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公开(公告)号：US10589875B2
公开(公告)日：2020-03-17
申请号：US16027779
申请日：2018-07-05
Applicant: Airbus Operations SAS
Inventor： Bernard Guering , Matthieu De Kergommeaux
Abstract: To facilitate the thermophonic insulation of an aircraft section, a method comprises engaging first respective parts of flexible structures, respectively connected to two flat mattresses, with a support device, by leaving free respective second parts of the flexible structures arranged at a distance from the first parts, then curving the two mattresses, by virtue of the mutual bringing together of the second parts, then inserting the support device into the aircraft section, and detaching each mattress from the support device and fixing each mattress to an aircraft structure delimiting the aircraft section.
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公开(公告)号：US20180094761A1
公开(公告)日：2018-04-05
申请号：US15717045
申请日：2017-09-27
Applicant: Airbus Operations SAS
Inventor： Bernard Guering
CPC classification number: F16L55/1608 , B64D13/00 , B64D13/06 , B64D2013/0614 , F16L21/06 , F16L59/14 , F16L2201/60
Abstract: A fluidic piping system for aircraft, comprising a pipe made in a single piece and an insulating sheath surrounding the pipe. The pipe comprises potential cutoff zones defining sections of the fluidic piping system, reinforced zones arranged in pairs on either side of each potential cutoff zone, and non-reinforced zones defined between the pairs of reinforced zones as intermediate zones. An aircraft system, such as a ventilation and air conditioning module for an aircraft avionics bay, can comprise a limited number of such fluidic piping systems, and can easily be repaired by replacing a damaged section of the piping without it being necessary to disassemble the aircraft equipped with such a system.
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公开(公告)号：US09714096B2
公开(公告)日：2017-07-25
申请号：US14136746
申请日：2013-12-20
Applicant: Airbus Operations (SAS)
Inventor： Yves Durand , Bernard Guering
CPC classification number: B64D13/00 , B64D2013/0614 , H05K7/20145 , H05K7/2059 , Y02T50/44
Abstract: An air extraction unit taking the form of a body, the geometric shape of which makes it easier to incorporate into an avionics bay of an aircraft. The air extraction unit derives from a multipurpose approach to the operational components of the avionics bay of an aircraft aimed at achieving weight and cost savings. All of the elements of the air extraction circuit are arranged in a compact housing of the body and are protected by the structure thereof. The air extraction unit can be used as a floor of an avionics bay that can be walked on, with a lateral organization.
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14.发明申请公开(公告)号：US20170166296A1
公开(公告)日：2017-06-15
申请号：US15370037
申请日：2016-12-06
Applicant: Airbus Operations SAS
Inventor： Bernard Guering , Laurent Saint-Marc
IPC: B64C13/04
CPC classification number: B64C13/044 , B64C25/44 , G05G1/405
Abstract: The rudder bar includes two actuation arrangements, each provided with two pedals, each actuation arrangement having a frame provided with two rails arranged on either side of said frame and being in the form of a concave curve, and, associated with each one of said rails, a movable carriage, each one of said movable carriages bearing one of said pedals, each one of said movable carriages being configured such that it can be moved on the associated rail, for a direction command, under an action exerted by at least one foot of a pilot on at least one of said pedals.
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15.发明申请TOOLING ASSEMBLY FOR INTEGRATING A CENTRAL PART OF AN AIRCRAFT, ASSOCIATED METHOD AND AIRCRAFT THUS INTEGRATED 审中-公开用于集成飞机的中央部分的装配组件，相关方法和航空器集成公开(公告)号：US20160304218A1
公开(公告)日：2016-10-20
申请号：US15133766
申请日：2016-04-20
Applicant: Airbus Operations (SAS)
Inventor： Bernard Guering , Laurent Saint-Marc
CPC classification number: B64D11/003 , B64C1/068 , B64C1/18 , B64D11/06 , B64F5/10
Abstract: A tooling assembly for integrating a central part of the fuselage of an aircraft. The tooling assembly comprises a tooling train which comprises a succession of movable carriages arranged behind one another and which are able to carry one or more items of aircraft equipment to be integrated into the central part of the aircraft. Such a tooling train, which extends over at least a length of the central part of the fuselage, makes it possible to integrate, at the same time, items of aircraft equipment produced in the form of elongate modules, thus reducing the time for integrating the items of aircraft equipment.
Abstract translation: 用于整合飞机机身中央部分的工具组件。 工具组件包括一个加工列车，该加工列车包括一系列相互排列的可移动滑架，并且能够携带一个或多个飞机设备物品整合到飞行器的中心部分。 这种在机身的中心部分的至少长度上延伸的加工列车使得可以同时整合以细长模块的形式生产的飞机设备的物品，从而减少了整合的时间 飞机设备项目。
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Patent Agency Ranking
公开(公告)号：US09434478B2
公开(公告)日：2016-09-06
申请号：US14106113
申请日：2013-12-13
Applicant: Airbus Operations (SAS)
Inventor： Yves Durand , Bernard Guering
CPC classification number: B64D43/00 , B64C1/1476 , B64C1/32
Abstract: The present invention relates to an aircraft cockpit with a double flight deck in which a central pane of a windscreen can be removed in order to at least partially clear an opening in order to constitute an emergency exit and ensure natural ventilation of the cockpit. Moreover, a central portion of a glare shield and of a flight station instrument panel are optionally moveable in order to facilitate access to the opening in the event of the need for emergency evacuation.
Abstract translation: 本发明涉及具有双飞行甲板的飞行器驾驶舱，其中可以移除挡风玻璃的中央窗格以便至少部分地清除开口以构成紧急出口并确保驾驶舱的自然通风。 此外，眩光屏蔽和飞行台仪表板的中心部分可选地可移动，以便在需要紧急撤离的情况下方便进入开口。
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17.发明授权Electrical and electronics bay of an aircraft with an improved architecture and aircraft incorporating said bay 有权具有改进的架构的飞机的电子和电子海湾和结合所述海湾的飞机公开(公告)号：US09351412B2
公开(公告)日：2016-05-24
申请号：US14138543
申请日：2013-12-23
Applicant: Airbus Operations (SAS)
Inventor： Yves Durand , Bernard Guering
CPC classification number: H05K5/0217 , B64D43/00 , H05K7/1412
Abstract: An electrical and electronics bay of an aircraft has at least two rows of systems elements, each row being separated by a single corridor extending an entire longitudinal length of the electrical and electronics bay and being devoid of the systems elements. Each row has at least one set of systems elements and at least one electrical power center, wherein the systems elements are arranged in cabinets. At least one of the cabinets includes at least one removable mobile shelf for allowing access from a front to the back of the cabinets. Bottom edges of back faces of the cabinet are arranged against the fuselage to remove an additional corridor at the back of the cabinet, and front faces of the cabinet are directly accessible from the single corridor.
Abstract translation: 飞机的电气和电子舱具有至少两排系统元件，每排由单个走廊分开，延伸整个电气和电子舱的纵向长度，并且没有系统元件。 每排具有至少一组系统元件和至少一个电力中心，其中系统元件布置在机柜中。 至少一个机柜包括至少一个可移动的移动架，用于允许从橱柜的前部到后面的通道。 机柜背面的底部边缘靠着机身排列，以便在机柜背面移除一个额外的走廊，机柜的正面可以从单个走廊直接进入。
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公开(公告)号：US20150024638A1
公开(公告)日：2015-01-22
申请号：US14332636
申请日：2014-07-16
Applicant: Airbus Operations (SAS)
Inventor： Bernard Guering
IPC: H01R9/22
CPC classification number: H01R9/223 , H01R9/2408 , H01R9/26 , H01R11/09 , H01R2201/26
Abstract: A power breaker strip comprising a strip support and a plurality of interphase spacer elements, and a plurality of interline spacer elements, assembled with the plurality of interphase spacer elements such that each interline spacer element extends at least partly between two consecutive interphase spacer elements. The interphase spacer elements and the interline spacer elements together delimit a plurality of per pitch zones of the strip in which connection terminals of several lines of electrical cables can be inserted.
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19.发明申请公开(公告)号：US20140209740A1
公开(公告)日：2014-07-31
申请号：US14230074
申请日：2014-03-31
Applicant: Airbus Operations SAS
Inventor： Bernard Guering , Alain Depeige
CPC classification number: B60R11/0229 , B64D11/0689 , B64D43/00 , B64D45/00 , B64D2045/0075
Abstract: A device for mixing at least two separate streams of components which, when mixed, form a combined fluid stream. The device comprises a conduit with at least two separate passageways leading to exit openings at an end face of the conduit. Each passageway communicates with a separate component stream and is arranged to direct the separate component stream in a downstream direction. The exit openings each have a predetermined cross-sectional flow area. A separate channel is located at a downstream end of each passageway exit opening. The channels are arranged to redirect the flow from each passageway to an axial direction. A single mixing chamber communicates with all of the separate channels, the mixing chamber being arranged to receive each of the component streams at an upstream end thereof and to permit a mixing of the component streams. An outlet is arranged downstream of the mixing chamber through which the combined fluid stream is dispensed.
Abstract translation: 用于混合至少两个单独的组分流的装置，其在混合时形成组合的流体流。 该装置包括具有至少两个独立通道的导管，导向通道在导管的端面处的出口。 每个通道与单独的部件流连通并且被布置成沿着下游方向引导单独的部件流。 出口各自具有预定的横截面流动面积。 单独的通道位于每个通道出口的下游端。 通道布置成将流从每个通道重新定向到轴向。 单个混合室与所有单独的通道连通，混合室被布置成在其上游端接收每个组分流，并允许组分流的混合。 出口设置在混合室的下游，通过该出口分配组合的流体流。
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公开(公告)号：US20140179211A1
公开(公告)日：2014-06-26
申请号：US14136746
申请日：2013-12-20
Applicant: Airbus Operations (SAS)
Inventor： Yves Durand , Bernard Guering
CPC classification number: B64D13/00 , B64D2013/0614 , H05K7/20145 , H05K7/2059 , Y02T50/44
Abstract: An air extraction unit taking the form of a body, the geometric shape of which makes it easier to incorporate into an avionics bay of an aircraft. The air extraction unit derives from a multipurpose approach to the operational components of the avionics bay of an aircraft aimed at achieving weight and cost savings. All of the elements of the air extraction circuit are arranged in a compact housing of the body and are protected by the structure thereof. The air extraction unit can be used as a floor of an avionics bay that can be walked on, with a lateral organization.
Abstract translation: 空气提取单元采取身体的形式，其几何形状使得更容易地并入飞行器的航空电子设备舱。 空气提取单元来自于一种旨在实现重量和成本节约的飞机航空电子设备的操作部件的多用途方法。 空气提取回路的所有元件都布置在主体的紧凑外壳中，并被其结构保护。 空气提取单元可用作航空电子海湾的地板，可以在侧面组织上行走。
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