The present application relates to a vortex generator (20). The present application also relates to an aircraft assembly with a hot air exhaust outlet (15). The aircraft assembly has an assembly surface over which a hot-air exhaust flow from the hot-air exhaust outlet (15) is exhausted. The aircraft assembly also has a vortex generator (20) with a flow surface (27, 28). The flow surface (27, 28) lies in an air flow over the vortex generator (20). The flow surface (27, 28) is arranged to interrupt the hot-air exhaust flow and generates a flow vortex to cool the air flow over the assembly surface.
AIRCRAFT ASSEMBLY WITH A HOT-AIR EXHAUST OUTLET
FLUGZEUGANORDNUNG MIT EINEM HEISSLUFT-ABGASAUSLASS
ENSEMBLE D'AÉRONEF COMPORTANT UNE SORTIE D'ÉCHAPPEMENT D'AIR CHAUD
07.09.2022
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
ACTUATED OUTLET DOOR FOR AIRCRAFT HIGH-TEMPERATURE EXHAUST
Europäisches Patentamt | 2022
|ACTUATED OUTLET DOOR FOR AIRCRAFT HIGH-TEMPERATURE EXHAUST
Europäisches Patentamt | 2016
|