The present invention provides a retractable vortex generator system for an aircraft, the system comprising a skin, a slot arranged on the skin, a plate comprising a contour configured for energizing the boundary layer of an air current, and driving means configured for rotating the plate between a first and a second position, wherein in the first position at least part of the contour of the plate protrudes through the slot, and in the second position the plate is retracted within the slot.
RAZOR VORTEX GENERATOR
KLINGENWIRBELGENERATOR
GÉNÉRATEUR DE VORTEX À LAME
2024-08-07
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Online Contents | 2002