Air inlet combining a filter and a bypass device for use with a turbine engine

摘要

An air inlet (10) for an engine (20) of an aircraft (50), the air inlet (10) having a duct (2) feeding outside air to said engine (20) together with a filter system combining at least one filter (3) and at least one bypass device (4). Said filter (3) and said bypass device (4) are fastened on a common support (1) situated at one end of said duct (2) and on a flank of a fuselage (51) of said aircraft (50). Said bypass device (4) comprises a cover (5) and an actuator (6) controlling opening of said cover (5). Thus, when said filter (3) no longer allows outside air to pass therethrough, said cover (5) is opened, and outside air passes via the bypass device (4) in order to feed said engine (20) with outside air.

主权项

1. An air inlet for an engine of an aircraft, the inlet comprising:
a duct for feeding outside air to said engine; at least one filter and at least one bypass device allowing said outside air to pass therethrough when said filter is obstructed; the air inlet being characterized in that said duct, said filter and said bypass device are fastened to a common support, said support being situated at one end of said duct and being fastenable to the aircraft so that the filter and the bypass device can be assembled on the support away from the aircraft.