An engine inlet (10) for efficient operation in both subsonic and supersonic flight wherein the inlet has a caret configuration, is rotatable about an off-body axis (30) for compression ramp angle and capture area variation and a diffuser (14) is engaged to the inlet in a scrubbing relationship to maintain a seal upon rotation of the inlet.
SUPERSONIC CARET INLET SYSTEM
ÜBERSCHALL-EINLASSSYSTEM MIT CARET
SYSTÈME D'ENTRÉE DE CARET SUPERSONIQUE
01.04.2020
Patent
Elektronische Ressource
Englisch
Europäisches Patentamt | 2022
Europäisches Patentamt | 2017
|