Diverter assemblies 12 for aircraft air inlets 10 include a diverter structure at least substantially surrounding the air inlet, and a fairing 20 mounted to an upper edge of the diverter structure forwardly of the air inlet.
Aircraft air inlet diverter assemblies with improved aerodynamic characteristics
Flugzeuglufteinlassumlenkanordnungen mit verbesserten aerodynamischen Merkmalen
Ensembles de déviation d'admission d'air d'aéronef présentant de meilleures caractéristiques aérodynamiques
2019-05-08
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
Submerged air inlet of aircraft based on diverter air introduction
European Patent Office | 2015
|ICAS2014_0308: AERODYNAMIC INLET DESIGN FOR CIVIL AIRCRAFT NACELLE
British Library Conference Proceedings | 2014
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