AIR INLET OF AN AIRCRAFT TURBINE ENGINE, AIRCRAFT EQUIPPED WITH SUCH AN AIR INLET AND PROCESS FOR OPTIMIZING THE OPERATION OF AN AIRCRAFT TURBINE ENGINE THROUGH AN AIR INLET

摘要

The present invention relates to an air inlet of an aircraft turbine engine comprising an air delivery duct delimited by a side wall and extended by a dynamic inlet duct, said dynamic inlet duct extending along a dynamic axis (AX1) to a front passage section, said dynamic inlet duct being provided with a protective grid against ingestion of external bodies. The grid being able to perform a translation along said dynamic axis (AX1) with respect to said front passage section, said air inlet comprises at least one lateral inlet formed in said lateral wall and means for closing off said lateral inlet. movable relative to this lateral inlet, said air inlet comprising a displacement means controlled by said translation of the grid to require a displacement of said sealing means relative to said lateral inlet.