Aircraft engine air intake including a foreign object separator

F - Mech Eng,Light,Heat,Weapons – 02 – C

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60/183

F02C 7/04 (2006.01) F02C 7/05 (2006.01)

Patent

CA 1229494

AIRCRAFT ENGINE AIR INTAKE INCLUDING A FOREIGN OBJECT SEPARATOR ABSTRACT OF THE DISCLOSURE The present invention comprises a method and apparatus for separating foreign objects from airflow channeled to an aircraft engine. According to an exemplary embodiment, an air intake including a foreign object separator is provided. The air intake includes an inlet duct having a pressure side, which inlet duct is effective for channeling airflow to the engine. A separator aperture is disposed in the pressure side of the inlet duct and is in flow communication with the separator aperture. The separator receptacle includes a turning wall which is substantially arcuate in a transverse plane, and is substantially closed for preventing the flow of airflow therethrough while being effective for receiving and capturing foreign objects which enter the inlet duct and pass through the separator aperture.

466396

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