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1.发明公开
公开(公告)号：EP3365816A1
公开(公告)日：2018-08-29
申请号：EP16790537.1
申请日：2016-10-20
发明人： GONNSEN, Johannes , ZENKER, Marcel
IPC分类号： G06F17/50
CPC分类号： G06F17/5095 , B64D11/0007 , B64D11/0015 , B64D11/02 , G01M1/125 , G06F17/50 , G06F2217/02 , G06F2217/36
摘要： Aircraft configurator for calculating mounting points for consumers (301) and routes (303, 304, 305, 306) along which the consumers are to be connected to adequate aircraft supply systems (302). A computing unit (101) can calculate different connecting routes and select the connecting route for which a key performance indicator is optimal and takes into account additional equipment influencing the route. This allows the efficiency for manufacturing the aircraft and for operating the aircraft to be increased.
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2.发明公开SANITARY MODULE COMPRISING A FOLDING ALCOVE FOR AN AIRCRAFT AND AIRCRAFT DOOR REGION 审中-公开带有折叠壁龛用于飞机和飞机舱门场卫生模块
公开(公告)号：EP3118114A1
公开(公告)日：2017-01-18
申请号：EP16174368.7
申请日：2016-06-14
发明人： GONNSEN, Johannes
IPC分类号： B64D11/02
CPC分类号： B64D25/00 , B64D11/02 , B64D2011/0046
摘要： The present invention provides a sanitary module (1) comprising a folding alcove (10) for an aircraft (100). The sanitary module (1) comprises a side wall (2) which forms a stationary vertical portion of an outer wall (11) of the sanitary module (1); an alcove wall which forms a movable vertical portion of the outer wall (11) of the sanitary module (1) and can be moved into an inner space (4) of the sanitary module (1); and two folding connections which each connect a vertical longitudinal edge of the alcove wall to a vertical longitudinal edge of the side wall (2) and form the folding alcove (10) together with the alcove wall. The folding connections can be folded out into the inner space (4) of the sanitary space (1) so that the alcove wall can be moved into the inner space (4) of the sanitary module (1) to create a folded-out state of the folding alcove (10) in such a way that an alcove (8) is formed in the outer wall (11) of the sanitary module (1) by the alcove wall and the folding connections. The folding connections can be folded in to create a folded-in state of the folding alcove (10) in such a way that the alcove wall is in contact with the side wall (2). The present invention further provides an aircraft door region (9) comprising a sanitary module (1) of this type.
摘要翻译： 本发明提供一种卫生模块（1），包括用于在飞行器（100）的折叠凹室（10）。 卫生模块（1）包括一个侧壁（2）形成所述卫生模块（1）的外壁（11）的固定垂直部分; 到凹室构成卫生模块（1）和所述外壁（11）的可动竖直部分可以移动到模块到卫生（1）的内部空间（4）的壁; 和两个折叠连接，其中每个凹穴壁的垂直纵向边缘连接到所述侧壁（2）的垂直纵向边缘，并与凹穴壁一起形成折叠凹室（10）。 折叠连接可折出到卫生空间的内部空间（4）（1）象凹穴壁可以移动到内部空间（4）卫生模块（1）来创建一个折出状态 在寻求一种方法来做到壁龛折叠凹室（10）（8）在卫生模块（1）由凹室壁和折叠连接的外壁（11）形成。 折叠连接可以折叠在创建一个在寻求一种方式并凹穴壁折叠在折叠壁龛（10）的状态是在与侧壁（2）接触。 本发明进一步提供了在包括这种类型的：（1）卫生模块飞机门区域（9）。
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公开(公告)号：EP2238030A2
公开(公告)日：2010-10-13
申请号：EP09705585.9
申请日：2009-01-15
发明人： GONNSEN, Johannes , GÄRTNER, Jens
IPC分类号： B64D11/06
CPC分类号： B64D11/00 , B64D11/00155 , B64D11/06 , B64D11/0601 , B64D11/064
摘要： According to an exemplary embodiment of the invention, a system for the simultaneous longitudinal movement of a plurality of selected seats or seat rows in an airplane is provided, a drive device being provided to move the seats, wherein the movement of the seats is done according to a change in a seating space configuration plan.
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公开(公告)号：EP3304359A1
公开(公告)日：2018-04-11
申请号：EP16726312.8
申请日：2016-06-01
IPC分类号： G06F17/50
CPC分类号： B64F5/10 , B33Y50/00 , G05B19/4099 , G05B2219/35134 , G05B2219/49007 , G06F17/5095 , G06F2217/02 , G06F2217/06 , G06F2217/12
摘要： The invention relates to a component design system (1) for generating aircraft component designs. The component design system (1) comprises a data base (10) comprising a set of rules (11) representative for different load characteristics of different component geometries. The component design system (1) further comprises an input module (20) for inputting user-specific load characteristics (21) relating to an aircraft component (41) to be generated and a processing unit (30) for determining a variety of geometrically different aircraft component designs (31) based on the input user-specific load characteristics (21) and the set of rules (11). The invention also relates to an aircraft assembly system comprising a component design system (1), a method for generating aircraft component designs, a program element and a computer-readable medium.
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5.发明公开VERFAHREN ZUM VERLEGEN EINES BODENBELAGS IN EINER KABINE EINES FAHRZEUGS 有权EERER KABINE EINES FAHRZEUGS VERFAHREN ZUM VERLEGEN EINES BODENBELAGS
公开(公告)号：EP2349843A2
公开(公告)日：2011-08-03
申请号：EP09759731.4
申请日：2009-11-24
发明人： GONNSEN, Johannes
CPC分类号： B64D11/00 , A47G27/0437 , B60N3/046 , B64F5/10 , Y10T156/10
摘要： A method for laying a floor covering (2) onto a floor in a cabin of a vehicle comprises the steps of applying a connection means (8, 10) to an element of a group comprising the floor covering (2) and a floor, compacting the floor covering (2) into a compact unit having an open end (14), bringing the floor covering (2) into the cabin, pulling the open end (14) of the floor covering (2) along a length of the cabin beneath seats disposed in the cabin on the cabin floor and connecting the floor covering (2) to the cabin floor using the connection means (8, 10). The connection is made by way of one or more adhesive layers (8, 10), for example. In this way, a carpet floor can be laid or replaced in a cabin of a vehicle without having to remove the seats located in the cabin.
摘要翻译： 一种将地板覆盖物铺设在车辆的舱室中的地板上的方法包括以下步骤：将连接装置施加到包括地板覆盖物和地板的组的元件上，将地板覆盖物压实成具有开口端的紧凑单元 将地板覆盖物带入舱室中，沿着位于舱室底板上的舱内的座舱下方的一段长度将地板覆盖物的开口端拉出，并使用连接装置将地板覆盖物连接到舱室底板。 例如，通过一个或多个粘合剂层进行连接。 以这种方式，可以在车辆的客舱中铺设或更换地毯，而不必去除位于机舱中的座椅。
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6.发明授权ARRANGEMENT OF LINE CONNECTIONS FOR INSTALLATIONS IN AN AIRCRAFT PASSENGER CABIN 有权线的连接安排IN A平面客舱植物
公开(公告)号：EP1848631B1
公开(公告)日：2010-09-29
申请号：EP06706946.8
申请日：2006-02-14
发明人： GONNSEN, Johannes , FOKKEN, Markus , DUPONT, Michael , HARRIEHAUSEN, Michael , LEHMANN, Lars , SCHEEL, Marc , REPP, Stefan
CPC分类号： B64D11/00 , B64D11/02 , B64D11/04 , Y10T137/6906
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7.发明公开
公开(公告)号：EP3362922A1
公开(公告)日：2018-08-22
申请号：EP16788460.0
申请日：2016-10-12
申请人： Airbus Operations GmbH , Airbus SAS
发明人： GONNSEN, Johannes , THIEME, Thomas
CPC分类号： G06F17/5095 , G06F2217/02 , G06F2217/06 , G06F2217/12 , Y02P90/265
摘要： Disclosed here is a component configurator that generates variants of an aircraft component to be installed. The component configurator includes a detection unit that detects a characteristic of the component, and that determines an available free space for an installation of the component in an installation environment. The available free space is defined by a geometry of the component and/or is dependent on a moving space required by a user. The detection unit is configured to generate geometrically different variants of the component based on the free space available for the installation of the component in the installation environment. The disclosed subject matter further relates to a method for generating variants of an aircraft component to be installed, a program element as well as a computer readable medium on which a program element is stored.
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公开(公告)号：EP3304360A1
公开(公告)日：2018-04-11
申请号：EP16727445.5
申请日：2016-06-01
CPC分类号： G06F17/5095 , B64F5/00 , G06F2217/02 , G06Q10/06 , G06Q50/04
摘要： Aircraft assembly system (100), comprising an input module (101), a database (102) and a processing unit (103). The input module (101) is adapted for inputting customer-specific data and, in particular, parameters which relate to the expected time of delivery, the number of personnel working in the aircraft assembly system or an apparatus of the system which cannot be used. By applying description logics, the processing unit (103) generates a manufacturing plan in accordance with a set of rules and the input parameters. In order to improve the manufacturing plan, input parameters may be changed by the system in an iterative process. This may provide for an efficient use of resources available.
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公开(公告)号：EP2905226A1
公开(公告)日：2015-08-12
申请号：EP15153507.7
申请日：2015-02-02
CPC分类号： B64D11/064 , B60N2/22 , B60N2/643 , B60N2/686 , B64D11/0649 , Y02T50/46
摘要： Stated is a passenger seat (10) for an aircraft (110), which passenger seat (10) comprises a seat pan (12) for providing a seat surface (14) for a passenger, and a backrest (16) with a lean-against surface (18) for leaning against, and a rear surface (20) situated opposite the lean-against surface (18). In this design the rear surface (20) comprises two indentations (66a, 66b), with each of them designed to at least partially accommodate a knee (68a, 68b) of a further passenger (70) seated behind the passenger.
摘要翻译： 具有用于飞行器（110）的乘客座椅（10），所述乘客座椅（10）包括用于为乘客提供座位表面（14）的座椅盘（12）和具有贫 - 和用于倾斜的表面（18），以及与所述倾斜表面（18）相对的后表面（20）。 在该设计中，后表面（20）包括两个压痕（66a，66b），其中每一个被设计成至少部分地容纳坐在乘客后面的另外的乘客（70）的膝盖（68a，68b）。
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公开(公告)号：EP3359940A1
公开(公告)日：2018-08-15
申请号：EP16778045.1
申请日：2016-10-07
CPC分类号： G01M1/127 , B64D9/00 , B64D11/00 , B64D11/02 , B64D11/04 , B64D11/06 , G06F17/5095 , Y02T50/46
摘要： An aircraft reconfigurator system reconfigures a predetermined aircraft configuration, in particular a cabin layout, for which a distance between a position of a center of gravity of the aircraft, the center of gravity being optimized with respect to aerodynamic characteristics, and the actual position of the center of gravity is determined and thereupon an element of the aircraft is selectively displaced such that the position of the center of gravity is approximated to the optimized position of the center of gravity. Afterwards, a new aircraft configuration, in which the selected element is arranged in the new position, is determined. By means of the reconfiguration of the aircraft it is possible to save fuel.
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