한국연소학회지 (Journal of the Korean Society of Combustion)

  • 제18권3호
  • /
  • Pages.61-67
  • /
  • 2013
  • /
  • 1226-0959(pISSN)
  • /
  • 2466-2089(eISSN)
한국연소학회 (The Korean Society of Combustion)
권호 표지
DOI QR코드

DOI QR Code

항공용 가스터빈 연소기 기본 설계 프로그램 개발 : Part 2 - 공기 유량 배분

Preliminary Design Program Development for Aircraft Gas Turbine Combustors : Part 2 - Air Flow Distribution

  • 김대식 (강릉원주대학교 기계자동차공학부) ;
  • 유경원 (국방과학연구소 제4본부) ;
  • 황기영 (국방과학연구소 제4본부) ;
  • 민성기 (국방과학연구소 제4본부)
  • 투고 : 2013.07.13
  • 심사 : 2013.09.15
  • 발행 : 2013.09.30
PDF 다운로드
⟨ 이전 논문 다음 논문 ⟩

초록

This study introduces the design methods for air flow distribution at the level of preliminary design, and reviews the typical combustion process and main functions of sub-components of aircraft gas turbine combustors. There are lots of design approaches and empirical equations introduced for air flow distributions at the combustors. It is shown that a decision on which design approaches work for the combustor development is totally dependent upon the objective of engine design, target performance, and so on. The current results suggested for preliminary air flow distributions need to be validated by combustor geometry checkups and performance evaluations for future works.

키워드

참고문헌

  1. Burrus, D. L., et al., "Energy efficient engine(E3) - Combustor test hardware detailed design report", NASA Report, NASA-CR-168301, 1984.
  2. Tietz, S., et al., "Development and application of a pre-design tool for aero-engine combustors", CEAS Aeronaut Journal, Vol.2, pp.111-123, 2011. https://doi.org/10.1007/s13272-011-0012-x
  3. 김대식 등, "가스터빈 연소기 기본 설계 기법 소개", 제 46회 KOSCO SYMPOSIUM 초록집(2013 년도 춘계학술대회), pp. 25-26, 2013.
  4. Lefebvre, A. H., et al., "Gas Turbine Combustion", 3rd edition, CRC Press 2010, ISBN 978-1-4200- 8604-1.
  5. Mellor, A. M., "Design of Modern Turbine Combustors", Academic Pres 1990, ISBN 0-12-4900 55-0.
  6. Rolls-Royce, "The Jet Engine", Rolls-Royce plc 2005, ISBN 0-902121-2-35.
  7. Mattingly, J. D., et al., "Aircraft engine design", 2nd edition, AIAA 2002, ISBN 1-56347-538-3.
  8. Gouws, J. J., "Combining an one-dimensional empirical and network solver with computational fluid dynamics to investigate possible modifications to a commercial gas turbine combustor", Master thesis, U. of Pretoria, 2007
  9. Singh, R., et al., "Lecture notes of gas turbine combustion", Cranfield University, 2013
  10. Skidmore, F. W., "Smoke emission tests on series II and Series III allison T56 turboprop engines", ARL Aero-Prop-TM-438, 1986
  11. Walsh, P., "Gas turbine performance", 2nd edition, Blackwell publishing 2004, ISBN 0-7918-0211-6.
  12. Oates, G. C., "Aircraft Propulsion Systems Technology and Design", AIAA Education Series, 1989
  13. Gosselin, P., "Prediction of wall heat transfer for a gas turbine combustor", J. of Power and Energy, vol. 213, pp. 169-180, 1999 https://doi.org/10.1243/0957650991537527

피인용 문헌

  1. Preliminary Design Program Development for Gas Turbine Combustor vol.20, pp.3, 2015, https://doi.org/10.15231/jksc.2015.20.3.027
  2. 연료의 미립화 및 증발 특성 데이터를 이용한 가스터빈 연소기 사이징 기법 고찰 vol.19, pp.3, 2013, https://doi.org/10.15435/jilasskr.2014.19.3.101