Development Trends of Combustor Technology for Jet Engines

제트엔진용 연소기 개발기술 동향

  • 민성기 (국방과학연구소 제3체계개발본부) ;
  • 임진식 (국방과학연구소 제3체계개발본부)
  • Published : 2004.03.01

Abstract

The advanced technology of jet engine combustor such as high temperature composite materials is being developed to enhance the life of turbine and to minimize pollutants emission in foreign countries. The domestic development status of combustor for jet engine are only limited to the basic technology of small engine combustor. The development program of combustor are required to improve current technology.

제트엔진용 연소기는 선진국에서는 터빈수명을 증대시키고, 공해물질 생성을 최소화하기 위해 고온 내열 복합재와 같은 첨단 기술개발이 진행되고 있다. 국내에서는 소형엔진용 연소기 개발기술에 국한되어 있으나, 향후 지속적인 기술발전을 위해 제트엔진용 연소기 개발프로그램의 도출이 요구된다.

Keywords

References

  1. Gas Turbine Combustion, Arthur H. Lefebvre, Hemisphere Publishing Corporation, 1983
  2. The Design and Development of Gas Turbine Combustors, Vol. I., Northern Research and Development Corporation, 1980
  3. Gas Turbine Engine Emissons-Problems, Progress and Future, Robert E. Jones, Prog. Energy Combustion Science, vol. 4. 1978, pp.73-113 https://doi.org/10.1016/0360-1285(78)90006-0
  4. Critical Technologies Plan for the Committees on Armed Services United States Congress, The Department of Defense, Washington D.C., U.S.A., 1991
  5. Overview of the NASA AST and UEET Emissions Reduction Projects, John Rohde, NASA Gleen Research Center, 2002
  6. NASA's Ultra Efficient Engine Technology (UEET) Program, Joe Shaw, NASA Glenn Research Center, 2002
  7. Propulsion Technology Partnerships for the New Millennium : A View From The Pentagon, Paul F. Piscopo, Office of Deputy Under Secretary of Defense, 1999
  8. Small Engine Component Technology (SECT) Study Program Final Report, E. Almodovar et' aI, AVCO Lycoming Division, 1986
  9. Small Engine Component Technology (SECT) Study Program Final Report, B. Singh, Teledyne CAE, 1986
  10. Small Engine Component Technology (SECT) Study Program Final Report, T. R. Larkin, Allison Gas Turbine Division, General Motors Corporation, 1986
  11. www.pr.wpafb.af.mil/divisions/prt/ ihptet/ihptet.html
  12. 항공기용 가스터빈 연소기의 연료노즐 설계 및 실험연구, 공창덕 외, 항공우주학회지 vol.23 no.2, 1995, pp.52-60
  13. HSNS 연료노즐 및 스월러 실험연구, 민성기 외, 항공우주학회지 vol.26 no.8, 1998, pp.92-104
  14. Ignition characteristics on the annular combustor with rotating fuel injection system, J,B.Park et aI, Proc. of ASME Turbo expo 2004, June 14-17, 2004