Implications of engine deterioration for creep life

Citation
M. Naeem et al., Implications of engine deterioration for creep life, APPL ENERG, 60(4), 1998, pp. 183-223
Citations number
26
Categorie Soggetti
Environmental Engineering & Energy
Journal title
APPLIED ENERGY
ISSN journal
03062619 → ACNP
Volume
60
Issue
4
Year of publication
1998
Pages
183 - 223
Database
ISI
SICI code
0306-2619(199808)60:4<183:IOEDFC>2.0.ZU;2-I
Abstract
World developments have led the armed forces of many countries to become mo re aware of how their increasingly-stringent financial budgets are spent. O ne major expenditure for military authorities is upon aero-engines. Deterio ration of an engine generally results in a lower specific thrust and higher specific fuel-consumption for the same spool speeds and turbine-entry temp eratures. In order to meet the thrust requirement for the same aircraft's p erformance, the engines are ran at higher spool speeds and/or turbine-entry temperatures. This results in greater rates of fuel consumption, and a sho rter life (due to the greater creep damage and low-cycle fatigue incurred). Possessing a better knowledge, of the impacts of engine deterioration on a n aircraft's operational performance as well as its fuel and residual life- expectancy, helps the users to improve engine utilization. (C) 1998 Elsevie r Science Ltd. ALI rights reserved.