가스터빈 연소기 기본 설계 기법 소개

Introduction to preliminary design tool for gas turbine combustors

  • 김대식 (강릉원주대학교 기계자동차공학부) ;
  • 유경원 (국방과학연구소 제4본부) ;
  • 황기영 (국방과학연구소 제4본부) ;
  • 민성기 (국방과학연구소 제4본부)
  • 발행 : 2013.06.21

초록

Gas turbine technology has steadily advanced since its inception and continues to evolve. Development is active in producing both smaller gas turbines and more powerful and efficient engines. However, it is shown that our state-of-the-art technologies for gas turbine developments remain at a basic level by comparisons with advanced technology countries. This paper shows that development process and preliminary design tools for gas turbine combustor were introduced as a first results of source technology secure researches for the gas turbine combustors.

키워드