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    Method and device for ensuring the safety of a low-altitude flight of an aircraft
    2.
    发明申请
    Method and device for ensuring the safety of a low-altitude flight of an aircraft 有权
    确保飞机低空飞行安全的方法和装置

    公开(公告)号：US20050261811A1

    公开(公告)日：2005-11-24

    申请号：US11128299

    申请日：2005-05-13

    申请人： Franck Artini ,  Jean-Pierre Demortier ,  Christophe Bouchet ,  Jacques Espinasse ,  Edward Strongman

    发明人： Franck Artini ,  Jean-Pierre Demortier ,  Christophe Bouchet ,  Jacques Espinasse ,  Edward Strongman

    IPC分类号： G01C5/00 ,  G05D1/06 ,  G06F17/00

    CPC分类号： G05D1/0646 ,  G01C5/005

    摘要： Method and device for ensuring the safety of a low-altitude flight of an aircraft. A device (1) for ensuring the safety of a low-altitude flight comprises information sources (5) able to determine current flight conditions, a monitoring unit (6) for realizing, with the aid of said current flight conditions, a function for global and autonomous monitoring of said low-altitude flight of the aircraft, making it possible to preserve the integrity of said aircraft during said flight, and means (13) for presenting the results of the monitoring function realized by said monitoring unit (6) to an operator.

    摘要翻译： 确保飞机低空飞行安全的方法和装置。 一种用于确保低空飞行的安全性的装置（1）包括能够确定当前飞行情况的信息源（5），用于在所述当前飞行条件的帮助下实现全局的功能的监视单元（6） 以及对所述飞行器的所述低空飞行进行自主监视，使得能够在所述飞行期间保持所述飞行器的完整性;以及用于将由所述监视单元（6）实现的监视功能的结果呈现给 操作员。

    Method and device for ensuring the safety of a low-altitude flight of an aircraft
    3.
    发明授权
    Method and device for ensuring the safety of a low-altitude flight of an aircraft 有权
    确保飞机低空飞行安全的方法和装置

    公开(公告)号：US07428451B2

    公开(公告)日：2008-09-23

    申请号：US11121055

    申请日：2005-05-04

    申请人： Franck Artini ,  Jacques Espinasse

    发明人： Franck Artini ,  Jacques Espinasse

    IPC分类号： G01C5/00

    CPC分类号： G05D1/0646 ,  G05D1/0202

    摘要： A method and device for ensuring the safety of a low-altitude flight of an aircraft is disclosed, wherein low-altitude flight is flight along a flight trajectory at low altitude, for example 500 feet, that allows an aircraft to follow as closely as possible the terrain being over-flown. To avoid collision with the terrain, a safety corridor, devoid of any obstacle, is determined which is delimited on either side of the lateral trajectory, and whose width depends on a global uncertainty, and the aircraft is guided along the flight trajectory, avoiding any exit of the aircraft from the safety corridor.

    摘要翻译： 公开了一种用于确保飞机的低空飞行的安全性的方法和装置，其中低空飞行是沿着低空的飞行轨迹飞行，例如500英尺，这允许飞机尽可能接近 地形正在飞越。 为了避免与地形的碰撞，确定没有任何障碍物的安全走廊，其在侧向轨迹的任一侧被划定，并且其宽度取决于全球不确定性，并且飞机沿着飞行轨迹被引导，避免任何 飞机从安全走廊出口。

    Method and device for ensuring the safety of a low-altitude flight of an aircraft
    4.
    发明申请
    Method and device for ensuring the safety of a low-altitude flight of an aircraft 有权
    确保飞机低空飞行安全的方法和装置

    公开(公告)号：US20050273223A1

    公开(公告)日：2005-12-08

    申请号：US11121055

    申请日：2005-05-04

    申请人： Franck Artini ,  Jacques Espinasse

    发明人： Franck Artini ,  Jacques Espinasse

    IPC分类号： G05D1/00 ,  G05D1/02 ,  G05D1/04 ,  G05D1/06 ,  B64C1/00

    CPC分类号： G05D1/0646 ,  G05D1/0202

    摘要： A method and device for ensuring the safety of a low-altitude flight of an aircraft is disclosed, wherein low-altitude flight is flight along a flight trajectory at low altitude, for example 500 feet, that allows an aircraft to follow as closely as possible the terrain being over-flown. To avoid collision with the terrain, a safety corridor, devoid of any obstacle, is determined which is delimited on either side of the lateral trajectory, and whose width depends on a global uncertainty, and the aircraft is guided along the flight trajectory, avoiding any exit of the aircraft from the safety corridor.

    摘要翻译： 公开了一种用于确保飞机的低空飞行的安全性的方法和装置，其中低空飞行是沿着低空的飞行轨迹飞行，例如500英尺，这允许飞机尽可能接近 地形正在飞越。 为了避免与地形的碰撞，确定没有任何障碍物的安全走廊，其在侧向轨迹的任一侧被划定，并且其宽度取决于全球不确定性，并且飞机沿着飞行轨迹被引导，避免任何 飞机从安全走廊出口。

    Method for displaying flight information
    5.
    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。

    Display system for an aircraft
    6.
    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
    7.
    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。