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1. 发明授权

US06928340B2 Process and system for moving a control surface of an aircraft 有权
标题翻译：用于移动飞机控制面的过程和系统
公开(公告)号：US06928340B2
公开(公告)日：2005-08-09
申请号：US10654621
申请日：2003-09-04
申请人： Marc Van De Kreeke , Guillaume Cassein
发明人： Marc Van De Kreeke , Guillaume Cassein
IPC分类号： B64C13/50 , G05D1/00
CPC分类号： B64C13/50 , Y02T50/44
摘要： An electric control system (1) comprises a control unit (4) which comprises a member (5) able to be actuated by a pilot and a means of load-wise protection (7), and which delivers a first deflection order representative of the action exerted by the pilot on the member (5), and of the contribution made by the means of load-wise protection (7), an actuator (11) which moves said control surface (2) about an axis (Z—Z), as a function of a deflection order, and a correction device (12) which comprises a means (13) for determining a second deflection order making it possible to limit the load, to which a stabilizer element of the aircraft is subjected, to a maximum load, and a means (14) for choosing one of the first and second deflection orders, which is transmitted to said actuator (11) so as to move said control surface (2).
摘要翻译：电控制系统（1）包括控制单元（4），该控制单元包括能够由导向装置致动的构件（5）和负载保护装置（7），并且传递第一偏转顺序，由飞行员对构件（5）施加的作用以及通过负载保护装置（7）作出的贡献，使所述控制表面（2）绕轴线（ZZ）移动的致动器（11）作为偏转顺序的功能和校正装置（12），其包括用于确定第二偏转顺序的装置（13），使得可以将飞机的稳定器元件所经受的载荷限制在最大载荷，以及用于选择第一和第二偏转顺序之一的装置（14），其被传送到所述致动器（11）以便移动所述控制表面（2）。

2. 发明授权

US06863242B2 Method and system for controlling an aircraft control surface 有权
标题翻译：用于控制飞机控制面的方法和系统
公开(公告)号：US06863242B2
公开(公告)日：2005-03-08
申请号：US10631009
申请日：2003-07-31
申请人： Marc Van De Kreeke , Guillaume Cassein
发明人： Marc Van De Kreeke , Guillaume Cassein
IPC分类号： B64C9/12 , B64C13/50 , B64C9/06
CPC分类号： B64C9/12 , B64C13/503
摘要： A system for controlling an aircraft control surface may include a control surface having at least two control surface elements mounted to rotate about an axis on a stabilizer element of the aircraft. An actuator with at least two actuating devices moves the control surface elements according to individual turn commands. Also, a first device determines a particular phase of flight of the aircraft. When the particular phase of flight is determined to exist by the first device, a second device generates differentiated individual turn commands for the actuating devices, according to an overall turn command received from a control unit, to provide prioritized control of the control surface element that generates the lowest force on the stabilizer element.
摘要翻译：用于控制飞机控制表面的系统可以包括具有至少两个控制表面元件的控制表面，所述至少两个控制表面元件被安装成围绕飞行器的稳定器元件上的轴线旋转。具有至少两个致动装置的致动器根据各个转动指令移动控制表面元件。此外，第一装置确定飞机的特定飞行阶段。当飞行的特定阶段被第一装置确定为存在时，第二装置根据从控制单元接收到的整体转向命令，为致动装置产生不同的单独转弯命令，以提供控制表面元件的优先控制，在稳定器元件上产生最小的力。

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