-
公开(公告)号：US20120138744A1
公开(公告)日：2012-06-07
申请号：US13304634
申请日：2011-11-26
申请人： James A. Fullerton , Scott E. Coburn , R. Klaus Brauer , Blake Emery , Sebastian Petry , Jeffrey Bernett , Don Chadwick , David Wykes
发明人： James A. Fullerton , Scott E. Coburn , R. Klaus Brauer , Blake Emery , Sebastian Petry , Jeffrey Bernett , Don Chadwick , David Wykes
CPC分类号： B64D11/0649 , B60N2/7011 , B64D11/06 , B64D11/0647 , Y02T50/46 , Y10T29/48 , Y10T29/49826
摘要： An aircraft passenger seat assembly as described herein is formed from two primary and modular components: a structural frame that provides passenger support and dynamic load paths for the seat assembly; and a comfort frame that provides the passenger seating surface and the external upholstery layer for the seat assembly. If the seat assembly is designed for multiple passengers, then a separate comfort frame is used for each passenger seat location. The structural frame can be formed as a molded composite construction, and the comfort frame can also utilize a molded composite support frame. The support frame is used as a mounting shell for a fabric carrier that includes the external upholstery layer. The modular design and use of composite materials results in a significant weight and parts count savings relative to conventional seat designs.
摘要翻译： 如本文所述的飞机乘客座椅组件由两个主要和模块化部件形成：为座椅组件提供乘客支撑和动态载荷路径的结构框架; 以及提供乘客座椅表面和用于座椅组件的外部装饰层的舒适框架。 如果座椅组件是为多个乘客设计的，则每个乘客座椅位置使用单独的舒适框架。 结构框架可以形成为模制复合结构，并且舒适框架还可以利用模制的复合支撑框架。 支撑框架用作包括外部装饰层的织物载体的安装壳体。 复合材料的模块化设计和使用相对于传统的座椅设计，节省了大量的重量和零件数量。
-
公开(公告)号：USD617254S1
公开(公告)日：2010-06-08
申请号：US29202347
申请日：2004-03-30
申请人： Peter S. Guard , R. Klaus Brauer , Paul Mikulencak
设计人： Peter S. Guard , R. Klaus Brauer , Paul Mikulencak
-
公开(公告)号：USD606923S1
公开(公告)日：2009-12-29
申请号：US29192055
申请日：2003-10-17
-
公开(公告)号：US07516919B2
公开(公告)日：2009-04-14
申请号：US11865644
申请日：2007-10-01
IPC分类号： B64C1/10
CPC分类号： B64D11/00 , B64C1/066 , B64D11/0023 , B64D11/02 , B64D11/0691 , B64D2011/0046
摘要： An architectural archway for an aircraft. The archways can be positioned individually, or in pairs or other sets along the length of an aircraft fuselage. The archways are used to run or connect various transport elements, such as electrical wiring, water lines, and environmental control system conduits, between the upper crown, lower bay and passenger cabin of the aircraft. The invention simplifies installation complexity and eliminates the installation and variability associated with running transport elements between the various sections of the aircraft.
摘要翻译： 一架飞机的建筑拱门。 拱门可以沿飞机机身的长度单独定位或成对安装。 拱门用于在飞机的上冠，下托架和客舱之间运行或连接各种运输元件，例如电线，水线和环境控制系统导管。 本发明简化了安装复杂性，并消除了与飞机各部分之间的运输元件运行相关联的安装和变化。
-
公开(公告)号：US07252267B2
公开(公告)日：2007-08-07
申请号：US10688624
申请日：2003-10-17
IPC分类号： B64D11/00
CPC分类号： B64D11/00 , B64C1/066 , B64D11/0023 , B64D11/02 , B64D11/0691 , B64D2011/0046
摘要： An architectural archway for an aircraft. The archways can be positioned individually, or in pairs or other sets along the length of an aircraft fuselage. The archways are used to run or connect various transport elements, such as electrical wiring, water lines, and environmental control system conduits, between the upper crown, lower bay and passenger cabin of the aircraft. The invention simplifies installation complexity and eliminates the installation and variability associated with running transport elements between the various sections of the aircraft.
摘要翻译： 一架飞机的建筑拱门。 拱门可以沿飞机机身的长度单独定位或成对安装。 拱门用于在飞机的上冠，下托架和客舱之间运行或连接各种运输元件，例如电线，水线和环境控制系统导管。 本发明简化了安装复杂性，并消除了与飞机各部分之间的运输元件运行相关联的安装和变化。
-
公开(公告)号：USD533129S1
公开(公告)日：2006-12-05
申请号：US29202429
申请日：2004-03-30
申请人： Peter S. Guard , R. Klaus Brauer , David A. Young
设计人： Peter S. Guard , R. Klaus Brauer , David A. Young
-
公开(公告)号：US06874731B1
公开(公告)日：2005-04-05
申请号：US10703797
申请日：2003-11-07
IPC分类号： B64D11/00
CPC分类号： B64D11/003 , Y02T50/46
摘要： A modular overhead stowage bin system has an outboard bin support and a center bin support coupleable to the fuselage. First and second stowage bin modules having different storage capacities are connectable to the outboard and center bin supports in first and second configurations. In a first configuration, the first and second stowage bin modules are coupled to the fuselage and have a first overhead aisle therebetween with first opposing edge portions. The first and second stowage bin modules in the second configuration are coupled to the fuselage and have a second overhead aisle therebetween. The second overhead aisle has second opposing edge portions each shifted laterally relative to the position of the first opposing edge portions of the first overhead aisle when the first and second stowage bin modules are in the first configuration.
摘要翻译： 模块化的高架货架系统具有舷外箱支架和可与机身相连的中央仓支架。 具有不同存储容量的第一和第二存储箱模块可连接到第一和第二配置中的外侧和中心仓支架。 在第一配置中，第一和第二储物箱模块联接到机身，并且在其间具有第一相对边缘部分的第一架空通道。 第二配置中的第一和第二存储箱模块耦合到机身并且在它们之间具有第二架空通道。 当第一和第二收纳箱模块处于第一配置时，第二架空通道具有相对于第一架空通道的第一相对边缘部分的位置横向偏移的第二相对边缘部分。
-
公开(公告)号：US07871039B2
公开(公告)日：2011-01-18
申请号：US11840208
申请日：2007-08-16
申请人： James A. Fullerton , Scott E. Coburn , R. Klaus-Brauer , Blake Emery , Sebastian Petry , Jeffrey Bernett , Don Chadwick , David Wykes
发明人： James A. Fullerton , Scott E. Coburn , R. Klaus-Brauer , Blake Emery , Sebastian Petry , Jeffrey Bernett , Don Chadwick , David Wykes
IPC分类号： B64D11/00
CPC分类号： B64D11/0649 , B60N2/7011 , B64D11/06 , B64D11/0647 , Y02T50/46 , Y10T29/48 , Y10T29/49826
摘要： An aircraft passenger seat assembly as described herein is formed from two primary and modular components: a structural frame that provides passenger support and dynamic load paths for the seat assembly; and a comfort frame that provides the passenger seating surface and the external upholstery layer for the seat assembly. If the seat assembly is designed for multiple passengers, then a separate comfort frame is used for each passenger seat location. The structural frame can be formed as a molded composite construction, and the comfort frame can also utilize a molded composite support frame. The support frame is used as a mounting shell for a fabric carrier that includes the external upholstery layer. The modular design and use of composite materials results in a significant weight and parts count savings relative to conventional seat designs.
摘要翻译： 如本文所述的飞机乘客座椅组件由两个主要和模块化部件形成：为座椅组件提供乘客支撑和动态载荷路径的结构框架; 以及提供乘客座椅表面和用于座椅组件的外部装饰层的舒适框架。 如果座椅组件是为多个乘客设计的，则每个乘客座椅位置使用单独的舒适框架。 结构框架可以形成为模制复合结构，并且舒适框架还可以利用模制的复合支撑框架。 支撑框架用作包括外部装饰层的织物载体的安装壳体。 复合材料的模块化设计和使用相对于传统的座椅设计，节省了大量的重量和零件数量。
-
公开(公告)号：US07469860B2
公开(公告)日：2008-12-30
申请号：US11763194
申请日：2007-06-14
IPC分类号： B64D13/00
CPC分类号： B64D11/00 , B64C1/066 , B64D11/0023 , B64D11/02 , B64D11/0691 , B64D2011/0046
摘要： An architectural archway for an aircraft. The archways can be positioned individually, or in pairs or other sets along the length of an aircraft fuselage. The archways are used to run or connect various transport elements, such as electrical wiring, water lines, and environmental control system conduits, between the upper crown, lower bay and passenger cabin of the aircraft. The invention simplifies installation complexity and eliminates the installation and variability associated with running transport elements between the various sections of the aircraft.
摘要翻译： 一架飞机的建筑拱门。 拱门可以沿飞机机身的长度单独定位或成对安装。 拱门用于在飞机的上冠，下托架和客舱之间运行或连接各种运输元件，例如电线，水线和环境控制系统导管。 本发明简化了安装复杂性，并消除了与飞机各部分之间的运输元件运行相关联的安装和变化。
-
公开(公告)号：US20080290715A1
公开(公告)日：2008-11-27
申请号：US11840208
申请日：2007-08-16
申请人： James A. Fullerton , Scott E. Coburn , R. Klaus Brauer , Blake Emery , Sebastian Petry , Jeffrey Bernett , Don Chadwick , David Wykes
发明人： James A. Fullerton , Scott E. Coburn , R. Klaus Brauer , Blake Emery , Sebastian Petry , Jeffrey Bernett , Don Chadwick , David Wykes
IPC分类号： B64D11/06
CPC分类号： B64D11/0649 , B60N2/7011 , B64D11/06 , B64D11/0647 , Y02T50/46 , Y10T29/48 , Y10T29/49826
摘要： An aircraft passenger seat assembly as described herein is formed from two primary and modular components: a structural frame that provides passenger support and dynamic load paths for the seat assembly; and a comfort frame that provides the passenger seating surface and the external upholstery layer for the seat assembly. If the seat assembly is designed for multiple passengers, then a separate comfort frame is used for each passenger seat location. The structural frame can be formed as a molded composite construction, and the comfort frame can also utilize a molded composite support frame. The support frame is used as a mounting shell for a fabric carrier that includes the external upholstery layer. The modular design and use of composite materials results in a significant weight and parts count savings relative to conventional seat designs.
摘要翻译： 如本文所述的飞机乘客座椅组件由两个主要和模块化部件形成：为座椅组件提供乘客支撑和动态载荷路径的结构框架; 以及提供乘客座椅表面和用于座椅组件的外部装饰层的舒适框架。 如果座椅组件是为多个乘客设计的，则每个乘客座椅位置使用单独的舒适框架。 结构框架可以形成为模制复合结构，并且舒适框架还可以利用模制的复合支撑框架。 支撑框架用作包括外部装饰层的织物载体的安装壳体。 复合材料的模块化设计和使用相对于传统的座椅设计，节省了大量的重量和零件数量。
-
-
-
-
-
-
-
-
-
搜索结果
25 条记录 (耗时 0.024 秒)