A method and apparatus for reducing bending moment on a wing of an aircraft can include at least one sensor provided on the aircraft configured to monitor a shape or position of the wing. The sensor can provide a change in the position or shape of the wing to a controller. The controller can operate one or more spoilers in response to the change in shape or position of the wings to reduce loading on the wings to reduce the bending moment.
METHOD AND APPARATUS FOR REDUCING AIRCRAFT WING BENDING MOMENT
12.12.2019
Patent
Elektronische Ressource
Englisch
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