Gas turbine engine and its associated air intake system

Details Gas turbine engine and its associated air intake system Gas turbine engine and its associated air intake system

F - Mech Eng,Light,Heat,Weapons

02

C

60/89

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

Patent

CA 1164666

ABSTRACT A gas turbine engine and its associated air intake system in which the air intake system comprises a generally horizontally extending duct through which an airflow is induced by an ejector pump powered by the engine. A portion of the air passing through the duct is directed through a second duct to the air inlet of the engine. The second duct is connected to the first duct in such a manner that the air directed to the engine air inlet is derived from a vertically upper region of the first duct. The arrangement is intended to reduce the amount of airborne particulate material ingested by the gas turbine engine.

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