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    Display system for an aircraft
    2.
    发明授权
    Display system for an aircraft 有权
    飞机显示系统

    公开(公告)号：US06980128B2

    公开(公告)日：2005-12-27

    申请号：US10715393

    申请日：2003-11-19

    申请人： Eric Godard ,  David Chabe ,  Jacques Espinasse

    发明人： Eric Godard ,  David Chabe ,  Jacques Espinasse

    IPC分类号： B64D43/02 ,  B64D43/00 ,  G01C21/00 ,  G01C23/00 ,  G05D1/06 ,  G08B21/00

    CPC分类号： B64D43/00 ,  G01C23/005

    摘要： A display system for an aircraft includes a central unit configured to determine a speed vector of the aircraft and to determine a longitudinal margin of maneuver of the aircraft. The longitudinal margin of maneuver is expressed as a load factor and is related to one of a pitch-up maneuver and a pitch-down maneuver. The display system also includes a display unit connected to the central unit. The display unit includes a display screen configured to display a first characteristic sign illustrating the speed vector and a second characteristic sign illustrating the longitudinal margin of maneuver.

    摘要翻译： 用于飞行器的显示系统包括中央单元，该中央单元被配置为确定飞行器的速度矢量并确定飞机的纵向纵向余量。 机动的纵向余量表示为负载因子，与俯仰操纵和俯仰操纵之一有关。 显示系统还包括连接到中央单元的显示单元。 显示单元包括被配置为显示示出速度矢量的第一特征符号和示出纵向纵向余量的第二特征符号的显示屏幕。

    Process and device for aiding the piloting of an aircraft
    3.
    发明授权
    Process and device for aiding the piloting of an aircraft 有权
    帮助驾驶飞机的过程和装置

    公开(公告)号：US06937166B2

    公开(公告)日：2005-08-30

    申请号：US10261484

    申请日：2002-10-02

    申请人： Eric Godard ,  David Chabe ,  Jacques Espinasse

    发明人： Eric Godard ,  David Chabe ,  Jacques Espinasse

    IPC分类号： B64D43/02 ,  B64D43/00 ,  G01C21/00 ,  G01C23/00 ,  G05D1/06 ,  G08B23/00

    CPC分类号： B64D43/00 ,  G01C23/005

    摘要： The device (1) for aiding piloting comprises means (2) for determining a speed vector of the aircraft, means of depiction (4) for presenting on a display screen (6) a first characteristic sign illustrating the speed vector of the aircraft, and auxiliary means (7) for determining at least one longitudinal margin of maneuver of the aircraft, which is expressed as a load factor and which relates to one of the two maneuvers of pitch-up and of pitch-down of the aircraft. The means of depiction (4) moreover present, on the display screen (6), at least one second characteristic sign which is associated with said first characteristic sign and which illustrates the longitudinal margin of maneuver.

    摘要翻译： 用于辅助驾驶的装置（1）包括用于确定飞行器的速度矢量的装置（2），用于在显示屏（6）上呈现示出飞行器的速度矢量的第一特征符号的描绘装置（4），以及 用于确定飞行器的至少一个纵向纵向余量的辅助装置（7），其表示为负载因数，并且涉及飞机的俯仰和俯仰的两个机动之一。 描绘装置（4）还在显示屏幕（6）上存在与所述第一特征符号相关联的至少一个第二特征符号，并且示出了纵向纵向余量。

    Method and device for the energy protection of an aircraft
    4.
    发明授权
    Method and device for the energy protection of an aircraft 有权
    飞机能量保护的方法和装置

    公开(公告)号：US08249792B2

    公开(公告)日：2012-08-21

    申请号：US12575286

    申请日：2009-10-07

    申请人： Emmanuel Blanvillain ,  Florian Constans ,  David Chabe

    发明人： Emmanuel Blanvillain ,  Florian Constans ,  David Chabe

    IPC分类号： G06F19/00

    CPC分类号： B64D31/06 ,  G05D1/0072

    摘要： Disclosed is a method and device for protecting an aircraft comprising at least one wing-mounted engine arranged on each of its wings against at least one of a low-energy situation and a high-energy situation during flight in which at least one engine is a failed engine. A control unit is triggered to activate a protection function, as a function of the number and position of failed engines. The control unit controls at least one non-failed engine, and the protection function is activated when activation conditions are met. The activation conditions indicate that the aircraft is either in the low-energy situation such that the total current power of the aircraft is less than a predetermined minimum power or that the aircraft is in the high-energy situation such that the total current power of the aircraft is greater than a predetermined maximum total power.

    摘要翻译： 公开了一种用于保护飞行器的方法和装置，其包括布置在其每个翼上的至少一个机翼安装的发动机，以抵抗飞行中的低能量情况和高能量情况中的至少一个，其中至少一个发动机是 发动机失效 触发控制单元以根据故障发动机的数量和位置来激活保护功能。 控制单元控制至少一个非故障发动机，并且当满足激活条件时激活保护功能。 激活条件表明飞机处于低能量状态，使得飞机的总电流功率小于预定的最小功率，或者飞机处于高能量状态，使得飞行器的总电流功率 飞机大于预定的最大总功率。

    Method for displaying flight information
    6.
    发明授权
    Method for displaying flight information 有权
    显示航班信息的方法

    公开(公告)号：US07015829B2

    公开(公告)日：2006-03-21

    申请号：US10715392

    申请日：2003-11-19

    申请人： Eric Godard ,  David Chabe ,  Jacques Espinasse

    发明人： Eric Godard ,  David Chabe ,  Jacques Espinasse

    IPC分类号： G08B23/00

    CPC分类号： B64D43/00 ,  G01C23/005

    摘要： A method for displaying flight information includes displaying a first characteristic sign illustrating a speed vector of an aircraft. The method also includes determining a first longitudinal margin of maneuver of the aircraft as a load factor, and displaying a second characteristic sign such that a position of the second characteristic sign relative to the first characteristic sign illustrates the first longitudinal margin of maneuver.

    摘要翻译： 用于显示飞行信息的方法包括显示示出飞行器的速度矢量的第一特征符号。 该方法还包括确定作为负载系数的飞机的第一纵向余量，以及显示第二特征符号，使得第二特征符号相对于第一特征符号的位置示出了第一纵向纵向余量。

    Process and device for aiding the driving of a vehicle running over the ground
    8.
    发明授权
    Process and device for aiding the driving of a vehicle running over the ground 有权
    帮助驾驶在地面上行驶的车辆的过程和装置

    公开(公告)号：US07139645B2

    公开(公告)日：2006-11-21

    申请号：US10615397

    申请日：2003-07-09

    申请人： Fabrice Villaume ,  Eric Godard ,  David Chabe

    发明人： Fabrice Villaume ,  Eric Godard ,  David Chabe

    IPC分类号： G06F19/00

    CPC分类号： G05D1/0083

    摘要： A device and process for aiding the driving of an aircraft running over the ground in an acceleration phase with a view to takeoff may include determining a current speed v0 of the aircraft and a value acc corresponding to a deceleration of the aircraft during emergency braking. A distance df to be traveled on the ground by the aircraft while stopping is calculated using the expression df=(v0)2/2 acc, and a stopping position of the aircraft is calculated from the distance df and a current position of the aircraft. Thereafter, the distance df and the stopping position are presented to a driver of the aircraft with the aid of an appropriate device.

    摘要翻译： 用于在加速阶段帮助​​驾驶飞机在地面上起飞的装置和过程可以包括确定飞行器的当前速度v0和对应于紧急制动期间航空器减速度的值。 使用表达式df =（v0）＆lt; 2＆gt; / 2 acc来计算停止时飞行器在地面上行驶的距离df，并且从距离df和df计算出飞行器的停止位置， 飞机的当前位置。 此后，借助适当的装置将距离df和停止位置提供给飞行器的驾驶员。

    Method and device for displaying a velocity vector of an aircraft
    9.
    发明授权
    Method and device for displaying a velocity vector of an aircraft 有权
    用于显示飞机速度矢量的方法和装置

    公开(公告)号：US06574533B2

    公开(公告)日：2003-06-03

    申请号：US10263649

    申请日：2002-10-04

    申请人： Eric Godard ,  David Chabe

    发明人： Eric Godard ,  David Chabe

    IPC分类号： G05D100

    CPC分类号： G01C23/005 ,  B64D43/00

    摘要： The device (1) comprises a first means (3) for measuring the effective value of the velocity vector of the aircraft, a computing unit (4) which determines a display value automatically and repetitively and which comprises a filtering means (6) which filters the value measured by the first means (3) so as to form a first term, a display unit (7) for presenting on a screen (2) a characteristic sign illustrating the velocity vector whose position on the screen (2) is representative of the display value, and a second means (9) for determining the derivative of a velocity vector controlled by an aircraft pilot. The computing unit (4) further comprises a computing means (10) which determines a second term from the derivative of the controlled velocity vector and a summator (12) which sums the first and second terms so as to form the display value.

    摘要翻译： 装置（1）包括用于测量飞行器的速度矢量的有效值的第一装置（3），自动和重复地确定显示值的计算单元（4），其包括滤波装置（6） 由第一装置（3）测量以形成第一项的值;显示单元（7），用于在屏幕（2）上呈现表示屏幕（2）上的位置代表的速度向量的特征符号 显示值，以及用于确定由飞行员飞行员控制的速度矢量的导数的第二装置（9）。 计算单元（4）还包括计算装置（10），该计算装置（10）根据受控速度向量的导数确定第二项，以及求和第一项和第二项之和以形成显示值的求和器（12）。