This invention provides construction variants of a cruise miniflap that is added to the 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, it has a cavity with a height of up to 1 % of the wing chord.
AIRCRAFT WING COMPRISING CRUISE MINI FLAPS
FLUGZEUGFLÜGEL UMFASSEND FLUGMINIKLAPPEN
AILE D'AÉRONEF COMPRENANT DES MINI-VOLETS DE CROISIÈRE
2020-12-02
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Wing flaps in light aircraft design
Engineering Index Backfile | 1945
|Online Contents | 1999
AIRCRAFT WING FLAPS HAVING AERODYNAMIC RESTORATION DOORS
Europäisches Patentamt | 2023
|