosion due to gas leakage in the heat exchanger for air cooling and gas heating. To prevent gas turbine from damage caused by gas explosion, removal of leakage gas from gas turbine is inevitably required before firing the gas turbine and installing alarm systems is also required for detecting gas leakage at stop valve to turbine while shut down.

Study on Gas Hydrates for the Solid Transportation of Natural Gas

  • Kim, Nam-Jin;Kim, Chong-Bo
    • Journal of Mechanical Science and Technology
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    • 제18권4호
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    • pp.699-708
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    • 2004
  • Natural gas hydrate typically contains 85 wt.% water and 15 wt.% natural gas, and commonly belongs to cubic structure I and II. When referred to standard conditions, 1 ㎤ solid hydrate contains up to 200㎥ of natural gas depending on pressure and temperature. Such the large volume of natural gas hydrate can be utilized to store and transport a large quantity of natural gas in a stable condition. In the present investigation, experiments were carried out for the formation of natural gas hydrate governed by pressure, temperature, gas compositions, etc. The results show that the equilibrium pressure of structure II is approximately 65% lower and the solubility is approximately 3 times higher than structure I. It is also found that for the sub-cooling of structure I and II of more than 9 and 11 K respectively, the hydrates are rapidly being formed. It is noted that utilizing nozzles for spraying water in the form of droplets into the natural gas dramatically reduces the hydrate formation time and increases its solubility at the same time.

가스터빈 내부 냉각계통 발화에 의한 고온부품 손상의 현상학적 고찰 (A Phenomenological Review on the Damage of Hot Gas Parts caused by Explosion of Gas Turbine Cooling System)

  • 유원주;이승현
    • 대한안전경영과학회:학술대회논문집
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    • 대한안전경영과학회 2010년도 춘계학술대회
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    • pp.81-95
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    • 2010
  • Gas turbines generating power operate in high temperature condition and use natural gas as fuel. For that reason, there are many cases where damage is done to the hot gas parts caused by the high temperature and many accidents occur like gas explosions, then various efforts are needed to maintain the hot gas parts and prevent accidents. It is difficult to find the root causes of damage to the hot gas parts from the gas explosion caused by gas leakage through rotor cooling air line from fuel gas heat exchanger during the shut down. To prevent gas turbine from damage, removal of gas leakage inside of gas turbine is required by purging the turbine before firing, improving the fuel gas heating system and installing alarm systems for detecting gas leakage from stop valve to turbine while the gas turbine has shut down.

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LNG 냉열 에너지의 지역 냉방 시스템에 관한 기반 연구 (A Basic Study on the District Cooling System of LNG Cold Thermal Energy)

  • 김청균
    • 한국가스학회지
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    • 제7권4호
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    • pp.36-43
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    • 2003
  • 본 논문에서는 LNG 냉열 에너지를 활용한 지역 냉방 시스템 가능성에 대해 고찰하고자 한다. 액상의 LNG는 기상의 가스로 변환하는 과정에서 많은 냉열 에너지를 발생한다. 최근에 빙축열을 이용한 건물의 냉방 시스템 구축과 심층수를 이용한 지역 냉방 시스템이 도심지의 기존 사무실 건물이나 대규모 건물의 냉방장치로 도입되고 있는 상황이다. LNG의 냉열 에너지는 기존의 냉매에 의존한 개별 냉방 시스템을 대체하는 새로운 냉열 에너지 공정으로 쾌적한 공간을 제공하는 천연의 대규모 냉각매체로 재사용될 수 있다. 버려지는 냉열 에너지는 낮은 코스트로 운영될 수 있는 중요한 청정 에너지원이기 때문에 냉방 시스템으로 개발되면, 기존의 에어콘 시스템에 견주어 볼 때 공기중에 유해한 오염원의 발생과 환경적으로 유해한 냉매 방출을 대폭적으로 줄일 수 있는 우수한 냉방 시스템이 될 것이다. 따라서, 본 연구에서는 냉열 에너지를 활용한 지역 냉방 시스템에 대한 환경 친화적 기본적 설계 개념, 여러 가지 냉방 시스템 성능에 대한 유익한 기반적 정보를 제공하고자 한다.

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HTS변압기에서 액체질소 표면 상부의 열전달 해석 (Heat Transfer Analysis above L$N_2$ Surface in HTS Transformer)

  • 최연석;장호명
    • 한국초전도저온공학회:학술대회논문집
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    • 한국초전도저온공학회 2003년도 학술대회 논문집
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    • pp.174-177
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    • 2003
  • Cooling load from the top plate to L$N_2$ surface, including wall conduction, gas conduction, radiation, and current leads, is investigated in a closed cooling system for HTS transformer. In general methods of load calculation, individual load is estimated separately, but they are actually coupled each other because of natural convection of nitrogen vapor. Using heat transfer analysis, we calculate cooling load with taking into account the effect of natural convection. Cooling load is under- estimated approximately 2 % when the natural convection is ignored. If the operating current is high, there will be a wide difference between actual cooling load and cooling load by individual calculation. Cooling load decreases with increasing number of radiation shield. With production, construction, and cooling load, three radiation shields are proper to 1 MVA HTS transformer.

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액화천연가스를 연료로 하는 시험용 액체로켓엔진의 성능해석 (Performance Analysis of the Experimental Liquid Rocket Engine using Liquefied Natural Gas as a Fuel)

  • 한풍규;이성웅;김경호;윤영빈
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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    • pp.198-204
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    • 2004
  • 액화천연가스를 연료로 사용하여 물 냉각 및 천연가스와 액화천연가스 재생냉각 연소시험을 수행하였다. 연소시험과 CEC86을 이용한 연소해석 결과를 액체로켓엔진 성능인자로서, 특성속도와 비추력 관점에서, 추진제 혼합비와 연료의 연소실 유입온도의 영향을 분석하였으며, 엔진성능이 추진제 혼합비와 연료의 연소실 유입온도의 영향을 크게 받고 있음을 알 수 있었다. 엔진 성능으로서 특성속도는 추진제 혼합비가 0.72∼0.75일 때, 이론적 비추력은 추진제 혼합비가 0.75일 때 최대 값을 보여주었으며, 연료의 연소실 유입온도의 증가에 비례하여 엔진 성능이 향상되는 경향에서 재생냉각이 엔진 성능을 증대시키는 경향을 확인하였다.

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