公开(公告)号：US20120018580A1

公开(公告)日：2012-01-26

申请号：US13165465

申请日：2011-06-21

Applicant: Julie Holvoet ,  Pierre Charon ,  Olivier Philippe

Inventor： Julie Holvoet ,  Pierre Charon ,  Olivier Philippe

IPC: B64C1/40

CPC classification number: B64C1/406 ,  B64C1/1492

Abstract: This invention proposes an insulation blanket for an aircraft, the said blanket coming in the form of a strip of insulation material of elongated shape having two more or less parallel longitudinal edges (12).This blanket comprises: at least one bar (14) extending over one face of the insulation blanket (6), from one longitudinal edge (12) to the other thereof, as well as means for holding (18) the said bar (14), and the bar (14) bears at least one system support intended to receive a system (30, 32).

Abstract translation: 本发明提出了一种用于飞行器的隔热毯，所述毯子以细长形状的绝缘材料带的形式具有两个或多个平行的纵向边缘（12）。 该毯包括：从绝缘毯（6）的一个面上延伸的至少一个杆（14），从一个纵向边缘（12）到另一个的另一个，以及用于保持（18）所述杆（14）的装置， ，并且所述杆（14）承载旨在接收系统（30,32）的至少一个系统支撑件。

公开(公告)号：US20110309197A1

公开(公告)日：2011-12-22

申请号：US13165461

申请日：2011-06-21

Applicant: Julie Holvoet ,  Matthieu De Kergommeaux ,  Jean-Claude Briois ,  Luc Michelet

Inventor： Julie Holvoet ,  Matthieu De Kergommeaux ,  Jean-Claude Briois ,  Luc Michelet

IPC: F16M13/02 ,  B64C99/00

CPC classification number: B64C1/406 ,  B64C1/40 ,  F16L3/24 ,  H02G3/32 ,  Y02T50/46

Abstract: This device is intended for an aircraft comprising frames, a skin and connecting pieces between the skin and the frames, referred to as clips.It comprises: two brackets (30), each bracket having a first branch (32) intended to be fastened to a clip of the aircraft and a second branch (34) provided with a slot (36), a stirrup-shaped clip (1) comprising a base (2) and two arms (4, 6), each arm (4, 6) having at its free end a securing lug (17) adapted for being able to be inserted in the slot (36) of one of the said brackets with a flange (19) that forms a stop countering displacement of the securing lug once the latter is inserted into the said slot, each arm (4, 6) further comprising at least one support (14, 22) for accommodating a system.

Abstract translation: 该装置适用于包括框架，皮肤以及皮肤和框架之间的连接件（称为夹子）的飞行器。 它包括：两个支架（30），每个支架具有一个第一分支（32），用于固定到飞行器的一个夹子上;第二分支（34）设置有一个槽（36），一个镫形的夹子 ），其包括基部（2）和两个臂（4,6），每个臂（4,6）在其自由端处具有固定凸耳（17），该固定凸耳适于能够插入到 所述支架具有凸缘（19），所述凸缘（19）在所述凸缘插入所述槽中时形成所述固定凸耳的止动对抗位移，每个臂（4,6）还包括至少一个支撑件（14,22） 系统。

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。

公开(公告)号：US09010687B2

公开(公告)日：2015-04-21

申请号：US13165465

申请日：2011-06-21

Applicant: Julie Holvoet ,  Pierre Charon ,  Olivier Philippe

Inventor： Julie Holvoet ,  Pierre Charon ,  Olivier Philippe

IPC: B64C1/40 ,  B64C1/14

CPC classification number: B64C1/406 ,  B64C1/1492

Abstract: This invention proposes an insulation blanket for an aircraft, the said blanket coming in the form of a strip of insulation material of elongated shape having two more or less parallel longitudinal edges (12).This blanket comprises: at least one bar (14) extending over one face of the insulation blanket (6), from one longitudinal edge (12) to the other thereof, as well as means for holding (18) the said bar (14), and the bar (14) bears at least one system support intended to receive a system (30, 32).

Abstract translation: 本发明提出了一种用于飞行器的隔热毯，所述毯子以细长形状的绝缘材料带的形式具有两个或多个平行的纵向边缘（12）。 该毯包括：从绝缘毯（6）的一个面上延伸的至少一个杆（14），从一个纵向边缘（12）到另一个的另一个，以及用于保持（18）所述杆（14）的装置， ，并且所述杆（14）承载旨在接收系统（30,32）的至少一个系统支撑件。

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：US08523112B2

公开(公告)日：2013-09-03

申请号：US13165461

申请日：2011-06-21

Applicant: Julie Holvoet ,  Matthieu De Kergommeaux ,  Jean-Claude Briois ,  Luc Michelet

Inventor： Julie Holvoet ,  Matthieu De Kergommeaux ,  Jean-Claude Briois ,  Luc Michelet

IPC: B64C1/40 ,  F16B1/00

CPC classification number: B64C1/406 ,  B64C1/40 ,  F16L3/24 ,  H02G3/32 ,  Y02T50/46

Abstract: A device for holding an insulating blanket and for fastening systems for an aircraft including aircraft frames, a skin, and connecting pieces between the skin and the frames, the connecting pieces including clips, includes two brackets and a member that contours at least a portion of one of the aircraft frames. Each bracket has a first branch configured to be fastened to one of the clips and a second branch provided with a slot. The member that contours at least a portion of one of the aircraft frames includes a base and two arms. Each arm has a free end forming a securing lug configured to be inserted into the slot of one of the brackets with a flange which forms a stop countering displacement of the securing lug once the latter is inserted into the slot. Each arm further includes at least one support configured to accommodate a system.

Abstract translation: 一种用于保持绝缘毯并用于紧固系统的装置，包括飞机框架，皮肤以及皮肤和框架之间的连接件，所述连接件包括夹子，包括两个托架和至少一部分轮廓的构件 其中一架飞机架。 每个支架具有构造成紧固到一个夹子的第一分支和设置有槽的第二分支。 轮廓至少一部分飞机框架的构件包括底座和两个臂。 每个臂具有形成固定凸耳的自由端，所述固定凸耳被构造成用凸缘插入到一个托架中的槽中，该凸缘在固定凸耳插入槽中时形成止动抵抗位移。 每个臂还包括构造成容纳系统的至少一个支撑件。