|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 0 인용 특허 : 10|
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 out...
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 andat 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. 2. An air ...