公开(公告)号：US20200167117A1

公开(公告)日：2020-05-28

申请号：US16691220

申请日：2019-11-21

Applicant: THALES

Inventor： Loïc BECOUARN ,  Florent MENNECHET ,  Valery BOTA

IPC: G06F3/14 ,  B64D43/00

Abstract: The display system has a non-planar three-dimensional display surface defined by an electronic display screen or a plurality of contiguous electronic display screens, the display surface having at least one curved display area having the form of a developable surface.

公开(公告)号：US20200097168A1

公开(公告)日：2020-03-26

申请号：US16579242

申请日：2019-09-23

Applicant: THALES

Inventor： Florent MENNECHET ,  Valéry Bota

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

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.

公开(公告)号：US20180315322A1

公开(公告)日：2018-11-01

申请号：US15960459

申请日：2018-04-23

Applicant: THALES

Inventor： Xavier SERVANTIE ,  Florent MENNECHET

IPC: G08G5/00 ,  G08G5/04 ,  B64D43/00

CPC classification number: G08G5/0021 ,  B64D43/00 ,  G01C23/005 ,  G02B27/0101 ,  G02B2027/0141 ,  G08G5/0052 ,  G08G5/0069 ,  G08G5/0078 ,  G08G5/04 ,  G08G5/045

Abstract: A method of visualization of the traffic around a reference aircraft including acquiring the actual position of a surrounding aircraft, delimiting part of the airspace around this position by a current three-dimensional contour, visualizing the current three-dimensional contour, tracking the actual position of the surrounding aircraft, and when this position is outside the current three-dimensional contour: delimiting part of the airspace around the actual position of the surrounding aircraft by a new current three-dimensional contour, and visualizing the current three-dimensional contour.

公开(公告)号：US20200262575A1

公开(公告)日：2020-08-20

申请号：US16790434

申请日：2020-02-13

Applicant: THALES

Inventor： Florent MENNECHET ,  Xavier SERVANTIE ,  Daniel HAURET

IPC: B64D37/00 ,  G01F9/02

Abstract: This method for determining at least one fuel cosumption domain for an aircraft is implemented by an electronic device. It comprises acquiring a flight envelope as a function of the altitude and a propulsion variable.It comprises, for at least one flight phase, calculating a consumption limit curve as a function of the altitude and the propulsion variable, corresponding to a forecasted average consumption for said flight phase; and determining—from the flight envelope and the limit curve—the consumption domain as a function of the altitude and the propulsion variable and including a first consumption subdomain lower than the forecasted consumption for said flight phase and a second consumption subdomain greater than said forecasted consumption, the first and second subdomains being separated by the limit curve.

公开(公告)号：US20200165001A1

公开(公告)日：2020-05-28

申请号：US16692448

申请日：2019-11-22

Applicant: Thales

Inventor： Loïc BECOUARN ,  Florent MENNECHET ,  Valery BOTA

IPC: B64D43/00 ,  G09G5/14

Abstract: The display system has a three-dimensional and curved display surface made up of a single electronic display screen or several joined electronic display screens, the display surface having at least one main zone dedicated to a pilot and suitable for being located in front of said pilot, the main zone being substantially planar or concave, and at least one lateral zone associated with each main zone, each lateral zone being concave and laterally extending the associated main zone.