公开(公告)号：US09766073B2

公开(公告)日：2017-09-19

申请号：US14324033

申请日：2014-07-03

Applicant: THALES

Inventor： Philippe Gaultier

IPC: G01C21/10 ,  B64D45/00 ,  G01C23/00

CPC classification number: G01C21/10 ,  B64D45/00 ,  G01C23/005 ,  G09G2380/12

Abstract: The general field of the invention is that of methods for representing a rate of turn indicator for an aircraft implemented by an on-board avionics system. The method includes a step of graphically representing on a visualization device a symbol called “aeroplane model”, said graphic representation being a function of the specific speed of the aircraft and of its angle of inclination. In a favored embodiment, said aeroplane model includes two straight arms interlinked by a common point and inclined to the horizontal symmetrically in such a way as to form an inverted V. The angle of inclination of the two arms of the V is proportional to the specific speed of the aircraft, the coefficient of proportionality being determined in such a way that when the specific speed and the angle of inclination correspond to values compatible with the standard rate, said arm is parallel to the horizon line, thus indicating that the aircraft is carrying out its turn at the standard rate.

公开(公告)号：US20160245654A1

公开(公告)日：2016-08-25

申请号：US14324033

申请日：2014-07-03

Applicant: THALES

Inventor： Philippe Gaultier

IPC: G01C21/10 ,  B64D45/00

CPC classification number: G01C21/10 ,  B64D45/00 ,  G01C23/005 ,  G09G2380/12

Abstract: The general field of the invention is that of methods for representing a rate of turn indicator for an aircraft implemented by an on-board avionics system. The method includes a step of graphically representing on a visualization device a symbol called “aeroplane model”, said graphic representation being a function of the specific speed of the aircraft and of its angle of inclination. In a favoured embodiment, said aeroplane model includes two straight arms interlinked by a common point and inclined to the horizontal symmetrically in such a way as to form an inverted V. The angle of inclination of the two arms of the V is proportional to the specific speed of the aircraft, the coefficient of proportionality being determined in such a way that when the specific speed and the angle of inclination correspond to values compatible with the standard rate, said arm is parallel to the horizon line, thus indicating that the aircraft is carrying out its turn at the standard rate.

Abstract translation: 本发明的一般领域是用于表示由车载航空电子系统实现的用于飞行器的转向指示器的速率的方法。 该方法包括以图形方式在可视化设备上表示称为“飞机模型”的符号的步骤，所述图形表示是飞机的具体速度及其倾斜角度的函数。 在有利的实施例中，所述飞行器模型包括两个由共同点相互连接并以对称的方式倾斜的直臂，以形成倒V形.V的两个臂的倾斜角与特定的 飞行器的速度，比例系数以这样的方式确定，即当特定速度和倾斜角度对应于与标准速率相符的值时，所述臂平行于地平线，从而指示飞机正在携带 轮到标准率。

公开(公告)号：US11789927B2

公开(公告)日：2023-10-17

申请号：US16935960

申请日：2020-07-22

Applicant: THALES

Inventor： Thierry Ganille ,  Pierre-Yves Dumas ,  Philippe Gaultier

IPC: G06G7/70 ,  G06F16/23 ,  G06F16/29 ,  B64D45/04 ,  G01S19/15

CPC classification number: G06F16/2365 ,  B64D45/04 ,  G01S19/15 ,  G06F16/29

Abstract: The invention relates to a method for validating at least one position stored in a database of an aircraft comprising a satellite positioning system, the database containing at least one radionavigation beacon position, a runway threshold position, and a displaced runway threshold position on a runway, on which the aircraft is intended to land, the validation of said at least one position comprising a consistency check between at least:



a signal received by the aircraft from a radionavigation beacon associated with said at least one position, and
the position of the aircraft provided by the satellite positioning system, and
the value of the position stored in the database.

公开(公告)号：US20210026836A1

公开(公告)日：2021-01-28

申请号：US16935960

申请日：2020-07-22

Applicant: THALES

Inventor： Thierry Ganille ,  Pierre-Yves Dumas ,  Philippe Gaultier

IPC: G06F16/23 ,  G06F16/29 ,  B64D45/04 ,  G01S19/15

Abstract: The invention relates to a method for validating at least one position stored in a database of an aircraft comprising a satellite positioning system, the database containing at least one radionavigation beacon position, a runway threshold position, and a displaced runway threshold position on a runway, on which the aircraft is intended to land, the validation of said at least one position comprising a consistency check between at least: a signal received by the aircraft from a radionavigation beacon associated with said at least one position, and the position of the aircraft provided by the satellite positioning system, and the value of the position stored in the database.