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
15.05.2019
Patent
Elektronische Ressource
Englisch
A boundary layer air intake for an aeroplane turbojet
Europäisches Patentamt | 2018
|AEROPLANE CONTROL SYSTEM, AEROPLANE AND AEROPLANE CONTROL METHOD
Europäisches Patentamt | 2015
|Engineering Index Backfile | 1942
Aeroplane crushing device, and aeroplane demolition method
Europäisches Patentamt | 2016
|