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    Intermediate support structure for the cockpit of an aircraft
    1.
    发明授权
    Intermediate support structure for the cockpit of an aircraft 有权
    飞机驾驶舱的中间支撑结构

    公开(公告)号：US09090327B2

    公开(公告)日：2015-07-28

    申请号：US13541188

    申请日：2012-07-03

    Applicant: Marc Tomasi ,  Patrick Lieven ,  Romain Delahaye

    Inventor： Marc Tomasi ,  Patrick Lieven ,  Romain Delahaye

    IPC: B64D11/00 ,  B64C1/06 ,  B64C1/18 ,  B64D13/00 ,  B64D43/00

    CPC classification number: B64C1/068 ,  B64C1/18 ,  B64C2211/00 ,  B64D11/00 ,  B64D13/00 ,  B64D43/00 ,  B64D2011/0046 ,  Y02T50/44 ,  Y02T50/46

    Abstract: An intermediate support structure for the cockpit of an aircraft is provided. The intermediate support structure includes a raised floor and at least one structural element extending as an arch above the raised floor, the arched structure being adapted to hold in position at least one item of equipment in the upper part of the cockpit. The intermediate support structure also includes a fastener for mounting the intermediate support structure onto a fuselage primary structure, where the fuselage primary structure defines a portion of the cockpit of the aircraft.

    Abstract translation: 提供了一种用于飞机驾驶舱的中间支撑结构。 中间支撑结构包括高架地板和至少一个构造元件，该构件在凸起地板上方延伸成拱形，拱形结构适于在驾驶舱上部的至少一个设备物品上保持位置。 中间支撑结构还包括用于将中间支撑结构安装到机身主结构上的紧固件，其中机身一次结构限定飞行器驾驶舱的一部分。

    INTERIOR COVERING DEVICE FOR AN AIRCRAFT CABIN INCORPORATING AT LEAST ONE SYSTEM
    2.
    发明申请
    INTERIOR COVERING DEVICE FOR AN AIRCRAFT CABIN INCORPORATING AT LEAST ONE SYSTEM 有权
    用于最少一个系统的飞机舱的内部覆盖装置

    公开(公告)号：US20120012218A1

    公开(公告)日：2012-01-19

    申请号：US13181074

    申请日：2011-07-12

    Applicant: Lionel SABADIE ,  Laurent Bertrandeau ,  Thomas Bernabe ,  Christian Banis ,  Marc Tomasi

    Inventor： Lionel SABADIE ,  Laurent Bertrandeau ,  Thomas Bernabe ,  Christian Banis ,  Marc Tomasi

    IPC: F16L3/00

    CPC classification number: B64C1/066 ,  B64C1/406 ,  B64D2011/0046 ,  H02G3/32

    Abstract: The invention relates to a device for interior covering (1) of an aircraft cabin, intended to be fastened to a structure of an aircraft and to extend along a skin of the aircraft, the said device comprising a covering panel (2).The covering panel bears at least one system, possibly through a system support.It advantageously comprises at least one air circulation pipe (3), referred to as air pipe, fastened to an exterior face (6) of the covering panel, each air pipe having an end (26), referred to as upstream end, equipped with a connection device (27).

    Abstract translation: 本发明涉及一种用于飞机机舱的内部覆盖物（1）的装置，其旨在被紧固到飞行器的结构并沿飞机的皮肤延伸，所述装置包括覆盖板（2）。 至少有一个系统可以通过系统支持来覆盖。 它有利地包括紧固到覆盖板的外表面（6）的至少一个称为空气管的空气循环管（3），每个空气管具有一个称为上游端的端部（26），其配备有 连接装置（27）。

    INSTALLATION ASSEMBLY INCLUDING A FIXATION RAIL FOR ATTACHING DEVICES IN AN AIRCRAFT
    4.
    发明申请
    INSTALLATION ASSEMBLY INCLUDING A FIXATION RAIL FOR ATTACHING DEVICES IN AN AIRCRAFT 有权
    安装组件，包括用于在飞机上安装设备的固定轨

    公开(公告)号：US20120160962A1

    公开(公告)日：2012-06-28

    申请号：US13165108

    申请日：2011-06-21

    Applicant: Julie Holvoet ,  Maximilien Fauvet ,  Didier Reynes ,  Marc Tomasi ,  Laurent Rebolloso ,  Luc Michelet

    Inventor： Julie Holvoet ,  Maximilien Fauvet ,  Didier Reynes ,  Marc Tomasi ,  Laurent Rebolloso ,  Luc Michelet

    IPC: B64C1/00 ,  B64C1/06

    CPC classification number: B64C1/406 ,  F16L3/1058 ,  F16L3/1203 ,  F16L3/13 ,  H02G3/32

    Abstract: The invention relates to a fastening assembly for the fastening of systems in an aircraft comprising frames (104), a skin (102) and connecting parts between the skin and the frames, referred to as clips (106), comprising: ramps (2), each ramp being adapted for extending between two consecutive frames of the aircraft; for each ramp, means (4) for fastening the ramp allowing fastening of the said ramp to two clips (106) situated respectively on two consecutive frames of the aircraft, system supports (18, 34), fastened or adapted for being fastened to the ramps, each system support being able to receive at least one system.

    Abstract translation: 本发明涉及一种紧固组件，用于将系统紧固在包括框架（104），皮肤（102）以及皮肤和框架之间的连接部件（称为夹子）的航空器中，包括：斜面（2） 每个斜坡适于在飞行器的两个连续的帧之间延伸; 对于每个斜坡，用于紧固斜坡的装置（4）允许将所述斜坡紧固到分别位于飞行器的两个连续框架上的两个夹子（106），系统支撑件（18,34）被紧固或适于紧固到 斜坡，每个系统支持能够接收至少一个系统。

    Fixation mechanism for installing thermal insulation sheets in an aircraft body
    6.
    发明授权
    Fixation mechanism for installing thermal insulation sheets in an aircraft body 有权
    用于固定绝缘毯和紧固系统的装置

    公开(公告)号：US08622348B2

    公开(公告)日：2014-01-07

    申请号：US13165446

    申请日：2011-06-21

    Applicant: Lionel Sabadie ,  Guillaume Courtin ,  Gilles Andrieu ,  Marc Tomasi ,  Didier Reynes ,  Christian Banis ,  Jean-Claude Briois

    Inventor： Lionel Sabadie ,  Guillaume Courtin ,  Gilles Andrieu ,  Marc Tomasi ,  Didier Reynes ,  Christian Banis ,  Jean-Claude Briois

    IPC: B64C1/06

    CPC classification number: B64C1/406 ,  H02G3/32 ,  Y02T50/46

    Abstract: The invention relates to a device for holding an insulating blanket and for fastening systems in an aircraft, comprising a base having two ends from each of which an arm extends.At least one arm has a U-shaped part having two more or less parallel branches, and in that the said device further comprises at least one support for accommodating a system.The invention also relates to an aircraft fuselage section comprising frames, an outer skin, stabilizers and at least one insulating blanket. This section comprises at least one holding device such as described above, mounted so that a frame is situated between the arms of the holding device so that the blanket is between the frame and the holding device.

    Abstract translation: 本发明涉及一种用于保持绝缘毯并用于在飞行器中紧固系统的装置，包括具有两个端部的基座，每个臂部延伸。 至少一个臂具有具有两个或更多个平行分支的U形部分，并且所述装置还包括用于容纳系统的至少一个支撑件。 本发明还涉及一种包括框架，外皮，稳定器和至少一个绝缘毯的飞机机身部分。 该部分包括如上所述的至少一个保持装置，其被安装成使得框架位于保持装置的臂之间，使得橡皮布在框架和保持装置之间。

    FIXATION MECHANISM FOR INSTALLING THERMAL INSULATION SHEETS IN AN AIRCRAFT BODY
    8.
    发明申请
    FIXATION MECHANISM FOR INSTALLING THERMAL INSULATION SHEETS IN AN AIRCRAFT BODY 有权
    用于在飞机机体中安装热绝缘片的固定机构

    公开(公告)号：US20110315823A1

    公开(公告)日：2011-12-29

    申请号：US13165446

    申请日：2011-06-21

    Applicant: Lionel Sabadie ,  Guillaume Courtin ,  Gilles Andrieu ,  Marc Tomasi ,  Didier Reynes ,  Christian Banis ,  Jean-Claude Briois

    Inventor： Lionel Sabadie ,  Guillaume Courtin ,  Gilles Andrieu ,  Marc Tomasi ,  Didier Reynes ,  Christian Banis ,  Jean-Claude Briois

    IPC: B64C7/00 ,  B64C1/40 ,  B64C1/06 ,  F16M13/02

    CPC classification number: B64C1/406 ,  H02G3/32 ,  Y02T50/46

    Abstract: The invention relates to a device for holding an insulating blanket and for fastening systems in an aircraft, comprising a base having two ends from each of which an arm extends.At least one arm has a U-shaped part having two more or less parallel branches, and in that the said device further comprises at least one support for accommodating a system.The invention also relates to an aircraft fuselage section comprising frames, an outer skin, stabilizers and at least one insulating blanket. This section comprises at least one holding device such as described above, mounted so that a frame is situated between the arms of the holding device so that the blanket is between the frame and the holding device.

    Abstract translation: 本发明涉及一种用于保持绝缘毯并用于在飞行器中紧固系统的装置，包括具有两个端部的基座，每个臂部延伸。 至少一个臂具有具有两个或更多个平行分支的U形部分，并且所述装置还包括用于容纳系统的至少一个支撑件。 本发明还涉及一种包括框架，外皮，稳定器和至少一个绝缘毯的飞机机身部分。 该部分包括如上所述的至少一个保持装置，其被安装成使得框架位于保持装置的臂之间，使得橡皮布在框架和保持装置之间。

    Intermediate support structure for the cockpit of an aircraft
    9.
    发明申请
    Intermediate support structure for the cockpit of an aircraft 有权
    飞机驾驶舱的中间支撑结构

    公开(公告)号：US20130009007A1

    公开(公告)日：2013-01-10

    申请号：US13541188

    申请日：2012-07-03

    Applicant: Marc Tomasi ,  Patrick Lieven ,  Romain Delahaye

    Inventor： Marc Tomasi ,  Patrick Lieven ,  Romain Delahaye

    IPC: B64D11/00 ,  B64D13/06 ,  B64C1/18

    CPC classification number: B64C1/068 ,  B64C1/18 ,  B64C2211/00 ,  B64D11/00 ,  B64D13/00 ,  B64D43/00 ,  B64D2011/0046 ,  Y02T50/44 ,  Y02T50/46

    Abstract: An intermediate support structure (10) for the cockpit of an aircraft comprises a raised floor (11) and at least one structural element (12,13) extending as an arch above the raised floor, said arched structure (12, 13) being adapted to hold in position at least one item of equipment (51) in the upper part of the cockpit, and comprises means for mounting said intermediate structure (10) onto a fuselage primary structure (100), defining a portion of the cockpit of an aircraft.

    Abstract translation: 一种用于飞行器驾驶舱的中间支撑结构（10）包括高架地板（11）和至少一个构造元件（12,13），所述至少一个结构元件（12,13）在凸起的地板上延伸成拱形，所述拱形结构（12,13）适于 在驾驶舱的上部中保持至少一件设备（51）的位置，并且包括用于将所述中间结构（10）安装到机身主结构（100）上的装置，其限定飞机的驾驶舱的一部分 。

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