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
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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.
Abstract
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.
참고문헌 (13)
- Energy efficient engine(E3), "Burrus, D. L.", NASA, ~, pp.NASA-CR-168301 (1984)
- Tietz, S., "Development and application of a pre-design tool for aero-engine combustors", CEAS Aeronaut Journal, 2, pp.111~123 (2011)
- 김대식 등, "가스터빈 연소기 기본 설계 기법 소개", 제 46회 KOSCO SYMPOSIUM 초록집(2013년도 춘계학술대회), pp.25~26 (2013)
- Lefebvre, A. H., "Gas Turbine Combustion" (2010), CRC Press
- Mellor, A. M., "Design of Modern Turbine Combustors" (1990), Academic Pres
- Rolls-Royce, "The Jet Engine" (2005), Rolls-Royce plc
- Mattingly, J. D., "Aircraft engine design" (2002), AIAA
- 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", 석사, pp.2007
- Singh, R., "Lecture notes of gas turbine combustion", Cranfield University, ~ (2013)
- Skidmore, F. W., "Smoke emission tests on series II and Series III allison T56 turboprop engines", ARL Aero-Prop-TM-438, ~ (1986)
- Walsh, P., "Gas turbine performance" (2004), Blackwell publishing
- Oates, G. C., "Aircraft Propulsion Systems Technology and Design" (1989), AIAA Education Series
- Gosselin, P., "Prediction of wall heat transfer for a gas turbine combustor", J. of Power and Energy, 213, pp.169~180 (1999)