Generalized Predictions of Particle-Vane Retention Probability in Gas Turbine Engines
نویسندگان
چکیده
Abstract The ingestion of airborne particulate into aircraft engines is an undesirable consequence their operation, particularly in and out arid locations that leads to reduced time between overhaul. Predicting the maintenance burden environments rich made difficult by large number parameters influence likelihood retention particles on nozzle guide vanes. In this contribution, we propose a new, reduced-order model can predict probability particle as function set independent variables relating both carrier gas flow particle. Two-dimensional CFD simulations deposition are performed General Electric E3 vane using existing, energy-based fouling turbines (EBFOG) model. Results from compared with experimental observations show good agreement mass fraction retained vane. We introduce allows be calculated for range engine operating states architectures defining new dimensionless parameter, generalized thermal Stokes number. This parameter normalizes response all softening temperatures allowing applied universally. Finally, demonstrate practical use showing its calculating accumulation factor size distribution.
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ژورنال
عنوان ژورنال: Journal of turbomachinery
سال: 2021
ISSN: ['0889-504X', '1528-8900']
DOI: https://doi.org/10.1115/1.4051108