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METHOD AND DEVICE FOR LIGHTENING LOADS ON THE WING SYSTEM OF AN AIRCRAFT IN ROLL MOTION
METHOD AND DEVICE FOR LIGHTENING LOADS ON THE WING SYSTEM OF AN AIRCRAFT IN ROLL MOTION
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机译:滚动运动中机翼系统的轻载方法和装置
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摘要
The invention concerns an aircraft with electric flight control system, wherein a device enables the load applied on the wing system to be lightened during a lateral roll maneuver, by comparing the roll control (X) with a threshold (X%) and by filtering said control. Through such an action on the roll control, it is possible to anticipate the load increases occurring on the wing system, and to reduce same. The loads can thus be maintained below a maximum value of the wing system dimensioning, in case of too great roll control relative to the use provided for the plane, and therefore to limit oversizing of the wing system.
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