|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64C-003/50 B64C-009/24 B64C-013/50 B64C-013/00 B64C-013/16|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 0 인용 특허 : 17|
A system for varying a wing camber of an aircraft wing may include a leading edge device coupled to the wing. The leading edge device may be configured to be actuated in an upward direction and a downward direction relative to a retracted position of the leading edge device.
1. A system for varying a wing camber, comprising: a flight control computer configured to compute an optimum slat setting based on aircraft state data;a control system communicatively coupled to the flight control computer, the control system including a control device moveable to any one of a plurality of control device positions including a designated control device position selected by the control device for selecting any one of a plurality of corresponding standard flap settings;a leading edge device coupled to a wing of the aircraft;a slat actuatio...