Gas turbine engine air intake

Details Gas turbine engine air intake Gas turbine engine air intake

F - Mech Eng,Light,Heat,Weapons

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

Patent

CA 1205295

ABSTRACT GAS TURBINE ENGINE COMPRSEESOR AIR INTAKE An air intake for a gas turbine engine compressor comprises an arcuate primary duct 14 which is in communication with the compressor of the gas turbine engine and which is provided with frangible wall portion. The frangible wall portion provides a barrier between the primary duct and a secondary duct and is so positioned and adapted as to be impacted and penetrated by a foreign body such as a bird which is above a predetermined weight and which has been ingested through the inlet of the primary duct. After penetrating the wall portion of the foreign body passes through the secondary duct and is discharged therefrom at a location remote from the primary duct.

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