发明名称 |
AIRCRAFT WITH A DEVICE FOR DIRECTIONALLY STABILIZING THE AIRCRAFT, COMPUTER PROGRAM PRODUCT AND METHOD FOR DIRECTIONALLY STABILIZING THE AIRCRAFT |
摘要 |
A method for reducing yawing motions of an aircraft in-flight, wherein a spoiler adjustment drive of a spoiler and a regulating flap adjustment drive of a regulating flap of the same respective airfoil are adjusted in a time segment in such a way that the motion of the spoiler being adjusted and the motion of the regulating flap of the same airfoil deflect in mutually opposite directions in the time segment. The spoiler and the regulating flap are adjusted on the airfoil, on which the adjusted deflections counteract the respectively occurring yawing motion. Also provided are a computer program product for carrying out this method and an aircraft with a directional stabilization device for carrying out this method.
|
申请公布号 |
US2012325977(A1) |
申请公布日期 |
2012.12.27 |
申请号 |
US201213464029 |
申请日期 |
2012.05.04 |
申请人 |
GIESSELER HANS-GERD;AIRBUS OPERATIONS GMBH |
发明人 |
GIESSELER HANS-GERD |
分类号 |
B64C13/16;B64C3/58;B64C9/04 |
主分类号 |
B64C13/16 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|