An aircraft airflow modification device 301, comprising: at least one resiliently deformable base member 305; and at least one resiliently deformable flap member 303 that extends from the resiliently deformable base member 305, wherein deformation of the resiliently deformable base member 305 from a first state to a second state results in corresponding deformation of the resiliently deformable flap member 303 from a first state to a second state.
AIRCRAFT AIRFLOW MODIFICATION DEVICE AND VORTEX GENERATOR ARRANGEMENT FOR AN AIRCRAFT
FLUGZEUGLUFTSTROMMODIFIZIERUNGSVORRICHTUNG UND WIRBELGENERATORANORDNUNG FÜR EIN FLUGZEUG
DISPOSITIF DE MODIFICATION D'ÉCOULEMENT D'AIR D'UN AÉRONEF ET DISPOSITIF DE GÉNÉRATION DE TOURBILLONS POUR UN AÉRONEF
2020-01-01
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
AIRCRAFT AIRFLOW MODIFICATION DEVICE AND VORTEX GENERATOR ARRANGEMENT FOR AN AIRCRAFT
European Patent Office | 2018
|Aircraft airflow modification device and vortex generator arrangement for an aircraft
European Patent Office | 2020
|