Title of article :
Implications of engineʹs deterioration upon an aero-engine HP turbine bladeʹs thermal fatigue life
Author/Authors :
M. Naeem، نويسنده , , R. Singh، نويسنده , , D. Probert، نويسنده ,
Issue Information :
روزنامه با شماره پیاپی سال 2000
Pages :
14
From page :
147
To page :
160
Abstract :
Possessing a better knowledge of the impacts of engine deterioration upon an aircraftʹs performance as well as its fuel and component life usage, helps the users make wiser management decisions and hence achieve improved engine utilization. For a military aircraft, using a computer performance simulation, the consequences of engine deterioration on a high pressure turbine bladeʹs thermal fatigue life are predicted.
Keywords :
Thermal fatigue , Turbineיs entry temperature , Engine deterioration , Equivalent full thermal cycle
Journal title :
INTERNATIONAL JOURNAL OF FATIGUE
Serial Year :
2000
Journal title :
INTERNATIONAL JOURNAL OF FATIGUE
Record number :
1160476
Link To Document :
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