公开(公告)号：US08678317B2

公开(公告)日：2014-03-25

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: B64C1/06

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

Abstract: A fastening assembly for the fastening of systems in an aircraft comprising frames, a skin, and clips between the skin and the frames. The fastening assembly includes: ramps, that extend between two consecutive frames of the aircraft; brackets for fastening the ramps to two of the clips situated respectively on two consecutive frames of the aircraft; system supports, fastened to the ramps, each system support being able to receive at least one system.

Abstract translation: 一种用于在航空器中紧固系统的紧固组件，包括框架，皮肤和皮肤和框架之间的夹子。 紧固组件包括：斜面，其在飞机的两个连续的框架之间延伸; 用于将斜坡固定到分别位于飞机的两个连续帧上的两个夹子的支架; 系统支持，固定到斜坡，每个系统支持能够接收至少一个系统。

公开(公告)号：US20110309196A1

公开(公告)日：2011-12-22

申请号：US13165115

申请日：2011-06-21

Applicant: Lionel SABADIE ,  Maximilien FAUVET ,  Laurent REBOLLOSO ,  Michel DAL-CIN

Inventor： Lionel SABADIE ,  Maximilien FAUVET ,  Laurent REBOLLOSO ,  Michel DAL-CIN

IPC: B64C7/00 ,  B64C1/40 ,  B64C1/06 ,  F16M13/02 ,  F16B45/00

CPC classification number: B64C1/406 ,  Y02T50/46

Abstract: This device for holding an insulating blanket and for fastening systems in an aircraft comprises a base (2) having two ends from each of which there extends an arm (4, 6).The base (2) of elongated shape defines a plane, referred to as reference plane, comprising two longitudinal edges (8), and at one end of the base (2), each longitudinal edge (8) has a flange (38) extending from the base (2) on the same side as arms (4, 6).An arm (6) is jointed onto the base (2).The said device further comprises at least one support (46, 54) for accommodating a system.

Abstract translation: 用于保持绝缘毯和用于紧固系统在飞行器中的装置包括具有两个端部的基部（2），每个端部延伸有臂（4,6）。 细长形状的底座（2）限定了一个被称为参考平面的平面，包括两个纵向边缘（8），并且在基部（2）的一端处，每个纵向边缘（8）具有凸缘（38） 从基座（2）在与臂（4,6）相同的一侧。 臂（6）连接在基座（2）上。 所述装置还包括用于容纳系统的至少一个支撑件（46,54）。

公开(公告)号：US08540191B2

公开(公告)日：2013-09-24

申请号：US13165115

申请日：2011-06-21

Applicant: Lionel Sabadie ,  Maximilien Fauvet ,  Laurent Rebolloso ,  Michel Dal-Cin

Inventor： Lionel Sabadie ,  Maximilien Fauvet ,  Laurent Rebolloso ,  Michel Dal-Cin

IPC: B64C1/40 ,  F16B1/00

CPC classification number: B64C1/406 ,  Y02T50/46

Abstract: A device for holding an insulating blanket and for fastening systems in an aircraft includes a base and at least one support. The base has two ends from each of which there extends an arm. One arm is a jointed arm that is jointed onto the base to be pivotable relative to the base. The at least one support is configured to accommodate a system. The base includes an elongated shape and defines a plane, the base includes two longitudinal edges, and at one end of the base, each longitudinal edge has a flange extending from the base on a same side of the base from which the arms extend.

Abstract translation: 用于保持绝缘毯并用于在飞行器中紧固系统的装置包括基座和至少一个支撑件。 底座有两个端部，每个端部延伸一个臂。 一个臂是一个连接的臂，它被连接到基座上以相对于基座可枢转。 所述至少一个支撑件配置成容纳系统。 基部包括细长形状并且限定平面，基部包括两个纵向边缘，并且在基部的一端处，每个纵向边缘具有在基部的与臂延伸的同一侧上从基部延伸的凸缘。

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。