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公开(公告)号：US20140175226A1
公开(公告)日：2014-06-26
申请号：US14138588
申请日：2013-12-23
Applicant: Airbus Operations (SAS)
Inventor： Yves Durand , Bernard Guering
CPC classification number: B64D43/00 , B64C1/18 , B64C2001/009 , B64F5/10 , Y10T29/49826
Abstract: An integral avionics bay module. The module has a structure that has an integral cabin floor on top that closes the structure. Installing such an integral avionics bay structure in a single operation inside a primary fuselage structure considerably reduces the integration time on the final assembly line for the aircraft.
Abstract translation: 一个完整的航空电子海湾模块。 该模块具有在顶部具有整体的舱室结构的结构，其关闭结构。 在主机身结构内的单一操作中安装这样一个整体的航空电子设备舱结构大大减少了飞机最终装配线上的集成时间。
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22.发明申请VENTILATION SYSTEM, AIR BLOWING AND EXTRACTION CIRCUITS OF SUCH A SYSTEM, AS WELL AS AN AIRCRAFT AVIONICS BAY 有权通风系统，这种系统的空气吹扫和提取电路，如航空航天飞机公开(公告)号：US20130082138A1
公开(公告)日：2013-04-04
申请号：US13628153
申请日：2012-09-27
Applicant: Airbus Operations SAS
Inventor： Bernard Guering , Yves Durand
IPC: B64D13/02
CPC classification number: B64C1/18 , B64D13/00 , B64D2013/0614 , H05K7/20554
Abstract: A ventilation system for an avionics bay has two strut assemblies for stiffening the floor of the cockpit, each strut assembly being arranged symmetrically regarding to the central plane of the aircraft, and means of distribution of the blowing air in the cabinets of the bay from the strut assemblies. The extraction circuit includes exhaust ducts integrated in the cabinets and couples together by tight inter-cabinets junctions in an overall configuration of maximized compactness.
Abstract translation: 用于航空电子设备舱的通风系统具有两个用于加强驾驶舱地板的支柱组件，每个支柱组件关于飞行器的中心平面对称地布置，以及将吹风空气分配在舱的机柜中的装置， 支柱组件。 提取电路包括集成在机柜中的排气管道，并通过紧密的机柜间连接在一起，以最大的紧凑性的整体结构。
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23.发明授权公开(公告)号：US11731781B2
公开(公告)日：2023-08-22
申请号：US16814513
申请日：2020-03-10
Applicant: Airbus Operations SAS
Inventor： Bernard Guering , Romain Delahaye
CPC classification number: B64D43/00 , B64D2011/0046
Abstract: A cabinet comprising at least one screen allowing display of data necessary for a flight-control of an aircraft connected to at least one avionics module for management of the data. The screen at least partially forms one of the sides of the cabinet and the module or modules are installed inside the cabinet. The cabinet has a base allowing the screen or screens to be placed at a desired height. As a result, a length of cable between screen and avionics modules is reduced to a minimum.
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公开(公告)号：US11542012B2
公开(公告)日：2023-01-03
申请号：US16855329
申请日：2020-04-22
Applicant: Airbus Operations SAS
Inventor： Bernard Guering
Abstract: An aerial workstation which comprises a seat having a sitting portion, a backrest that is connected by a first articulation that allows the backrest to pivot relative to the sitting portion, and an arm configured to position the seat in various positions and orientations in space as required. The aerial workstation makes it possible to be able to translate the seat in a cockpit in an introduction direction, and to make it pivot about a pivot axis that coincides with the direction of introduction within the cockpit.
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公开(公告)号：US10358218B2
公开(公告)日：2019-07-23
申请号：US15133766
申请日：2016-04-20
Applicant: Airbus Operations (SAS)
Inventor： Bernard Guering , Laurent Saint-Marc
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.
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Patent Agency Ranking
公开(公告)号：US10071797B2
公开(公告)日：2018-09-11
申请号：US15133758
申请日：2016-04-20
Applicant: Airbus Operations (SAS)
Inventor： Bernard Guering , Laurent Saint-Marc
CPC classification number: B64C1/20 , B64C1/18 , B64C5/02 , B64C25/04 , B64D11/04 , B64D11/0696 , B64D27/02
Abstract: An aircraft comprising a fuselage which has a central part with a cross section of constant geometry which comprises a floor. The floor comprises two lateral portions which are fixed respectively to two opposite lateral edges of the fuselage and which enclose a central portion to which they are fixed. One of the lateral floor portions is fixed to the central portion so as to allow a relative lateral movement between the two portions in the event of a modification in pressure inside the fuselage. The cross section thus deforms homogeneously when the fuselage is pressurized and the floor is not involved in maintaining the shape of the fuselage.
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27.发明申请公开(公告)号：US20170247101A1
公开(公告)日：2017-08-31
申请号：US15441496
申请日：2017-02-24
Applicant: Airbus Operations SAS
Inventor： Bernard Guering
CPC classification number: B64C1/18 , B64C1/065 , B64C1/20 , B64F5/10 , B64F5/50 , B66C13/18 , B66C19/00
Abstract: An aircraft nose floor comprising a grid structure formed by an interlacing of crosspieces and longitudinal elements. The crosspieces are parallel to one another and the longitudinal elements are parallel to one another and fastened to the crosspieces. The floor forms a unified module configured to be transported in one piece to the inside of an aircraft nose during the integration phase. The integration time is reduced, and the operators' tasks are made easier.
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28.发明申请公开(公告)号：US20170166291A1
公开(公告)日：2017-06-15
申请号：US15375478
申请日：2016-12-12
Applicant: Airbus Operations SAS
Inventor： Bernard Guering
Abstract: A zone provided between the forward pressure bulkhead in an aircraft and the floor. The nose section of the aircraft in which the flat surface pressure bulkhead including at least one transverse frame comprises at least two rods, of which one of the front ends is attached to the bulkhead and/or the frame and the other rear end is attached to a structural element, the two rods further apart from the front to the rear, thus providing a work space. Therefore, the rods provide a more comfortable work area while picking up part of the loads from the bulkhead to the floor.
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29.发明授权公开(公告)号：US09592771B2
公开(公告)日：2017-03-14
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: An aircraft cockpit including a viewing device comprising a screen pivotably mounted on a mounting that allows height adjustment. A screen may also be placed at the top central portion of the instrument panel. The central screen is movable between an extended position and a retracted position in which the screen does not block the view of the pilots through the cockpit windscreen. A glare screen cowl, made at least partially of a taut fabric is used to cover the viewing screens, except optionally the mobile central screen which can pass through the cowl via an opening provided for that purpose. An avionics rack may be positioned forward of the screens of the instrument panel, in which the mounting is advantageously also used to support other devices such as a rudder control system and writing shelves.
Abstract translation: 包括观察装置的飞行器驾驶舱包括可枢转地安装在允许高度调节的安装件上的屏幕。 屏幕也可以放置在仪表板的顶部中央部分。 中央屏幕可在延伸位置和缩回位置之间移动，在该位置屏幕不阻挡飞行员通过驾驶舱挡风玻璃的视野。 至少部分由绷紧织物制成的眩光屏幕罩被用于覆盖观看屏幕，除了可选择地移动的中央屏幕之外，可以通过为此目的提供的开口穿过整流罩。 航空电子设备机架可以位于仪表板的屏幕的前方，其中安装件也有利地用于支撑诸如舵控制系统和书写架的其它装置。
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公开(公告)号：US20160304185A1
公开(公告)日：2016-10-20
申请号：US15133745
申请日：2016-04-20
Applicant: Airbus Operations (SAS)
Inventor： Frederic Vinches , Bernard Guering
Abstract: A cabin space dedicated to passengers and, beneath said cabin space, an under-cabin space which extends along the longitudinal axis of said aircraft. The under-cabin space comprises, distributed along two lines parallel to the longitudinal axis of the aircraft, two sets of systems which are able to carry out functions necessary for the operation of the aircraft. The two lines of sets of systems are disposed respectively in two lateral zones of the under-cabin space which are spaced apart transversely from one another and enclose a free central zone which extends along the longitudinal axis of the aircraft. This arrangement thus eliminates any technical zone from the under-cabin space, thereby facilitating the internal layout and maintenance.
Abstract translation: 一个专用于乘客的驾驶舱空间，以及在所述驾驶舱空间之下的沿着所述飞行器的纵向轴线延伸的下舱空间。 机舱内空间包括沿平行于飞行器的纵向轴线的两条线分布的两组能够执行飞机操作所必需的功能的系统。 两组系统分别设置在舱室空间的两个横向区域中，这两个横向区域彼此横向间隔开并且包围沿飞行器的纵向轴线延伸的自由中心区域。 因此，这种布置消除了从机舱内空间的任何技术区域，从而便于内部布局和维护。
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