公开(公告)号：US20160200448A1

公开(公告)日：2016-07-14

申请号：US14973574

申请日：2015-12-17

Applicant: AIRBUS OPERATIONS (S.A.S.)

Inventor： Pierre SCACCHI ,  Matthieu MAYOLLE

IPC: B64D43/02 ,  G01C23/00 ,  G05D1/04

CPC classification number: B64D43/02 ,  G01C23/005 ,  G05D1/042 ,  G05D1/0607 ,  G05D1/0653 ,  G05D1/101 ,  G08G5/0021 ,  G08G5/003 ,  G08G5/0047 ,  G08G5/0065 ,  G08G5/025

Abstract: A method and device for aiding piloting of an aircraft, during at least one flight phase including piloting steps. The device includes a unit for real-time acquisition of flight parameters of the aircraft, a calculation unit for calculating in real time with the parameters, for each of the piloting steps, a distance between current position of the aircraft and a position along a flight trajectory followed by the aircraft, at which the aircraft will reach the corresponding piloting step. At least one display unit is provided for displaying, in real time, characteristic signs each illustrating one of the piloting steps, the characteristic signs being integrated into the environment viewed with the aid of the screen and being positioned so as to make it possible to locate a place of the environment along the flight trajectory followed by the aircraft, at which the aircraft will reach the piloting step.

Abstract translation: 一种用于在包括驾驶步骤的至少一个飞行阶段期间帮助驾驶飞机的方法和装置。 该装置包括用于实时获取飞行器的飞行参数的单元，用于每个驾驶步骤实时计算参数的计算单元，飞行器的当前位置与沿着飞行的位置之间的距离 随后是飞机的轨迹，飞机将到达相应的驾驶步骤。 提供至少一个显示单元，用于实时地显示各自示出引导步骤之一的特征符号，特征符号被集成到借助于屏幕观看的环境中并且被定位成使得可以定位 航空器沿着飞行轨迹的环境的一个地方，飞机将到达飞行阶段。

公开(公告)号：US20140209739A1

公开(公告)日：2014-07-31

申请号：US14167095

申请日：2014-01-29

Applicant: AIRBUS OPERATIONS S.A.S.

Inventor： Matthieu MAYOLLE ,  Caroline ACANFORA ,  Louis-Emmanuel ROMANA ,  Julien FONTAN

IPC: B64C25/48

CPC classification number: B64C25/48 ,  B60T8/1703 ,  B60T2201/16 ,  B64C25/50

Abstract: The device includes, but is not limited to a calculating unite for automatically applying, if conditions for turning of the aircraft are met, a symmetrical braking value at a brake assembly, then in the course of the turn automatically distributing this symmetrical braking value in differential braking between braking device of the left main landing gear and braking device of the right main landing gear of the aircraft, as a function of current directional command orders, in such a way as to maintain a constant overall braking level, at least for directional command orders below a predetermined threshold.

Abstract translation: 该装置包括但不限于如果满足飞行器转动条件的自动应用的计算联合，在制动组件处的对称制动值，则在转向过程中自动将该对称制动值分配在差速器 至少对于方向指令，左主起落架的制动装置与飞机的右主起落架的制动装置之间的制动作为当前方向指令命令的函数，以保持恒定的总制动水平 低于预定阈值。

公开(公告)号：US20160185448A1

公开(公告)日：2016-06-30

申请号：US14808453

申请日：2015-07-24

Applicant: Airbus Operations (S.A.S.)

Inventor： Pierre SCACCHI ,  Thierry Bourret ,  Franck LAINE ,  Matthieu MAYOLLE ,  Sabrina BETTON ,  Cécile PUISSACQ ,  Olivier SAPIN

IPC: B64C13/22 ,  B64C13/04 ,  B64C13/18

CPC classification number: B64C13/22 ,  B64C13/04 ,  B64C13/042 ,  B64C13/18 ,  B64D43/00 ,  G01C23/005 ,  G05D1/0061

Abstract: A control system and method for an aircraft configured to operate according to a first mode of operation corresponding to an automatic piloting of the aircraft and a second mode of operation corresponding to a manual piloting of the aircraft, the system including a selection member. The system is configured to operate according to the first mode of operation when the selection member is not actuated continuously and to operate according to the second mode of operation when the selection member is actuated continuously.

Abstract translation: 一种用于飞行器的控制系统和方法，其被配置为根据对应于飞行器的自动驾驶的第一操作模式进行操作，以及对应于飞行器的手动驾驶的第二操作模式，所述系统包括选择构件。 当选择构件被连续致动时，该系统构造成在选择构件不连续致动时根据第一操作模式操作并根据第二操作模式进行操作。