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    SLIDE SYSTEM AND SLIDE ASSEMBLY FOR A DRAWER AND DRAWER ASSEMBLY
    41.
    发明申请
    SLIDE SYSTEM AND SLIDE ASSEMBLY FOR A DRAWER AND DRAWER ASSEMBLY 审中-公开

    公开(公告)号：US20180110334A1

    公开(公告)日：2018-04-26

    申请号：US15334572

    申请日：2016-10-26

    Applicant: DASSAULT AVIATION

    Inventor： Ludovic HAMON ,  Grégory LE FLOC'H

    IPC: A47B88/14 ,  A47B88/04 ,  A47B88/10

    CPC classification number: A47B88/43 ,  A47B88/45 ,  A47B88/487 ,  A47B88/493 ,  A47B2210/0059 ,  A47B2210/0078

    Abstract: A slide system for slidably opening and closing a drawer is provided. The slide system includes an outer slide for mounting the slide system on a side wall of an enclosure, comprising a longitudinal slide outer channel, a sliding member, configured to be mounted on a side wall of the drawer, slidably movable within said slide outer channel. The outer slide includes a fixing part for attachment of the outer slide on the side wall of the enclosure, a sliding part comprising said slide outer channel, and an intermediate part, extending from said fixing part to said sliding part. The fixing part, the intermediate part and the sliding part define a groove extending upwardly from said intermediate part. The slide system comprises a casing element for encasing the sliding member by extending vertically from an upper portion the side wall of the drawer towards the intermediate part of the outer slide and being at least partly received within the groove.

    Supporting device for an interior layout assembly of an aircraft cabin, related assembly and method
    42.
    发明授权
    Supporting device for an interior layout assembly of an aircraft cabin, related assembly and method 有权

    公开(公告)号：US09938016B2

    公开(公告)日：2018-04-10

    申请号：US15010696

    申请日：2016-01-29

    Applicant: DASSAULT AVIATION

    Inventor： Nicolas Hance

    IPC: B64D11/00 ,  B64D11/06

    CPC classification number: B64D11/0605 ,  B64D11/0638

    Abstract: A supporting device for an interior layout assembly of an aircraft cabin, a related assembly and method are provided. The device includes a stationary frame; a table that can be deployed relative to the frame between a retracted position and a horizontal deployed position; a mechanism for guiding the movement of the table relative to the frame between the retracted position and the deployed horizontal position. The guide mechanism defines at least one bearing point for the table during its passage from the retracted position to the deployed horizontal position, the bearing point having a globally invariable position relative to the frame, the table being configured to pivot on the bearing point while moving laterally away relative to the bearing point, by sliding on the bearing point, to the deployed position.

    Method for determining a state of credibility of measurements of an incidence sensor of an aircraft and corresponding system
    43.
    发明授权
    Method for determining a state of credibility of measurements of an incidence sensor of an aircraft and corresponding system 有权

    公开(公告)号：US09933451B2

    公开(公告)日：2018-04-03

    申请号：US14388775

    申请日：2013-03-26

    Applicant: DASSAULT AVIATION

    Inventor： Sebastien Dupont De Dinechin

    IPC: B64F5/60 ,  G01P13/02 ,  G01P21/02

    CPC classification number: G01P13/025 ,  B64F5/60 ,  G01P21/025

    Abstract: A method for determining a state of credibility of measurements of an angle-of-attack sensor of an aircraft is provided. This method includes at least one coherence test between angle-of-attack measurements from said angle-of-attack sensor, and the measurements of a flight characteristic of the aircraft, distinct from the angle-of-attack. The coherence test includes determining an angle-of-attack value from said angle-of-attack sensor, determining said flight characteristic of the aircraft, determining a value of at least one indicator of the coherence of the angle-of-attack value with the value of said flight characteristic, and activating a low state of credibility, in which the measurements of said angle-of-attack sensor are deemed unreliable, or an intermediate state of credibility, in which the measurements from said angle-of-attack sensor are deemed coherent with said flight characteristic, based on the value of said coherence indicator.

    SUPPORT FOR A RADIO EQUIPMENT OF AN AIRCRAFT, RADIO SYSTEM AND AIRCRAFT
    44.
    发明申请
    SUPPORT FOR A RADIO EQUIPMENT OF AN AIRCRAFT, RADIO SYSTEM AND AIRCRAFT 审中-公开

    公开(公告)号：US20170320591A1

    公开(公告)日：2017-11-09

    申请号：US15582811

    申请日：2017-05-01

    Applicant: DASSAULT AVIATION

    Inventor： Jérôme TABUTEAU ,  Jérôme BRUNET

    IPC: B64D47/00 ,  B64C1/36 ,  B64D45/00

    Abstract: A support device for a radio equipment of an aircraft, radio system and aircraft are provided. The support device includes a fastening structure (31), intended to be secured to a lower surface of a fuselage of an aircraft, and a support platform (33) of the radio equipment (25). The support platform (33) is mounted pivoting on the fastening structure (31) around a pivot axis (A) between an operational position and a backup position. The support device comprises a locking mechanism (56), able to be actuated from a locked configuration, in which said locking mechanism (56) keeps the support platform (33) in its operational position while preventing any pivoting of the support platform (33), to an unlocked configuration, in which the locking mechanism (56) allows the support platform (33) to pivot relative to the fastening structure (31).

    System for assisting in a dispatch decision of an aircraft and related process
    46.
    发明申请
    System for assisting in a dispatch decision of an aircraft and related process 有权

    公开(公告)号：US20170217602A1

    公开(公告)日：2017-08-03

    申请号：US15418705

    申请日：2017-01-28

    Applicant: DASSAULT AVIATION

    Inventor： Rémi BREBAN

    IPC: B64D45/00

    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.

    Device for displaying flight characteristics of an aircraft, aircraft instruments, and related method
    47.
    发明授权
    Device for displaying flight characteristics of an aircraft, aircraft instruments, and related method 有权
    显示飞机飞行特性，飞机仪表及相关方法的装置

    公开(公告)号：US09574901B2

    公开(公告)日：2017-02-21

    申请号：US14388770

    申请日：2013-03-26

    Applicant: DASSAULT AVIATION

    Inventor： Sebastien Dupont de Dinechin

    IPC: G01P21/00 ,  G01C23/00 ,  B64D43/00

    CPC classification number: G01C23/00 ,  B64D43/00

    Abstract: A device for displaying flight characteristics of an aircraft is provided. The device includes a display for the selective display of flight characteristics of an aircraft, as a function of a state of credibility assigned to measurements from static pressure, total pressure and angle-of-attack sensors, configured for selectively displaying a primary set of flight characteristics comprising at least one flight characteristic coming from a measurement from one of said sensors, when the measurements from said sensors are deemed reliable, and a secondary set of flight characteristics, distinct from said primary set, comprising at least one secondary flight characteristic designed to replace a counterpart flight characteristic from the primary set, when the measurements from at least one sensor are deemed unreliable, said secondary flight characteristic being independent of any measurement by the or each sensor deemed unreliable done when the measurements from that sensor are deemed unreliable.

    Abstract translation: 提供了一种用于显示飞行器飞行特性的装置。 该装置包括用于选择性地显示飞行器的飞行特性的显示器，作为分配给静态压力，总压力和迎角传感器的测量值的可信度状态的函数，被配置用于选择性地显示主要飞行组 特征包括来自所述传感器之一的测量的至少一个飞行特征，当来自所述传感器的测量被认为是可靠的，并且与所述主组不同的第二组飞行特征包括至少一个二次飞行特性，其被设计为 当来自至少一个传感器的测量值被认为不可靠时，替换相对应的飞行特性，当从该传感器的测量被认为不可靠时，所述次要飞行特性与被认为不可靠的任何测量无关。

    COMMUNICATION METHOD BETWEEN AN EMBEDDED COMMUNICATION SYSTEM OF AN AIRCRAFT AND A COMMUNICATION DEVICE, AND COMMUNICATION MODULE, TERMINAL AND ASSEMBLY
    48.
    发明申请
    COMMUNICATION METHOD BETWEEN AN EMBEDDED COMMUNICATION SYSTEM OF AN AIRCRAFT AND A COMMUNICATION DEVICE, AND COMMUNICATION MODULE, TERMINAL AND ASSEMBLY 审中-公开
    飞机和通信设备嵌入式通信系统之间的通信方法以及通信模块，终端和组件

    公开(公告)号：US20170026809A1

    公开(公告)日：2017-01-26

    申请号：US15211528

    申请日：2016-07-15

    Applicant: DASSAULT AVIATION

    Inventor： Stéphane GOUVERNEUR

    IPC: H04W4/04 ,  H04L29/12

    CPC classification number: H04W4/40 ,  H04B7/185 ,  H04L61/605 ,  H04W4/046 ,  H04W76/15 ,  H04W84/06 ,  H04W88/02

    Abstract: A communication method between an embedded communication system of an aircraft and a communication device is provided. The method includes a step for establishing a communication between the embedded communication system and the communication device, done according to a communication parameter associated with the communication device, contained in a memory of a communication terminal. The establishment step includes a phase for establishing a first auxiliary communication between terminal and the communication system, a phase for establishing a second auxiliary communication between the terminal and the communication device, according to the communication parameter, and a phase for transferring the second auxiliary communication from the terminal toward the communication system.

    Abstract translation: 提供了一种飞行器的嵌入式通信系统和通信设备之间的通信方法。 该方法包括根据通信终端的存储器中包含的与通信设备相关联的通信参数来建立嵌入式通信系统和通信设备之间的通信的步骤。 该建立步骤包括用于建立终端与通信系统之间的第一辅助通信的阶段，根据通信参数建立终端和通信设备之间的第二辅助通信的阶段，以及用于传送第二辅助通信的阶段 从终端到通信系统。

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