|국가/구분||United States(US) Patent 등록|
|§371/§102 date||19990914 (19990914)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 13 인용 특허 : 4|
A control process for the control surfaces of an aircraft to prevent lateral deviation of the trajectory on the ground during a landing or interrupted takeoff, in which the spoilers are extended asymmetrically.
[ What is claimed is:] [1.]1. Process for controlling the control surfaces of an aircraft to resist lateral deviation of the trajectory on the ground when landing or during an interrupted take-off, the process comprising:turning a rudder to resist the deviation;extending spoilers to increase the pressure of the aircraft on the ground, wherein the spoilers are extended asymmetrically, and at least one of the spoilers is retracted, on the wing opposite the side towards which the rudder is turned; andactivating the retraction of the spoilers by an order fro...