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
31.10.2019
Patent
Elektronische Ressource
Englisch
ADAPTABLE INERTIAL PARTICLE SEPARATOR FOR A GAS TURBINE ENGINE INTAKE
Europäisches Patentamt | 2020
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