An aircraft airflow modification device, comprising: at least one resiliently deformable base member; and at least one resiliently deformable flap member that extends from the resiliently deformable base member. Deformation of the resiliently deformable base member from a first state to a second state results in corresponding deformation of the resiliently deformable flap member from a first state to a second state.
Aircraft airflow modification device and vortex generator arrangement for an aircraft
2020-08-11
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
AIRCRAFT AIRFLOW MODIFICATION DEVICE AND VORTEX GENERATOR ARRANGEMENT FOR AN AIRCRAFT
European Patent Office | 2020
|AIRCRAFT AIRFLOW MODIFICATION DEVICE AND VORTEX GENERATOR ARRANGEMENT FOR AN AIRCRAFT
European Patent Office | 2018
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