This disclosure provides construction variants of a cruise miniflap of an aircraft wing that is added to trailing edge flap of an aircraft wing and can be used for improving the aerodynamic properties of an aircraft. In the rear edge of the cruise miniflap there is a cavity with a height of up to 1% of the wing chord.
Cruise miniflaps for aircraft wing
2019-06-20
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
LAMINAR FLOW WING OPTIMIZED FOR TRANSONIC AND SUPERSONIC CRUISE AIRCRAFT
Europäisches Patentamt | 2021
|