Aerodynamic structures having lower surface spoilers are described herein. One disclosed example apparatus includes a first spoiler of an aerodynamic structure of an aircraft, where the first spoiler is to deflect away from a first side of the aerodynamic structure and a second spoiler on a second side of the aerodynamic structure opposite of the first side, where the second spoiler is to deflect away from the second side to reduce a load on at least one of the first spoiler or a flap of the aerodynamic structure.
AERODYNAMIC STRUCTURES HAVING LOWER SURFACE SPOILERS
AERODYNAMISCHE STRUKTUREN MIT UNTERSEITENSPOILERN
STRUCTURES AÉRODYNAMIQUES AYANT DES SPOILERS DE SURFACE INFÉRIEURE
03.07.2019
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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