|국가/구분||United States(US) Patent 등록|
|국제특허분류(IPC7판)||B64C-003/38 B64C-013/16 B64C-009/16 B64C-013/04|
|발명자 / 주소|
|출원인 / 주소|
|인용정보||피인용 횟수 : 0 인용 특허 : 22|
A system for optimizing performance of an aircraft may include a flight control computer for computing an optimum flap setting based on aircraft data. The system may further include a flap control system having a flap control device. The system may additionally include a flap actuation system coupled to the flap control system for positioning the trailing edge device at the optimum flap setting.
1. A system for optimizing performance of an aircraft, comprising: a flight control computer configured to compute an optimum flap setting based on aircraft data;a flap control system having a flap control device for selecting one of multiple flap lever positions comprising non-designated flap lever positions and at least one designated flap lever position, the non-designated flap lever positions and the designated flap lever position each corresponding to a standard flap setting, the flap control device having a variable-trailing-edge-position switch be...