An airplane having at least one turbojet and means for taking at least a portion of the boundary layer of the flow of air over a surface of the airplane and for guiding the air that has been taken to an air inlet of the turbojet, the airplane being characterized in that the means for guiding air include means for diffusing the air that has been taken circumferentially in uniform manner over 360° at the air inlet of the turbojet.
A boundary layer air intake for an aeroplane turbojet
2019-05-15
Patent
Electronic Resource
English
AEROPLANE CONTROL SYSTEM, AEROPLANE AND AEROPLANE CONTROL METHOD
European Patent Office | 2015
|Engineering Index Backfile | 1942
TIBKAT | 26.1998,12 -