Maneuver load alleviation system

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244 75R, 244 90R, B64C 910

Patent

active

047961929

ABSTRACT:
A system for reducing wing root bending moment load during aircraft maneuvers. The system operates to reduce the lift on the outboard section of the wing by moving an outboard flap upward in response to commands calculated from aircraft parameters and a predetermined wing root bending moment load limit.

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patent: 4455004 (1984-06-01), Whitaker, Sr.
patent: 4472780 (1984-09-01), Chenoweth et al.
patent: 4479620 (1984-10-01), Rogers et al.

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