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1.发明公开
公开(公告)号：EP3626452A1
公开(公告)日：2020-03-25
申请号：EP19207936.6
申请日：2017-12-21
申请人： The Boeing Company
发明人： Drexler, Jason W. , Wilde, John C. , Wang, Xiaoxi
摘要： Methods and apparatus to form venting pathways in pressure sensitive adhesives for laminate stacks are disclosed. An example method includes forming a laminate stack including a gas permeable nonwoven layer and a pressure sensitive adhesive layer, a surface of the pressure sensitive adhesive layer facing a surface of the gas permeable nonwoven layer, and processing the laminate stack such that a plurality of venting pathways are formed in the pressure sensitive adhesive layer to enable trapped gas to pass through the pressure sensitive adhesive layer.
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公开(公告)号：EP3521009A1
公开(公告)日：2019-08-07
申请号：EP19163523.4
申请日：2016-02-09
申请人： The Boeing Company
摘要： A decorative laminate including a decorative layered structure defining a first surface and a second surface opposed from the first surface, and a gas permeable layer underlying the decorative layered structure. (Fig. 1)
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公开(公告)号：EP4382310A1
公开(公告)日：2024-06-12
申请号：EP23207103.5
申请日：2023-10-31
申请人： The Boeing Company
发明人： Drexler, Jason W. , Womack, II, Lloyd Layton , Metting, Stephanie Iris , Wilde, John Christopher , Braaten, Nathan T. , Greene, Edward , Larson-Smith, Kjersta
CPC分类号： B44C1/105 , B44C1/18 , B41M5/0047 , B41M7/0081 , B41M7/009 , B44C1/1733 , B44C5/04 , B44C5/0415 , B44C5/0423
摘要： A method for digitally printing a decorative surface material is disclosed, including providing a substrate (122) to a digital printer (308), printing a print material onto a top surface (120) of the print substrate (122), and curing the print material. The method also includes applying an adhesive (108, 116, 124) to a back surface (120) of the decorative print and applying the decorative print to an interior panel (102, 118, 126, 212, 216). The print material includes a visible or variable image, or a textured surface (120). The decorative surface material may provide a decorative interior panel (102, 118, 126, 212, 216) for an aerospace vehicle, such as a wall covering. The substrate (122) may include a flame barrier material, aluminum, or fiberglass.
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5.发明公开
公开(公告)号：EP4261031A3
公开(公告)日：2023-11-01
申请号：EP23195113.8
申请日：2017-03-30
申请人： The Boeing Company
发明人： Benham, Gary , Wang, Xiaoxi , Wilde, John , Drexler, Jason W.
IPC分类号： B32B5/02 , B32B5/10 , B32B5/18 , B32B7/12 , B32B27/06 , B32B27/08 , B32B27/12 , B32B27/30 , B32B5/22 , B32B5/24 , B32B27/28 , B32B27/40 , B32B3/12
摘要： Methods and apparatus to couple a decorative layer to a core layer of a panel via a barrier layer are disclosed. An example apparatus includes a decorative layer coupled to a panel. The panel has a core layer. The example apparatus includes a barrier layer disposed between the core layer and the decorative layer. The barrier layer is to impede at least one of gas or vapor from escaping from the core layer to the decorative layer to deter the at least one of gas or vapor from exerting a pressure on the decorative layer to deter a portion of the decorative layer from separating from the panel. (Fig. 3A)
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6.发明公开
公开(公告)号：EP4261031A2
公开(公告)日：2023-10-18
申请号：EP23195113.8
申请日：2017-03-30
申请人： The Boeing Company
发明人： Benham, Gary , Wang, Xiaoxi , Wilde, John , Drexler, Jason W.
IPC分类号： B32B3/12
摘要： Methods and apparatus to couple a decorative layer to a core layer of a panel via a barrier layer are disclosed. An example apparatus includes a decorative layer coupled to a panel. The panel has a core layer. The example apparatus includes a barrier layer disposed between the core layer and the decorative layer. The barrier layer is to impede at least one of gas or vapor from escaping from the core layer to the decorative layer to deter the at least one of gas or vapor from exerting a pressure on the decorative layer to deter a portion of the decorative layer from separating from the panel. (Fig. 3A)
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公开(公告)号：EP3533608A1
公开(公告)日：2019-09-04
申请号：EP19156116.6
申请日：2019-02-08
申请人： The Boeing Company
摘要： Methods and systems according to one or more examples are provided for laminating composite materials. In one example, a method comprises receiving a first layer material and a second layer material at a nip roller assembly and laminating, by the nip roller assembly, the first and second layer material to provide a laminated composite material comprising a main portion and at least one edge portion. The method further comprises delaminating the at least one edge portion of the laminated composite material to provide a partially laminated composite material for use in manufacturing a composite product.
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8.发明公开
公开(公告)号：EP3061601A1
公开(公告)日：2016-08-31
申请号：EP16154832.6
申请日：2016-02-09
申请人： The Boeing Company
CPC分类号： B32B27/12 , B32B5/022 , B32B5/024 , B32B7/12 , B32B15/08 , B32B15/14 , B32B15/20 , B32B27/08 , B32B27/304 , B32B27/322 , B32B37/14 , B32B2262/0276 , B32B2262/101 , B32B2305/72 , B32B2307/4023 , B32B2307/724 , B32B2405/00 , B32B2451/00 , B32B2605/003 , B32B2605/18 , B64C1/066
摘要： A decorative laminate including a decorative layered structure defining a first surface and a second surface opposed from the first surface, and a gas permeable layer underlying the decorative layered structure. (Fig. 1)
摘要翻译： 一种装饰层压板，其包括限定第一表面的装饰层状结构和与第一表面相对的第二表面，以及在装饰层状结构下方的透气层。 （图。1）
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