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논문검색

가스터빈 내부 냉각계통 발화에 의한 고온부품 손상의 현상학적 고찰

원문정보

A Phenomenological Review on the Damage of Hot Gas Parts caused by Explosion of Gas Turbine Cooling System

유원주, 이승현

피인용수 : 0(자료제공 : 네이버학술정보)

초록

영어

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.

목차

Abstract
 1. 서론
 2. 가스터빈 고온부품의 손상 경향
  2.1 열화에 의한 소손
  2.2 이물질 충격에 의한 물리적 손상
  2.3 크리프 및 피로에 의한 균열손상
 3. 부품별 손상형태와 원인분석
  3.1 연료가스 열교환기 손상
  3.2 연소실 고온부품 손상
  3.3 터빈 고온부품 손상
  3.4 터빈 냉각용 공기 Filter 손상
 4. 현상학적고찰을통한손상메커니즘규명
  4.1 가스 누설 과정
  4.2 발화 과정
  4.3 터빈 냉각공기용 Filter 손상 과정
  4.4 연료가스 열교환기 손상 과정
  4.5 터빈과 연소실 고온부품 손상 과정
 5. 결론
 6. 참고문헌

저자정보

  • 유원주 Won-Ju Yu. 한국동서발전(주)
  • 이승현 Seong-Hyun Lee. 한국동서발전(주)

참고문헌

자료제공 : 네이버학술정보

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