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    Head up display system, associated display system and computer program product
    2.
    发明授权
    Head up display system, associated display system and computer program product 有权

    公开(公告)号：US10969589B2

    公开(公告)日：2021-04-06

    申请号：US16612691

    申请日：2019-09-26

    Applicant: THALES

    Inventor： Florent Mennechet ,  Valéry Bota

    IPC: G06F3/041 ,  G02B27/01 ,  G01C23/00 ,  G06F3/0488

    Abstract: The invention relates to a head-up display system embedded in an aircraft pilotable by a pilot and having a head-down display screen. The display system includes: a head-up display screen configured to be arranged in the cockpit in a Plurality of positions and to be observed by the pilot from an observation point along a viewing field; at least one position, called interposition position, of the head-up screen corresponding to a position in which a part, called interposed part, is arranged across from a part of the head-down display screen in the viewing field between the observation point and this part; a display control module configured to display a conformal display area and when the head-up display screen is in the interposition position, a non-conformal display area in the interposed part.

    PLANNING METHOD OF A FLIGHT OF AN AIRCRAFT, ASSOCIATED DISPLAY, COMPUTER PROGRAM PRODUCT AND PLANNING SYSTEM
    3.
    发明申请
    PLANNING METHOD OF A FLIGHT OF AN AIRCRAFT, ASSOCIATED DISPLAY, COMPUTER PROGRAM PRODUCT AND PLANNING SYSTEM 审中-公开

    公开(公告)号：US20200096344A1

    公开(公告)日：2020-03-26

    申请号：US16579580

    申请日：2019-09-23

    Applicant: THALES

    Inventor： Florent Mennechet ,  Valéry Bota

    IPC: G01C21/20 ,  G06F3/0488 ,  G06F3/14

    Abstract: The invention relates to a flight planning method for planning a flight of an aircraft controllable by at least one pilot and comprising a flight management system and a head-down display screen, the flight planning method comprising of the following steps; acquisition of an information item relating to a tactile motion effected by the pilot on the head-down display screen, the head-down display screen displaying a geographical map of the environment of the aircraft; association of the information relating to the tactile motion of the pilot with a first set of geographical points of the geographical map, the first set of geographical points being capable of being used by the flight management system; and displaying of the first set of geographical points on the head-down display screen.

    Guidance method and system for assisting in following a trajectory for velocity-vector piloting of an aircraft
    4.
    发明授权
    Guidance method and system for assisting in following a trajectory for velocity-vector piloting of an aircraft 有权

    公开(公告)号：US11629976B2

    公开(公告)日：2023-04-18

    申请号：US16706484

    申请日：2019-12-06

    Applicant: THALES

    Inventor： Thierry Ganille ,  Florent Mennechet ,  Xavier Servantie

    IPC: G01C23/00 ,  B64D43/00

    Abstract: A method for guidance and for assisting in following a trajectory for velocity-vector piloting of an aircraft includes a step of calculating, at all times, lateral and vertical offsets of the current position of the aircraft from a target trajectory, estimated by a flight management system, and then a joining heading and a joining gradient for the aircraft to join the trajectory depending on these offsets; and a following fourth step of displaying, in head-up or head-down form, a consistent guidance symbol centered on the calculated joining heading and the calculated joining gradient for joining the trajectory, on a piloting screen showing a velocity vector. The fourth step may display, in addition to the guidance symbol, one or more items of information anticipating the next trajectory break.

    Planning method of a flight of an aircraft, associated display computer program product and planning system
    5.
    发明授权
    Planning method of a flight of an aircraft, associated display computer program product and planning system 有权

    公开(公告)号：US10860206B2

    公开(公告)日：2020-12-08

    申请号：US16579242

    申请日：2019-09-23

    Applicant: THALES

    Inventor： Florent Mennechet ,  Valéry Bota

    IPC: G06F3/0488 ,  B64D43/00 ,  G06T17/05 ,  G08G5/00 ,  G06F3/0481

    Abstract: The invention relates to a method for planning the flight of a pilot-piloted aircraft and comprising a tactile head-down display defining a display plane and displaying images representing a three-dimensional surface viewed in perspective through the display plane, and arranged with respect to this display plane according to a display parameter.The method comprises the following steps: acquisition of information relating to a tactile displacement on the display screen; association of the information relating to the tactile displacement with a first set of points located in the display plane; projection of the first set of points on the displayed three-dimensional surface in order to obtain a second set of geographical points located on this three-dimensional surface; and display of images representing the second set.

    Visualization method of the attitude of an aircraft, associated computer program product and visualization system
    7.
    发明授权
    Visualization method of the attitude of an aircraft, associated computer program product and visualization system 有权

    公开(公告)号：US11047707B2

    公开(公告)日：2021-06-29

    申请号：US16261223

    申请日：2019-01-29

    Applicant: THALES

    Inventor： Florent Mennechet ,  Xavier Servantie

    IPC: G01C23/00

    Abstract: The present invention relates to a visualization method of the attitude of an aircraft, comprising the formation of a pitch scale (E) defining a lower border and an upper border, and including: to visualize the nil pitch angle of the aircraft, a zero graduation on the lower border and the upper border; to visualize the negative pitch angles of the aircraft, straight parallel graduations forming at least two groups converging toward one another with the approach of the zero graduation from the lower border; and to visualize the positive pitch angles of the aircraft, curved graduations, the curvature of which increases moving away from the zero graduation toward the upper border.

    VISUALIZATION METHOD OF THE ATTITUDE OF AN AIRCRAFT, ASSOCIATED COMPUTER PROGRAM PRODUCT AND VISUALIZATION SYSTEM
    8.
    发明申请
    VISUALIZATION METHOD OF THE ATTITUDE OF AN AIRCRAFT, ASSOCIATED COMPUTER PROGRAM PRODUCT AND VISUALIZATION SYSTEM 审中-公开

    公开(公告)号：US20190242722A1

    公开(公告)日：2019-08-08

    申请号：US16261223

    申请日：2019-01-29

    Applicant: THALES

    Inventor： Florent Mennechet ,  Xavier Servantie

    IPC: G01C23/00

    CPC classification number: G01C23/005

    Abstract: The present invention relates to a visualization method of the attitude of an aircraft, comprising the formation of a pitch scale (E) defining a lower border and an upper border, and including: to visualize the nil pitch angle of the aircraft, a zero graduation on the lower border and the upper border; to visualize the negative pitch angles of the aircraft, straight parallel graduations forming at least two groups converging toward one another with the approach of the zero graduation from the lower border; and to visualize the positive pitch angles of the aircraft, curved graduations, the curvature of which increases moving away from the zero graduation toward the upper border.

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