|국가/구분||United States(US) Patent 등록|
|미국특허분류(USC)||364/463 ; 244/75R ; 244/90R|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 53 인용 특허 : 6|
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.
A maneuver load alleviation system for shifting the wing airload inboard towards the wing root of an aircraft during a maneuver, the system comprising: means receiving input data for computing the wing root bending moment load of each wing of the aircraft during the maneuver on the basis of a plurality of parameters, including the roll rate or acceleration of the aircraft; means coupled to the means for computing for comparing the computed wing root bending moment load of each wing with a threshold level of the wing root bending moment; and means coupled...