Air inlet filter for gas turbine engine

B - Operations – Transporting – 01 – D

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60/183

B01D 46/26 (2006.01) B01D 46/04 (2006.01) B01D 46/52 (2006.01) F02C 7/052 (2006.01)

Patent

CA 1266382

- 21 - ABSTRACT OF THE DISCLOSURE An annular air filter is rotationally mounted within a plenurn box, which in turn is securely mounted to the inlet end of a gas turbine engine. At least a portion of the annular air filter surrounds the inlet end of the engine. A motor is provided to rotationally drive the air filter relative to both the plenum box and the engine. An air pressure nozzle is disposed adjacent the inner circumfer- ential surface of the air filter, and a vacuum nozzle is disposed adjacent the outer circumferential surface thereof. The air pressure and vacuum nozzles clean the air filter as the air filter is rotated relative thereto.

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