There is disclosed an inertial particle separator communicating with an engine inlet. The inertial particle separator has: a main duct body; a bypass duct; and a splitter defined by an intersection of the main duct and the bypass duct. The main duct and the bypass duct having particular geometric characteristics. A method of separating particles via inertia in an aircraft engine inlet is also provided.
GAS TURBINE ENGINE WITH INERTIAL PARTICLE SEPARATOR
2019-10-31
Patent
Electronic Resource
English
ADAPTABLE INERTIAL PARTICLE SEPARATOR FOR A GAS TURBINE ENGINE INTAKE
European Patent Office | 2020
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