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1. 发明授权

US4323884A Digital-analog interface for insertion between a digital control signal transmitter and a controlled moving element 失效
标题翻译：用于在数字控制信号发射器和受控移动元件之间插入的数字 - 模拟接口
公开(公告)号：US4323884A
公开(公告)日：1982-04-06
申请号：US966722
申请日：1978-12-05
申请人： Michel Durandeau , Norbert Voisin , Jean P. Verdier
发明人： Michel Durandeau , Norbert Voisin , Jean P. Verdier
IPC分类号： G05D3/12 , H03M1/00 , H03K13/02
CPC分类号： G05D3/124 , H03M1/485 , H03M1/785
摘要： This invention relates to a digital-analog interface for insertion between the control circuit of a moving element and a transmitter of digital control signals.This interface comprises an inductive detector of the actual position of the moving element. The inductive detector has a single primary winding directly connected to an a.c. source and two secondary windings. The detector secondary windings are connected in parallel to one input of a summing circuit, through a first resistance of fixed value and through a second resistance of adjustable value, respectively. Means responsive to the transmitter digital control signals are provided to adjust the value of the second resistance. The output of the summing circuit is connected to the control circuit of the moving element.
摘要翻译：本发明涉及用于插入移动元件的控制电路和数字控制信号的发射器之间的数字 - 模拟接口。该接口包括移动元件的实际位置的感应检测器。感应检测器具有直接连接到一个直流的单个初级绕组。源极和二次绕组。检测器次级绕组通过固定值的第一电阻和可调整值的第二电阻并联连接到求和电路的一个输入端。提供响应于发射机数字控制信号的装置以调节第二电阻的值。求和电路的输出连接到移动元件的控制电路。

2. 发明授权

US4079906A Servo-control device for controlling a control surface of an aircraft 失效
标题翻译：用于控制飞行器的控制表面的伺服控制装置
公开(公告)号：US4079906A
公开(公告)日：1978-03-21
申请号：US779513
申请日：1977-03-21
申请人： Michel Durandeau , Jean-Pierre Verdier , Norbert Voisin
发明人： Michel Durandeau , Jean-Pierre Verdier , Norbert Voisin
IPC分类号： B64C13/24 , B64C13/38 , B64C13/42 , G05D1/00
CPC分类号： B64C13/38
摘要： In a servocontrol device for controlling a control surface of an aircraft, which device is associated with a mechanical control member such as control column, wheel, pedals, and which comprises two identical double-acting hydraulic rams, integral with each other and each controlled by means of a slide valve, the slide valves each being controlled by a servovalve, whilst each servovalve is controlled by an electrical chain associated therewith, emitting an electrical control signal taking into account the displacements of said control member, the chains are connected to each other by crossed connections and they comprise apparatus for delivering equal signals to said servovalves.The invention is directed to the control of the control surfaces of an aircraft.
摘要翻译：在用于控制飞行器的控制表面的伺服控制装置中，哪个装置与机械控制构件（例如控制柱，车轮，踏板）相关联，并且包括两个相同的双作用液压柱塞，它们彼此成一体，并且各自由滑阀的装置，每个由伺服阀控制的滑阀，而每个伺服阀由与其相关联的电链控制，发射电控制信号，考虑到所述控制构件的位移，链条彼此连接通过交叉连接，并且它们包括用于向所述伺服阀输送相等信号的装置。

3. 发明授权

US5913492A System for controlling an aircraft control surface tab 失效
标题翻译：用于控制飞机控制表面标签的系统
公开(公告)号：US5913492A
公开(公告)日：1999-06-22
申请号：US855190
申请日：1997-05-13
申请人： Michel Durandeau , Etienne Foch
发明人： Michel Durandeau , Etienne Foch
IPC分类号： B64C9/10 , B64C9/04
CPC分类号： B64C9/10
摘要： A system for controlling the tab (6) of an aircraft control surface (3) having a pair of position sensors (12 and 15) that supply information regarding the turning of the control surface (3) and the position of a jack (13), respectively, on the basis of signals generated by the sensors (12 and 15) as well as possibly on the basis of at least one parameter (p) originating from the aircraft, such as airspeed, positions of lift-augmenting devices, forces exerted by the pilot on a control, etc., and which formulates a command for the jack (13).
摘要翻译：一种用于控制飞行器控制表面（3）的突片（6）的系统，具有一对位置传感器（12和15），所述位置传感器提供关于控制表面（3）的转动和插孔（13）的位置的信息，分别基于由传感器（12和15）产生的信号，以及可能基于来自飞行器的至少一个参数（p），例如空速，升力增强装置的位置，施加的力由飞行员进行控制等，并且制定用于千斤顶（13）的命令。

4. 发明授权

US4744532A Aircraft flight control system 失效
标题翻译：飞机飞行控制系统
公开(公告)号：US4744532A
公开(公告)日：1988-05-17
申请号：US93100
申请日：1987-09-01
申请人： Bernard Ziegler , Michel Durandeau , Thierry Collard
发明人： Bernard Ziegler , Michel Durandeau , Thierry Collard
IPC分类号： B64C13/24 , B64C13/50 , G05D1/00 , B64C9/00
CPC分类号： G05D1/0077 , B64C13/503 , Y02T50/44
摘要： Flight control system for aircraft of the type provided with ailerons, elevators, upper surface spoilers, and upper surface air-brakes, a rudder and horizontal stabilizers with variable angle of incidence, said system comprising an electric control, in some cases without any mechanical emergency control for said upper surface spoilers and air-brakes.According to the invention:the ailerons and elevators are electrically controlled without any mechanical aid,the rudder is mechanically controlled, andthe horizontal stabilizers with variable angle of incidence are electrically controlled with mechanical aid.the electrical flight controls are optimized.
摘要翻译：具有副翼，电梯，上表面扰流板和上表面空气制动器的类型飞机的飞行控制系统，具有可变入射角的舵和水平稳定器，所述系统包括电气控制，在某些情况下没有任何机械紧急控制所述上表面扰流板和空气制动器。根据本发明：副翼和电梯在没有任何机械辅助的情况下被电控制，方向舵被机械地控制，并且具有可变入射角的水平稳定器通过机械辅助被电控制。电气飞行控制优化。

5. 发明授权

US06241182B1 Hybrid control system for an aircraft aerodynamic surface 有权
标题翻译：用于飞机空气动力学表面的混合控制系统
公开(公告)号：US06241182B1
公开(公告)日：2001-06-05
申请号：US09300915
申请日：1999-04-28
申请人： Michel Durandeau , Etienne Foch
发明人： Michel Durandeau , Etienne Foch
IPC分类号： B64C1342
CPC分类号： B64C13/503 , B64C13/42
摘要： System for controlling an aerodynamic surface (1) (flap, aileron, control surface, etc.) of an aircraft. According to the invention, this system comprises: an electric machine (8) which can operate either as a motor or as a generator, the output of which is connected mechanically to said aerodynamic surface (1); and a logic device (17) receiving information about the operating status of the electrical power supply (11) of the machine (8) and of the hydraulic servocontrol (2, 5) and controlling the actuation of said surface (1) either by said machine (8) or by said servocontrol (2, 5).
摘要翻译：用于控制飞机的空气动力学表面（1）（翼片，副翼，控制表面等）的系统。根据本发明，该系统包括：可以作为电动机或发电机操作的电机（8），其输出机械地连接到所述空气动力学表面（1）; 以及逻辑设备（17），接收关于机器（8）的电源（11）和液压伺服控制（2,5）的操作状态的信息，并且通过所述机器来控制所述表面（1）的致动（8）或所述伺服控制（2,5）。

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