Method and device for lightening loads on the wing system of...

Data processing: vehicles – navigation – and relative location – Vehicle control – guidance – operation – or indication – Aeronautical vehicle

Reexamination Certificate

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Details

C701S124000, C244S07600R, C340S945000

Reexamination Certificate

active

08010243

ABSTRACT:
A device used in an aircraft with an electrical flight control system to reduce load applied to the wing during a lateral roll maneuver, by comparing a roll control with a threshold, and filtering a control. As a result of this action on the roll control, resulting load increases on the wing can be anticipated and reduced. Loads can thus remain below a maximum design value for the wing if the applied roll control is too high for planned use of the aircraft, therefore limiting overdesign of the wing.

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patent: 5850615 (1998-12-01), Osder
patent: 2005/0192718 (2005-09-01), Delaplace et al.
patent: 2 864 032 (2005-06-01), None

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