A system and method for generating lift provided by a multi-element aircraft wing are provided. The system includes a main wing element, a slat interconnected to the main wing element, and a flap interconnected to the main wing element. The system also includes at least one port defined in at least one of the slat, main wing element, and flap. In addition, the system includes at least one fluidic device operable to regulate fluid flow into and out of the at least one port to control boundary layer flow over at least one of the slat, main wing element, and flap.
Sistema de incremento de sustentación y método asociado
2020-07-08
Patent
Elektronische Ressource
Spanisch
IPC: | B64C AEROPLANES , Flugzeuge |
Sistema deslizante para vehículo recreativo y método asociado
Europäisches Patentamt | 2024
|PLATAFORMA FLOTANTE CON SISTEMA DE ANCLAJE Y SUSTENTACIÓN ASOCIADOS
Europäisches Patentamt | 2015
|SISTEMA DE MEDICIÓN DE COMPOSICIONES FERROVIARIAS Y MÉTODO ASOCIADO
Europäisches Patentamt | 2020
|SISTEMA DE MEDICION DE COMPOSICIONES FERROVIARIAS Y METODO ASOCIADO
Europäisches Patentamt | 2020
|