|국가/구분||United States(US) Patent 등록|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 14 인용 특허 : 6|
The movable surfaces affecting the camber of a wing are dynamically adjusted to optimize wing camber for optimum lift/drag ratios under changing conditions during a given flight phase. In a preferred embodiment, an add-on dynamic adjustment control module provides command signals for optimum positioning of trailing edge movable surfaces, i.e., inboard flaps, outboard flaps, ailerons, and flaperons, which are used in place of the predetermined positions of the standard flight control system. The dynamic adjustment control module utilizes inputs of changin...
The invention claimed is: 1. An aircraft flight control system for dynamic adjustment of a wing's movable surfaces for effecting variable camber, comprising: a flight control system for sending command signals to movable surfaces on the wing; an actuator system for receiving said command signals and positions the movable surfaces of the wing corresponding to said command signals; and a dynamic adjustment control module for computing and outputting optimal wing surface positions; the dynamic adjustment control module being programmed to perform a predic...