An exhaust infrared signature reduction arrangement includes an exhaust duct, a first vane support disposed within the exhaust duct and a second vane support disposed within the exhaust duct downstream from the first vane support. The first vane support and the second vane support are movable between a first configuration and a second configuration.
LOW INFRARED SIGNATURE EXHAUST THROUGH ACTIVE FILM COOLING, ACTIVE MIXING AND ACTIVE VANE ROTATION
ABGAS MIT GERINGER INFRAROTSIGNATUR DURCH AKTIVE FILMKÜHLUNG, AKTIVE MISCHUNG UND AKTIVE SCHAUFELDREHUNG
ÉCHAPPEMENT À SIGNATURE INFRAROUGE FAIBLE PAR REFROIDISSEMENT À FILM ACTIF, MÉLANGE ACTIF ET ROTATION D'AUBE ACTIVE
2018-06-06
Patent
Electronic Resource
English
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
LOW INFRARED SIGNATURE EXHAUST THROUGH ACTIVE FILM COOLING ACTIVE MIXING AND ACITVE VANE ROTATION
European Patent Office | 2018
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