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公开(公告)号:USD711305S1
公开(公告)日:2014-08-19
申请号:US29418287
申请日:2012-04-13
申请人: Christopher Pirie , Sebastian Petry , Michael Kemery , Aaron Hawkins , Erik Nilsen , Eddie Goh
设计人: Christopher Pirie , Sebastian Petry , Michael Kemery , Aaron Hawkins , Erik Nilsen , Eddie Goh
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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。
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公开(公告)号:US09555891B2
公开(公告)日:2017-01-31
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。
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公开(公告)号:US08087613B2
公开(公告)日:2012-01-03
申请号:US12960855
申请日:2010-12-06
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。
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公开(公告)号:US20110101165A1
公开(公告)日:2011-05-05
申请号:US12960855
申请日:2010-12-06
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。
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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。
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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。
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