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公开(公告)号：US08732977B2
公开(公告)日：2014-05-27
申请号：US11776929
申请日：2007-07-12
申请人： Richard Adams , Peter Griggs , Glenn Watson
发明人： Richard Adams , Peter Griggs , Glenn Watson
CPC分类号： C08L63/00 , B64C1/06 , C08K3/04 , Y10T428/31511 , C08L2666/54
摘要： A method of producing a structural component comprising manufacturing a structural component from a moisture absorbable material the toughness of which increases with increasing moisture absorption and subsequently subjecting the structural component to at least one of elevated temperature and humidity for a period of time such that the structural component attains a predetermined moisture content and distribution.
摘要翻译： 一种制造结构部件的方法，包括从吸湿材料制造结构部件，其韧性随着吸湿性的增加而增加，随后使结构部件处于高温和高湿度中的至少一个持续一段时间，使得结构 组分达到预定的水分含量和分布。
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2.发明授权Aircraft wing cover comprising a sandwich panel and methods to manufacture and design the said wing cover 有权包括夹芯板的飞机机翼盖和用于制造和设计所述机翼盖的方法公开(公告)号：US09085350B2
公开(公告)日：2015-07-21
申请号：US13521787
申请日：2011-01-14
IPC分类号： B64C1/00 , B64C3/20 , B29C70/08 , B29C70/86 , B29C70/88 , B29D99/00 , B64C3/26 , B29K105/04 , B29L31/30 , B29L31/60
CPC分类号： B64C3/20 , B29C70/086 , B29C70/088 , B29C70/865 , B29C70/887 , B29D99/0021 , B29K2105/043 , B29L2031/3085 , B29L2031/608 , B64C3/26 , Y02T50/43 , Y10T156/1074
摘要： An aircraft wing cover (10) comprising an integrally stiffened sandwich panel including first and second skins (11, 12) sandwiching a core layer (13), wherein at least one of the skins has a plurality of spanwise extending integral regions of increased thickness (18) accommodated by corresponding regions (19) of decreased thickness in the core. Also, a method of fabricating an aircraft wing cover, and a method of designing an aircraft wing.
摘要翻译： 1.一种飞机机翼盖（10），包括整体加强的夹层板，其包括夹着芯层（13）的第一和第二表皮（11,12），其中所述表皮中的至少一个具有增加厚度的多个翼展方向延伸的整体区域 18），其由芯中的厚度减小的相应区域（19）容纳。 另外，制造飞机机翼盖的方法以及飞机机翼的设计方法。
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3.发明申请AIRCRAFT WING COVER COMPRISING A SANDWICH PANEL AND METHODS TO MANUFACTURE AND DESIGN THE SAID WING COVER 有权包含三面板的飞机盖子和制造和设计固定盖板的方法公开(公告)号：US20130099058A1
公开(公告)日：2013-04-25
申请号：US13521787
申请日：2011-01-14
IPC分类号： B64C3/20
CPC分类号： B64C3/20 , B29C70/086 , B29C70/088 , B29C70/865 , B29C70/887 , B29D99/0021 , B29K2105/043 , B29L2031/3085 , B29L2031/608 , B64C3/26 , Y02T50/43 , Y10T156/1074
摘要： An aircraft wing cover (10) comprising an integrally stiffened sandwich panel including first and second skins (11, 12) sandwiching a core layer (13), wherein at least one of the skins has a plurality of spanwise extending integral regions of increased thickness (18) accommodated by corresponding regions (19) of decreased thickness in the core. Also, a method of fabricating an aircraft wing cover, and a method of designing an aircraft wing.
摘要翻译： 1.一种飞机机翼盖（10），包括整体加强的夹层板，其包括夹着芯层（13）的第一和第二表皮（11,12），其中所述表皮中的至少一个具有增加厚度的多个翼展方向延伸的整体区域 18），其由芯中的厚度减小的相应区域（19）容纳。 另外，制造飞机机翼盖的方法以及飞机机翼的设计方法。
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4.发明申请公开(公告)号：US20060078008A1
公开(公告)日：2006-04-13
申请号：US11288381
申请日：2005-11-29
申请人： Frank Bordonaro , Amitava Das , Paul Schmidt , Glenn Watson
发明人： Frank Bordonaro , Amitava Das , Paul Schmidt , Glenn Watson
IPC分类号： H04J3/12
CPC分类号： H04L47/10 , H04L41/0893 , H04L41/0896 , H04L41/5022 , H04L43/00 , H04L43/0894 , H04L43/16 , H04L65/80 , H04Q3/0025
摘要： A signaling network node is configured for identifying a received signaling message as belonging to one of a plurality of prescribed originating node groups, based on prescribed message class selection criteria. Each originating node group has at least one originating node and is assigned at least one congestion threshold relative to a message rate (e.g., messages per unit time or number of bytes per unit time). The signaling network node determines the message rate for each corresponding originating node group; if the message rate for an originating node group exceeds the corresponding at least one congestion threshold, the signaling network node outputs a congestion signaling message to the originating node having sent the signaling message, for reduction of the corresponding message rate.
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