A method and apparatus for reducing bending moment on a wing (14) of an aircraft (10) can include at least one sensor (104) provided on the aircraft (10) configured to monitor a shape or position of the wing (14). The sensor (104) can provide a change in the position or shape of the wing (14) to a controller (102). The controller (102) can operate one or more spoilers (92) in response to the change in shape or position of the wings (14) to reduce loading on the wings (14) to reduce the bending moment.
CONTROLLER ANS SYSTEM FOR REDUCING AIRCRAFT WING BENDING MOMENT
STEUERGERÄT UND SYSTEM ZUR REDUZIERUNG DES FLUGZEUGFLÜGELBIEGEMOMENTS
CONTRÔLEUR ET SYSTÈME POUR RÉDUIRE LE MOMENT DE FLEXION D'UNE AILE D'AVION
24.07.2024
Patent
Elektronische Ressource
Englisch
IPC: | G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT |
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