公开(公告)号：EP3031723B1

公开(公告)日：2020-01-01

申请号：EP15196956.5

申请日：2015-11-30

申请人： Airbus Operations GmbH

发明人： Gonnsen, Johannes

IPC分类号： B64D11/04

公开(公告)号：EP3101565A1

公开(公告)日：2016-12-07

申请号：EP15170092.9

申请日：2015-06-01

申请人： Airbus Operations GmbH

发明人： Gonnsen, Johannes ,  Bueno Moreno, Irene

IPC分类号： G06F17/50 ,  G06Q10/06 ,  G06Q50/04

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.

摘要翻译： 飞机组装系统（100），包括输入模块（101），数据库（102）和处理单元（103）。 输入模块（101）适于输入客户特定的数据，特别是与期望的交付时间有关的参数，在飞行器组装系统中工作的人员数量或不能使用的系统的装置。 通过应用描述逻辑，处理单元（103）根据一组规则和输入参数生成制造计划。 为了改进制造计划，输入参数可以由迭代过程中的系统改变。 这可以有效地利用可用的资源。

公开(公告)号：EP3248875A1

公开(公告)日：2017-11-29

申请号：EP16171020.7

申请日：2016-05-24

申请人： Airbus Operations GmbH

发明人： Gonnsen, Johannes

IPC分类号： B64D11/06

CPC分类号： B64D11/0691 ,  B64D11/04 ,  B64D11/062 ,  B64D11/064

摘要： A flight attendant seat (10) comprises a carrier device (12) having guiding means (14) with opposed first and second (18) ends, and a storage compartment (20) within which the first end of the guiding means (14) is disposed. The guiding means (14) are adapted to provide guidance along their longitudinal extension between their first and second (18) ends. The flight attendant seat (10) further comprises a plurality of segments (22) each of which slidingly mounted to the guiding means (14) so as to allow a sliding movement of said plurality of segments (22) along the guiding means (14) and relative to the carrier device (12) between a stored position of the plurality of segments (22), in which the plurality of segments (22) is received within the storage compartment (20) of the carrier device (12), and an exposed position of the plurality of segments (22). A seat element (24) of the flight attendant seat (10) is pivotally mounted to a first segment (26) of said plurality of segments (22) so as to be pivotable between an inoperative position and an operative position in which a flight attendant may sit down on the seat element (24). At least one backrest element (28) of the flight attendant seat (10) is respectively mounted to at least one second segment (30) of said plurality of segments (22). With the plurality of segments (22) being in its exposed position, the seat element (24) when pivoted to its operative position and the at least one backrest element (28) together are adapted to be used by a flight attendant as flight attendant seat.

摘要翻译： 一种乘务员座位（10），包括具有带有相对的第一端部和第二端部（18）的引导装置（14）的承载装置（12）以及存储室（20），所述引导装置（14）的第一端部位于所述存储室 处置。 引导装置（14）适于沿它们的第一和第二端（18）之间的纵向延伸提供引导。 乘务员座位（10）还包括多个分段（22），每个分段滑动地安装到引导装置（14），以允许所述多个分段（22）沿着引导装置（14）滑动移动， （22）的储存位置与其中所述多个区段（22）被接纳在所述承载装置（12）的所述储存隔间（20）内的所述多个区段（22）的相对于所述承载装置（12） 所述多个区段（22）的暴露位置。 空乘人员座位（10）的座位元件（24）枢转地安装到所述多个段（22）的第一段（26），以便能够在非操作位置和操作位置之间枢转，其中空乘人员 可坐在座位元件（24）上。 乘务员座位（10）的至少一个靠背元件（28）分别安装到所述多个节段（22）中的至少一个第二节段（30）。 在多个节段（22）处于其暴露位置时，枢转到其操作位置时的座椅元件（24）和至少一个靠背元件（28）一起适合由空乘人员用作乘务员座椅 。

公开(公告)号：EP3248873A1

公开(公告)日：2017-11-29

申请号：EP16171140.3

申请日：2016-05-24

申请人： Airbus Operations GmbH

发明人： Gonnsen, Johannes

IPC分类号： B64D11/04 ,  B64D11/00

CPC分类号： B64D11/04 ,  B64D2011/0046

摘要： The present invention concerns an aircraft monument (100), comprising a desk (102), and a movable part (104) that is mounted to the aircraft monument (100) by means of an attachment device (106) such that the movable part (104) is pivotable about an axis (A) between a first position in which the movable part (104) covers a first area of the desk (102) and is essentially arranged inside of the aircraft monument (100) such that its front faces in a first direction towards the back of the aircraft monument (100), and a second position in which the movable part (104) is at least partially arranged outside of the aircraft monument (100) and its front faces in a second direction that crosses the first direction, wherein the movable part (104), in its second position, covers a second area of the desk (102) that is less than the first area.

摘要翻译： 本发明涉及包括桌子（102）和可移动部分（104）的飞机建造物（100），所述可移动部分通过附接装置（106）安装到飞机建造物（100），使得可移动部分 104）围绕轴线（A）在第一位置和第二位置之间枢转，在所述第一位置中，活动部件（104）覆盖桌子（102）的第一区域并且基本上布置在飞机建造物（100）内部，使得其前表面 朝向飞机构件（100）的后部的第一方向以及第二位置，在该第二位置中，可移动部件（104）至少部分地布置在飞机建造物（100）的外部并且其前部面在第二方向上穿过 第一方向，其中可移动部件（104）在其第二位置覆盖桌子（102）的小于第一区域的第二区域。

公开(公告)号：EP3101564A8

公开(公告)日：2017-02-15

申请号：EP15170090.3

申请日：2015-06-01

申请人： Airbus Operations GmbH

发明人： Gonnsen, Johannes ,  Bueno Moreno, Irene

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.

公开(公告)号：EP3023918A1

公开(公告)日：2016-05-25

申请号：EP14193916.5

申请日：2014-11-19

申请人： Airbus Operations GmbH ,  Airbus Defence and Space GmbH

发明人： Gonnsen, Johannes ,  Schubotz, René

IPC分类号： G06Q10/04 ,  G06Q10/08

CPC分类号： G06Q10/083 ,  G06Q10/04 ,  G06Q10/08

摘要： According to an exemplary embodiment of the present invention, a configuration system for calculating a feature of each element of a plurality of elements is provided. The system comprises a database in which a set of rules for each element of the plurality of elements is stored, and a processing unit which is designed to automatically vary a first feature of a first element or for automatically replacing the first element by another element, and for calculating the features of the elements in accordance with the set of rules. By allowing to automatically vary a feature of an element or by allowing automatic replacement of an element by another element, the configuration of the elements may be optimized.

摘要翻译： 根据本发明的示例性实施例，提供了一种用于计算多个元件中的每个元件的特征的配置系统。 该系统包括：数据库，其中存储有多个元素中的每个元素的一组规则;以及处理单元，其被设计为自动地改变第一元素的第一特征或者由另一元素自动替换第一元素， 并根据该组规则计算元素的特征。 通过允许自动地改变元件的特征或通过允许由另一元件自动替换元件，可以优化元件的配置。

公开(公告)号：EP3248875B1

公开(公告)日：2018-08-29

申请号：EP16171020.7

申请日：2016-05-24

申请人： Airbus Operations GmbH

发明人： Gonnsen, Johannes

IPC分类号： B64D11/06

CPC分类号： B64D11/0691 ,  B64D11/04 ,  B64D11/062 ,  B64D11/064

摘要： A flight attendant seat (10) comprises a carrier device (12) having guiding means (14) with opposed first and second (18) ends, and a storage compartment (20) within which the first end of the guiding means (14) is disposed. The guiding means (14) are adapted to provide guidance along their longitudinal extension between their first and second (18) ends. The flight attendant seat (10) further comprises a plurality of segments (22) each of which slidingly mounted to the guiding means (14) so as to allow a sliding movement of said plurality of segments (22) along the guiding means (14) and relative to the carrier device (12) between a stored position of the plurality of segments (22), in which the plurality of segments (22) is received within the storage compartment (20) of the carrier device (12), and an exposed position of the plurality of segments (22). A seat element (24) of the flight attendant seat (10) is pivotally mounted to a first segment (26) of said plurality of segments (22) so as to be pivotable between an inoperative position and an operative position in which a flight attendant may sit down on the seat element (24). At least one backrest element (28) of the flight attendant seat (10) is respectively mounted to at least one second segment (30) of said plurality of segments (22). With the plurality of segments (22) being in its exposed position, the seat element (24) when pivoted to its operative position and the at least one backrest element (28) together are adapted to be used by a flight attendant as flight attendant seat.

公开(公告)号：EP3101564A1

公开(公告)日：2016-12-07

申请号：EP15170090.3

申请日：2015-06-01

申请人： Airbus Operations GmbH

发明人： Gonnsen, Johannes

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.

摘要翻译： 本发明涉及一种用于生成飞行器部件设计的部件设计系统（1）。 组件设计系统（1）包括数据库（10），其包括代表不同组件几何形状的不同负载特性的一组规则（11）。 所述部件设计系统（1）还包括输入模块（20），用于输入与要生成的飞行器部件（41）相关的用户特定的负载特性（21）;以及处理单元（30），用于确定各种不同的几何不同 飞机部件设计（31）基于输入的用户特定的负载特性（21）和一组规则（11）。 本发明还涉及一种包括部件设计系统（1），用于生成飞行器部件设计的方法，程序元件和计算机可读介质的飞行器组装系统。

公开(公告)号：EP3248874B1

公开(公告)日：2019-07-03

申请号：EP16171429.0

申请日：2016-05-25

申请人： Airbus Operations GmbH

发明人： Gonnsen, Johannes

IPC分类号： B64D11/04

公开(公告)号：EP3101615A1

公开(公告)日：2016-12-07

申请号：EP15170088.7

申请日：2015-06-01

申请人： Airbus Operations GmbH

发明人： Gonnsen, Johannes

IPC分类号： G06Q50/04 ,  G06Q10/06 ,  G06Q10/08

CPC分类号： G06Q50/04 ,  G06Q10/06 ,  G06Q10/08 ,  Y02P90/30

摘要： Aircraft assembly system, comprising a topology and ontology generation system, which uses description logic for generating a specific aircraft design and configuration. The aircraft design and configuration can be automatically changed by the system in order to reach a different design and configuration.

摘要翻译： 飞机组装系统，包括拓扑和本体生成系统，其使用描述逻辑来产生特定的飞行器设计和配置。 飞机的设计和配置可以由系统自动更改，以达到不同的设计和配置。