公开(公告)号：US11661207B2

公开(公告)日：2023-05-30

申请号：US17159808

申请日：2021-01-27

Applicant: THALES

Inventor： Henri Belfy ,  Laurent Flotte ,  Frédéric Marot

IPC: B64D45/00 ,  B64C19/00 ,  B64C39/02 ,  G07C5/08

CPC classification number: B64D45/00 ,  B64C19/00 ,  B64C39/024 ,  G07C5/0816 ,  B64D2045/0085 ,  B64U2201/00

Abstract: The invention relates to an electronic device for the centralized computation and diffusion of the state(s) of an aircraft, configured for at least calculate the value of one or more aircraft state(s), generate a list of aircraft state(s) the value of which is accessible via the electronic device, the list comprising, for each state, information representative of the said state, diffuse the list to each consumer avionics device, of at least one value of at least one state, receive, from at least one consumer avionics device, at least one request for transmission of one or more values of at least one first state selected from the list, the request comprising the said representative information related to the said at least one first selected state, and transmit, to at least one consumer avionics device, only the value or values of the at least one selected state.

公开(公告)号：US10854097B2

公开(公告)日：2020-12-01

申请号：US16664342

申请日：2019-10-25

Applicant: THALES

Inventor： Laurent Flotte ,  Ronan Demoment ,  Stéphane Fleury ,  Xavier Rueff ,  Daniel Maulet

IPC: G08G5/04

Abstract: An anti-collision device of an aircraft including a plurality of sensors, the plurality of sensors including at least two separate sensors, each sensor being configured to respectively deliver its own set of captured data as a function of the proximity of at least one obstruction, the anti-collision device including: at least one data homogenization module configured to transform at least one set of captured data in a corresponding set of unmarked data, each set of unmarked data respectively associated with at least one sensor being made up of a plurality of identical data types from one set of unmarked data to another, and a data processing module configured to generate, from said sets of unmarked data, at least one piece of information representative of the presence or absence of obstruction(s).

公开(公告)号：US10510243B2

公开(公告)日：2019-12-17

申请号：US16148834

申请日：2018-10-01

Applicant: THALES

Inventor： Chris Deseure ,  Laurent Flotte

IPC: G08B29/18 ,  G05B23/02 ,  G06F11/07 ,  G06F11/28 ,  B64D45/00

Abstract: A method for processing an error when performing a predetermined avionics procedure, related computer program and detection and alert system is disclosed. In one aspect, the method is carried out automatically by the detection and alert system of an aircraft, the method including monitoring the operation of one or several avionics device(s) of the aircraft, the monitoring based on the tracking of a sequence representative of the predetermined avionics procedure being carried out. The method further includes: detecting a break of the sequence due to an incorrect command and/or skipping of at least one expected command according to the predetermined avionics procedure being performed, and retrieving at least one piece of information representative of the break in the sequence.

公开(公告)号：US09965963B2

公开(公告)日：2018-05-08

申请号：US15171887

申请日：2016-06-02

Applicant: THALES

Inventor： Grégoire Jacotot ,  Cédric Flaven ,  Laurent Flotte

IPC: G08G5/00 ,  G05D1/00 ,  G06F11/16

CPC classification number: G08G5/0047 ,  G05D1/0077 ,  G06F11/16

Abstract: A method for monitoring the flight trajectory of an aircraft comprises the steps reiterated in time consisting in receiving and comparing two trajectory objects, the trajectory objects being associated with two initially identical flight trajectories determined independently of each other over time; and, in case of difference between the two trajectory objects, determining a failed trajectory from the two flight trajectories by comparison with the last known state without fault, the last known state without fault corresponding to two identical trajectory objects. Developments describe the use of flight plan segments, of signatures, fault isolation simultaneously to a change of current leg, the use of levels of operational safety according to an RNP-AR procedure and the notification of the pilot of the trajectory determined as having failed. Software and system aspects are also described.

公开(公告)号：US10569899B2

公开(公告)日：2020-02-25

申请号：US16141217

申请日：2018-09-25

Applicant: THALES

Inventor： Chris Deseure ,  Laurent Flotte ,  Guillaume Urbanski

IPC: G08B21/00 ,  B64D45/00 ,  G06Q10/06 ,  G06Q50/30 ,  B64F5/60 ,  G05B23/02

Abstract: The invention relates to a method for controlling the restitution of alert(s) and/or of system(s) reconfiguration procedure(s), including the surveillance of device(s) of a vehicle and the determination of alert(s) and/or of associated reconfiguration procedure(s) to be restituted for the crew, the vehicle operating according to a mission carried out by using at least one operational capacity, and further including, for a current mission: obtaining a list of operational capacities required by said current mission; from said required operational capacities and at least one piece of information from an accessible database, controlling the restitution of alert(s) and/or of system(s) reconfiguration procedure(s) by: modifying the associated level of alert(s) and/or of procedure(s), and sequencing the restitution of alert(s) and/or of procedure(s) based on said level, and/or filtering said alert(s) and/or reconfiguration procedure(s) before restitution.

公开(公告)号：US10358231B2

公开(公告)日：2019-07-23

申请号：US15344676

申请日：2016-11-07

Applicant: THALES

Inventor： Laurent Flotte ,  Chris Deseure ,  Guillaume Urbanski

IPC: B64D45/00 ,  B64D15/20 ,  B64D43/00 ,  G08G5/00 ,  G05B23/02

Abstract: This decision aid method includes the following steps: acquiring (110) operating states of systems, the operating states being determined by a monitoring system; determining (120) an availability state of each operational capacity, based on the operating states of only the systems of the aircraft implementing that operational capacity, each availability state being chosen from among the group consisting of: a normal state, a downgraded state, an impacted state and a lost state; selecting (150) one or more operational capacities based on the current movement context of the aircraft; communicating (150) the availability state of each selected operational capacity to the pilot.

公开(公告)号：US20190122570A1

公开(公告)日：2019-04-25

申请号：US16165882

申请日：2018-10-19

Applicant: THALES

Inventor： Laurent Flotte ,  Ronan Demoment ,  Stéphane Fleury

IPC: G08G5/04 ,  G05B15/02 ,  G08G5/00

Abstract: A method for determining endpoint(s) for deciding to trigger evasive maneuver by an aircraft, an associated device and computer program are disclosed. In one aspect, the method includes obtaining an anticipated route of the aircraft and a set of locations on the route presenting a collision risk for the aircraft, determining, for each location of the set, an endpoint for deciding to trigger an evasive maneuver associated with the location, by applying a rule for determining an endpoint associated with the location, and segmenting the route into a set of N route segments, with N≥2. The rule for determining the endpoint associated with the location of the set is a function of the route segment in which the location associated with the set is located.