|국가/구분||United States(US) Patent 등록|
|§371/§102 date||20070604 (20070604)|
|발명자 / 주소|
|출원인 / 주소|
|대리인 / 주소||
|인용정보||피인용 횟수 : 2 인용 특허 : 4|
A roll steering method subdivides the direction of an aircraft control surface into two elements and, during a roll control operation using ailerons, steers an upper element of the control surface in the roll direction and a lower element in the opposite direction.
The invention claimed is: 1. A method for improving the roll steering of an aircraft of large dimensions comprising:a fuselage,two wings symmetric with respect to said fuselage, provided with controllable aerodynamic surfaces configured to produce a roll movement for the aircraft, anda vertical fin projecting upwards with respect to the rear part of said fuselage and provided with a rudder extending along the rear edge of said fin and configured to turn, with respect to said vertical fin, about an axis of rotation,said method comprising:dividing said rud...