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.
Method and apparatus for reducing aircraft wing bending moment
25.07.2018
Patent
Elektronische Ressource
Englisch
METHOD AND APPARATUS FOR REDUCING AIRCRAFT WING BENDING MOMENT
Europäisches Patentamt | 2021
|METHOD AND APPARATUS FOR REDUCING AIRCRAFT WING BENDING MOMENT
Europäisches Patentamt | 2019
|Method and apparatus for reducing aircraft wing bending moment
Europäisches Patentamt | 2021
|CONTROLLER ANS SYSTEM FOR REDUCING AIRCRAFT WING BENDING MOMENT
Europäisches Patentamt | 2024
|