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    Aircraft vision system with relief lines and associated method
    121.
    发明授权
    Aircraft vision system with relief lines and associated method 有权

    公开(公告)号：US10011369B2

    公开(公告)日：2018-07-03

    申请号：US14044245

    申请日：2013-10-02

    Applicant: DASSAULT AVIATION

    Inventor： Olivier Baudson ,  Arnaud Turpin

    IPC: B64D45/00 ,  G06T19/00 ,  G01C23/00

    CPC classification number: B64D45/00 ,  G01C23/00 ,  G06T19/006

    Abstract: The vision system for an aircraft according to the invention comprises a display management system, on a display, capable of dynamically displaying synthetic information coming from a synthetic environment generating assembly on the display. The management assembly can control the display, on a first region of the display, of relief lines representative of the terrain situated facing the aircraft, without displaying synthetic surface representations of the terrain in the intermediate areas situated between the relief lines of the first region of the display. The generating assembly includes means for determining the position of the crest lines of the terrain from topographical data present in at least one database, and means for computing the position of the relief lines from the position of the crest lines of the terrain.

    Interior layout assembly of an aircraft cabin, and related method
    122.
    发明授权
    Interior layout assembly of an aircraft cabin, and related method 有权

    公开(公告)号：US09988149B2

    公开(公告)日：2018-06-05

    申请号：US15010722

    申请日：2016-01-29

    Applicant: DASSAULT AVIATION

    Inventor： Yann Maillaut

    IPC: B64D11/00 ,  B64D11/06

    CPC classification number: B64D11/0638 ,  B64D11/0605

    Abstract: An interior layout assembly of an aircraft cabin, and related method are provided. The assembly includes a table, a console defining a receiving housing and a cover mounted on the console. The cover in the closed configuration and the console define a passage slot between them. The assembly also includes a flap closing off the passage slot, movable by the table from an active configuration closing the passage slot to a retracted configuration freeing the passage slot during the passage of the table from its retracted position to the deployed position.

    System for assisting in a dispatch decision of an aircraft and related process
    123.
    发明授权
    System for assisting in a dispatch decision of an aircraft and related process 有权

    公开(公告)号：US09950809B2

    公开(公告)日：2018-04-24

    申请号：US15418705

    申请日：2017-01-28

    Applicant: DASSAULT AVIATION

    Inventor： Rémi Breban

    IPC: G08B21/00 ,  B64D45/00 ,  G05B23/02

    CPC classification number: B64D45/00 ,  G05B23/0272

    Abstract: A system for assisting in a dispatch decision of an aircraft and related process are provided. The system includes a synthesis module, configured to generate at least one dispatch status for the aircraft, based on at least one defect and/or fault datum of the aircraft received from the acquisition module and at least data contained in a first database and in a second minimum equipment list database; and a display, configured to display at least one synthesis window containing at least one defect and/or fault identification indicator of the aircraft developed from the or each defect and/or fault datum, and at least one dispatch status indicator based on the dispatch status determined by the synthesis module.

    Assistance system for the implementation of aircraft procedures comprising a chain of operations to carry out, and related process
    124.
    发明授权
    Assistance system for the implementation of aircraft procedures comprising a chain of operations to carry out, and related process 有权

    公开(公告)号：US09751634B2

    公开(公告)日：2017-09-05

    申请号：US15060815

    申请日：2016-03-04

    Applicant: DASSAULT AVIATION

    Inventor： Bruno Ramirez ,  Gilles Constant ,  Gaëtan Bramoullé

    IPC: G01C21/00 ,  B64D45/00 ,  G05B23/02

    CPC classification number: B64D45/00 ,  G05B23/0272

    Abstract: An assistance system for the implementation of aircraft procedures comprising a chain of operations to carry out is provided. The system includes a procedure database receiving the specifications of a plurality of procedures to be performed and a display and/or validation module which is able to collect the specifications of the procedure, to display a piece of characteristic information at least one operation of the procedure on the basis of the collected specifications, and/or to receive validation of the performance of at least one operation of the procedure. The system includes a conflict determination module which is able to generate for at least one operation of the procedure, feasibility information for the operation of the procedure during the course of the procedure, depending on the current operating states of the functional systems of the aircraft.

    Method of designing a system of electrical wirings for a complex system, and corresponding complex system
    125.
    发明授权
    Method of designing a system of electrical wirings for a complex system, and corresponding complex system 有权

    公开(公告)号：US09734279B2

    公开(公告)日：2017-08-15

    申请号：US14471764

    申请日：2014-08-28

    Applicant: DASSAULT AVIATION

    Inventor： Guillaume Reydellet ,  Philippe Mareschal ,  Romain Bernard

    IPC: G06F17/50 ,  B60R16/023 ,  B60R16/03

    CPC classification number: G06F17/5095 ,  B60R16/023 ,  B60R16/03 ,  G06F2217/36

    Abstract: A method for designing a system of electrical wirings for a complex system, in particular applicable to the design of electrical wirings of an aircraft, is provided. The electrical wirings allow the flow of digital, analog or discrete data between the components of the complex system and/or the transmission of electricity to components of the complex system, the components of the complex system being grouped together in subsystems, each able to perform a predetermined function, and able to be broken down into subsystems each capable of performing a predetermined sub-function. The wirings are distributed into functional groups such that all of the wirings allowing the flow of one or more data and/or the transmission of electricity, directly or indirectly necessary for the operation of the components of a subsystem, for performing the corresponding function or sub-function are distributed in a single and same functional group.

    System and method for controlling and monitoring aircraft equipment
    129.
    发明申请
    System and method for controlling and monitoring aircraft equipment 审中-公开

    公开(公告)号：US20170183085A1

    公开(公告)日：2017-06-29

    申请号：US15385966

    申请日：2016-12-21

    Applicant: DASSAULT AVIATION

    Inventor： Arnaud BRANTHOMME ,  Guy SCHALLER ,  Lorianne BOUTZEN

    IPC: B64C17/10 ,  B64C13/16 ,  G06F3/14 ,  B64C13/04

    CPC classification number: B64C17/10 ,  B64C13/042 ,  B64C13/16 ,  B64D37/00 ,  B64D43/00 ,  F02C9/26 ,  G06F3/14

    Abstract: A system for controlling and monitoring pieces of equipment of an aircraft, each piece of equipment being able to be switched between two logic activation state values, comprising a man-machine interface, a module for configuration of a functional activation state of a function able to be performed on at least pieces of equipment of a system of the aircraft, the functional activation state being configurable between an active state and an inactive state, the configuration module being adapted for detecting an action of selection of a functional activation state of the function by an operator, and a control and monitoring module configured for determining a logic activation state of each of the pieces of equipment of the system, so that, when each of the pieces of equipment is in the determined logic activation state, the function is in the selected functional activation state.

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