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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：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：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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公开(公告)号：US5118053A
公开(公告)日：1992-06-02
申请号：US413330
申请日：1989-09-27
申请人： Ashok K. Singh , Scott E. Coburn
发明人： Ashok K. Singh , Scott E. Coburn
IPC分类号： B64C1/18
CPC分类号： B64C1/18 , B64C2001/009
摘要： A system for preventing the sudden depressurization of a compartment in an aircraft from causing structural damage or damage to other critical aircraft components. The system includes a pivotable closure. Normally, this closure is latched across a passage between a pressurized compartment such as a passenger cabin and a dump such as the space between the cabin wall and the outer skin of the aircraft. In the event that pressure is suddenly lost in a second pressurized compartment such as a cargo hold beneath the floor of the passenger compartment, a pressure differential is created across a flap-type latch actuator carried by the closure. This rotates the actuator, disengaging an actuator-associated latch element from a fixedly mounted keeper and thereby allowing the closure to be swung to an open position by outrushing air. This makes the entire area of the passage to the dump available for the outflow of air. As a consequence, the pressure between the two compartments is rapidly equalized, keeping the floor of the passenger compartment from collapsing and preventing damage to critical aircraft components routed beneath the floor or through the aircraft body such as control cables, electrical leads, and hydraulic lines.
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