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公开(公告)号：US20110024565A1
公开(公告)日：2011-02-03
申请号：US12739023
申请日：2008-10-22
CPC分类号： B64C1/068 , B64C1/066 , B64D2011/0046 , Y10T29/49117 , Y10T29/49826
摘要： An aircraft component assembly system (10; 10′; 10″) for the assembly of an interior component, a pipe and/or an electric line in an aircraft comprises at least one arc-shaped frame element (12; 12′; 12″), a connection element (32) that extends between a first and a second end of the frame element (12; 12′; 12″), a fastening apparatus for fastening the interior component, the pipe and/or the electric line to the frame element (12; 12′; 12″) and/or the connection element (32), and a first guide device (46) that is provided on the frame element (12; 12′; 12″) and/or the connection element (32) and is devised to interact with a second guide device (52), which is complementary to the first guide device (46) and provided on an aircraft structure (40), in such a way that the aircraft component assembly system (10; 10; 10″) is connectable to the aircraft structure (40) in a manner displaceable relative to the aircraft structure (40).
摘要翻译： 一种用于在飞行器中组装内部组件，管道和/或电线的飞行器部件组件系统（10; 10'; 10“），包括至少一个弧形框架元件（12; 12'; 12” ），在框架元件（12; 12'; 12“）的第一和第二端之间延伸的连接元件（32），用于将内部部件，管道和/或电线紧固到 框架元件（12; 12'; 12“）和/或连接元件（32）和设置在框架元件（12; 12'; 12”）上的第一引导装置（46）和/或连接 元件（32）并且被设计成与第二引导装置（52）相互作用，第二引导装置（52）与第一引导装置（46）互补并且设置在飞机结构（40）上，使得飞行器部件组装系统 10; 10“）可以以相对于飞行器结构（40）可移位的方式连接到飞行器结构（40）。
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2.发明申请Frame element, aircraft component assembly system and method of fitting a component in an aircraft 有权框架元件，飞机部件组装系统以及在飞行器中安装部件的方法公开(公告)号：US20090272849A1
公开(公告)日：2009-11-05
申请号：US12380074
申请日：2009-02-23
CPC分类号： B64C1/066 , B64C1/40 , Y10T29/49904
摘要： A frame element (10; 10′) for use in an aircraft component assembly system (46) is attachable to an aircraft structure (36) and comprises at least one fastening device for fastening at least one aircraft interior component (34) or at least one insulation pack (52) to the frame element (10; 10′). An aircraft component assembly system (46) comprises a plurality of such frame elements (10; 10′). In a method of fitting a component (34, 52) in an aircraft, a frame element (10; 10′) is provided. At least one interior component (34) or at least one insulation pack (52) is fastened to the frame element (10; 10′). Then the frame element (10; 10′) having the at least one interior component (34) or the at least one insulation pack (52) fastened thereto is attached to an aircraft structure (36).
摘要翻译： 用于飞行器部件组装系统（46）的框架元件（10; 10'）可附接到飞机结构（36），并且包括用于紧固至少一个飞行器内部部件（34）或至少 一个绝缘包（52）连接到所述框架元件（10; 10'）。 飞机部件组装系统（46）包括多个这样的框架元件（10; 10'）。 在一种将部件（34,52）装配在飞行器中的方法中，提供了一个框架元件（10; 10'）。 至少一个内部部件（34）或至少一个绝缘包（52）被紧固到所述框架元件（10; 10'）。 然后，具有固定到其上的至少一个内部部件（34）或至少一个绝缘包装（52）的框架元件（10; 10'）附接到飞行器结构（36）。
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3.发明授权Frame element, storage bin and method for installing a storage bin in an aircraft 有权框架元件，存储箱和在飞机上安装存储箱的方法公开(公告)号：US08226033B2
公开(公告)日：2012-07-24
申请号：US12380066
申请日：2009-02-23
IPC分类号： B64D11/00
CPC分类号： B64D11/003 , B64C1/066 , B64C1/40 , Y10T29/49826
摘要： A frame element (10) for use in an aircraft component installation system (46) is attachable to an aircraft structure (36) and comprises a storage bin fastening device which is designed to fasten a storage bin (26) at various positions on the frame element (10). A storage bin (26) for use in an aircraft comprises a complementary device to the storage bin fastening device of the frame element (10), in order to fasten the storage bin (26) at various positions on the frame element (10). In a method for the installation of a storage bin (26) in an aircraft a frame element (10) is provided. A storage bin (26) is fastened in a desired position on the frame element (10). The frame element (10) is attached to an aircraft structure (36).
摘要翻译： 用于飞行器部件安装系统（46）的框架元件（10）可附接到飞行器结构（36）并且包括存储箱紧固装置，其被设计成将存放箱（26）固定在框架上的各个位置 元件（10）。 用于飞行器的存储箱（26）包括与框架元件（10）的存储箱紧固装置的互补装置，以便将存储箱（26）紧固在框架元件（10）上的各个位置。 在用于在飞行器中安装存储箱（26）的方法中，提供了一个框架元件（10）。 存储箱（26）被固定在框架元件（10）上的期望位置。 框架元件（10）附接到飞行器结构（36）。
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4.发明授权Frame element, aircraft component assembly system and method of fitting a component in an aircraft 有权框架元件，飞机部件组装系统以及在飞行器中安装部件的方法公开(公告)号：US09340273B2
公开(公告)日：2016-05-17
申请号：US12380074
申请日：2009-02-23
CPC分类号： B64C1/066 , B64C1/40 , Y10T29/49904
摘要： A frame element (10; 10′) for use in an aircraft component assembly system (46) is attachable to an aircraft structure (36) and comprises at least one fastening device for fastening at least one aircraft interior component (34) or at least one insulation pack (52) to the frame element (10; 10′). An aircraft component assembly system (46) comprises a plurality of such frame elements (10; 10′). In a method of fitting a component (34, 52) in an aircraft, a frame element (10; 10′) is provided. At least one interior component (34) or at least one insulation pack (52) is fastened to the frame element (10; 10′). Then the frame element (10; 10′) having the at least one interior component (34) or the at least one insulation pack (52) fastened thereto is attached to an aircraft structure (36).
摘要翻译： 用于飞行器部件组装系统（46）的框架元件（10; 10'）可附接到飞机结构（36），并且包括用于紧固至少一个飞行器内部部件（34）或至少 一个绝缘包（52）连接到所述框架元件（10; 10'）。 飞机部件组装系统（46）包括多个这样的框架元件（10; 10'）。 在一种将部件（34,52）装配在飞行器中的方法中，提供了一个框架元件（10; 10'）。 至少一个内部部件（34）或至少一个绝缘包（52）被紧固到所述框架元件（10; 10'）。 然后，具有固定到其上的至少一个内部部件（34）或至少一个绝缘包装（52）的框架元件（10; 10'）附接到飞行器结构（36）。
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公开(公告)号：US08474758B2
公开(公告)日：2013-07-02
申请号：US12739023
申请日：2008-10-22
CPC分类号： B64C1/068 , B64C1/066 , B64D2011/0046 , Y10T29/49117 , Y10T29/49826
摘要： An aircraft component assembly system for the assembly of an interior component, a pipe or an electric line in an aircraft includes at least one arc-shaped frame element, a connection element that extends between a first and a second end of the frame element, and a fastening apparatus for fastening the interior component, the pipe or the electric line to the frame element or the connection element. The system also includes a first guide device that is provided on the frame element or the connection element and is devised to interact with a second guide device, which is complementary to the first guide device and provided on an aircraft structure, in such a way that the aircraft component assembly system is connectable to the aircraft structure in a manner displaceable relative to the aircraft structure.
摘要翻译： 一种用于在飞行器中组装内部部件，管道或电线的飞行器部件组装系统，包括至少一个弧形框架元件，在框架元件的第一和第二端之间延伸的连接元件，以及 用于将内部部件，管子或电线紧固到框架元件或连接元件的紧固装置。 该系统还包括设置在框架元件或连接元件上并且被设计成与第二引导装置相互作用的第一引导装置，第二引导装置与第一引导装置互补并且设置在飞行器结构上，使得 飞机部件组装系统可以以相对于飞行器结构可移位的方式连接到飞行器结构。
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6.发明申请Frame element, storage bin and method for installing a storage bin in an aircraft 有权框架元件，存储箱和在飞机上安装存储箱的方法公开(公告)号：US20090230244A1
公开(公告)日：2009-09-17
申请号：US12380066
申请日：2009-02-23
CPC分类号： B64D11/003 , B64C1/066 , B64C1/40 , Y10T29/49826
摘要： A frame element (10) for use in an aircraft component installation system (46) is attachable to an aircraft structure (36) and comprises a storage bin fastening device which is designed to fasten a storage bin (26) at various positions on the frame element (10). A storage bin (26) for use in an aircraft comprises a complementary device to the storage bin fastening device of the frame element (10), in order to fasten the storage bin (26) at various positions on the frame element (10). In a method for the installation of a storage bin (26) in an aircraft a frame element (10) is provided. A storage bin (26) is fastened in a desired position on the frame element (10). The frame element (10) is attached to an aircraft structure (36).
摘要翻译： 用于飞行器部件安装系统（46）的框架元件（10）可附接到飞行器结构（36）并且包括存储箱紧固装置，其被设计成将存放箱（26）固定在框架上的各个位置 元件（10）。 用于飞行器的存储箱（26）包括与框架元件（10）的存储箱紧固装置的互补装置，以便将存储箱（26）紧固在框架元件（10）上的各个位置。 在用于在飞行器中安装存储箱（26）的方法中，提供了一个框架元件（10）。 存储箱（26）被固定在框架元件（10）上的期望位置。 框架元件（10）附接到飞行器结构（36）。
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公开(公告)号：US08262023B2
公开(公告)日：2012-09-11
申请号：US12438036
申请日：2007-08-17
IPC分类号： B64C1/00
CPC分类号： B64C1/066 , B64C1/40 , B64D13/00 , Y10T29/49622
摘要： A frame element for use in an aircraft air-conditioning system is attachable to an aircraft structure and includes at least one strut which is formed to at least in sections as a hollow cylinder, wherein an air inlet connection of the at least one-section-wise hollow cylindrically formed strut of the frame element is connectable to an air outlet duct of an aircraft air-conditioning unit, and an air outlet connection of the at least one section-wise hollow cylindrically formed strut of the frame element is connectable to an air outlet opening terminating in a cabin region of an aircraft.
摘要翻译： 用于飞行器空调系统的框架元件可附接到飞行器结构，并且包括至少一个至少部分地形成为中空圆柱体的支柱，其中至少一个截面形状的空气入口连接， 框架元件的明智的中空圆柱形支柱可连接到飞行器空调单元的空气出口管道，并且框架元件的至少一个截面中空圆柱形的支柱的空气出口连接可连接到空气 出口开口终止于飞机的舱区域。
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8.发明申请FRAME ELEMENT, AIRCRAFT AIR-CONDITIONING SYSTEM AND METHOD FOR THE INSTALLATION OF A FRAME ELEMENT IN AN AIRCRAFT 有权框架元件，飞机空调系统和安装飞机中的框架元件的方法公开(公告)号：US20110024561A1
公开(公告)日：2011-02-03
申请号：US12438036
申请日：2007-08-17
CPC分类号： B64C1/066 , B64C1/40 , B64D13/00 , Y10T29/49622
摘要： A frame element (10; 10′) for use in an aircraft air-conditioning system is attachable to an aircraft structure (36) and includes at least one strut (12, 14, 16, 18; 12′, 14′, 16′) which is formed at least in sections as a hollow cylinder, wherein an air inlet connection (12a, 14a; 12a′, 14a′) of the at least one section-wise hollow cylindrically formed strut (12, 14, 16, 18; 12′, 14′, 16′) of the frame element (10; 100 is connectable to an air outlet duct of an aircraft air-conditioning unit, and an air outlet connection (12b, 14b; 12b′, 14b′) of the at least one section-wise hollow cylindrically formed strut (12, 14, 16, 18; 12′, 14′, 16′) of the frame element (10; 100 is connectable to an air outlet opening terminating in a cabin region of an aircraft.
摘要翻译： 用于飞机空调系统的框架元件（10; 10'）可附接到飞行器结构（36），并且包括至少一个支柱（12,14,16,18,22'，14'，16' ），其至少形成为中空圆柱体，其中所述至少一个截面中空圆柱形支柱（12,14,16,18; 18）的空气入口连接件（12a，14a; 12a'，14a' 框架元件（10; 100可连接到飞行器空调单元的空气出口管道）和空气出口连接件（12b，14b; 12b'，14b'）的12'，14'，16' 框架元件（10; 100）的至少一个截面中空圆柱形的支柱（12,14,16,18; 12'，14'，16'）可连接到终止于 飞机。
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9.发明申请公开(公告)号：US20100152883A1
公开(公告)日：2010-06-17
申请号：US12638474
申请日：2009-12-15
IPC分类号： G06F17/00
CPC分类号： B65G1/02 , B65C9/0062 , B65C9/40 , B65G43/00
摘要： An apparatus and a method for controlling an apparatus for furnishing articles is disclosed. A conveyor unit is used to convey the articles. At least one exchangeable furnishing unit is designed to exchange identification data and/or control information during connection to the apparatus with the apparatus and/or with the conveyor unit. At least one storage area is provided, wherein the storage area stores at least two furnishing units. An automatically controlled feeding and withdrawing unit is used to operatively connect the storage area with the apparatus.
摘要翻译： 公开了一种用于控制用于制造物品的装置的装置和方法。 传送单元用于传送物品。 至少一个可更换的装置单元被设计成在与设备和/或与传送单元连接到设备期间交换识别数据和/或控制信息。 提供至少一个存储区域，其中存储区域存储至少两个家具单元。 使用自动控制的进给和取出单元将存储区域与设备连接起来。
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公开(公告)号：US08882044B2
公开(公告)日：2014-11-11
申请号：US12532343
申请日：2008-03-25
申请人： Thomas Bock , Michael Auburger , Patrique Doemeland , Brigitte Gerner , Florian Schuephaus , Silvan Fiedler
发明人： Thomas Bock , Michael Auburger , Patrique Doemeland , Brigitte Gerner , Florian Schuephaus , Silvan Fiedler
CPC分类号： B64C1/066
摘要： A gap covering device for covering a gap between two mutually adjacent first aircraft interior panels includes a visible portion as well as a retaining portion connected to the visible portion and extending opposite the visible portion. A receiving structure is fastened to an inner surface of the visible portion and/or of the retaining portion and has a receiving contour adapted to an edge contour of the first aircraft interior panels.
摘要翻译： 用于覆盖两个相互相邻的第一飞行器内部面板之间的间隙的间隙覆盖装置包括可见部分以及连接到可见部分并且与可见部分相对延伸的保持部分。 接收结构紧固到可见部分和/或保持部分的内表面，并且具有适于第一飞机内部面板的边缘轮廓的接收轮廓。
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