Generalised Predictions of Particle-Vane Retention Probability in Gas Turbine Engines
Abstract The ingestion of airborne particulate into aircraft engines is an undesirable consequence of their operations, particularly in and out of arid locations which leads to reduced time between overhaul. Predicting the maintenance burden in environments rich in airborne particulate is made difficult by the large number of parameters which influence the likelihood of retention of the particles on nozzle guide vanes. In this contribution we propose a new, reduced-order model which can predict the probability of particle retention as a function of a reduced set of independent variables relating to both the carrier gas flow and particle. Two-dimensional CFD simulations of particle deposition are performed on the General Electric E3 nozzle guide vane using the existing, energy-based EBFOG particle deposition model. Results from the model are compared with experimental observations of particle deposition and show good agreement with the mass fraction retained by a vane. We introduce a function which allows the probability of retention to be calculated for a range of engine operating states and architectures by defining a new dimensionless parameter, the generalised thermal Stokes number. This parameter normalises the thermal response of a particle for all gas and particle softening temperatures allowing the retention probability function to be applied universally. Finally, we demonstrate a practical use of this model by showing its use in calculating the accumulation factor for a particle size distribution.