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1. 发明授权

US5975464A Aircraft with removable structural payload module 失效
标题翻译：具有可移动结构有效载荷模块的飞机
公开(公告)号：US5975464A
公开(公告)日：1999-11-02
申请号：US158186
申请日：1998-09-22
申请人： Elbert Rutan
发明人： Elbert Rutan
IPC分类号： B64C39/02 , B64C1/00
CPC分类号： B64C39/02
摘要： An aircraft includes a forward fuselage segment, an aft fuselage segment, a wing structure supported from the aft fuselage segment, a tail structure supported from either the aft fuselage segment or the wing structure, and an engine supported from either the aft fuselage segment or the wing structure. A payload module is disposed between and connects the forward fuselage segment and the aft fuselage segment, so as to form the structural attachment between the forward fuselage segment and the aft fuselage segment. The payload module is disconnectable from the forward fuselage segment and the aft fuselage segment such that the forward fuselage segment and the aft fuselage segment are not connected to each other when the payload module is disconnected from the forward fuselage segment and the aft fuselage segment.
摘要翻译：飞机包括前机身段，后机身段，从后机身段支撑的机翼结构，从后机身段或机翼结构支撑的尾部结构，以及从后机身段或机翼结构。有效载荷模块设置在前机身段和后机身段之间，并连接到机身前部段和后机身段，以形成前机身段与后机身段之间的结构连接。有效载荷模块可从前机身段和后机身段断开，使得当有效载荷模块与前机身段和后机身段断开时，前机身段和后机身段都不相互连接。

2. 发明授权

US6110567A Composite structural panel having a face sheet reinforced with a channel stiffener grid 失效
标题翻译：复合结构板具有用通道加强筋网加强的面板
公开(公告)号：US6110567A
公开(公告)日：2000-08-29
申请号：US238100
申请日：1999-01-27
申请人： Cory R. Bird
发明人： Cory R. Bird
IPC分类号： B32B3/28 , E04C2/32 , B32B1/00 , E04C2/34
CPC分类号： B32B3/28 , E04C2/326 , Y10T428/24636 , Y10T428/24661 , Y10T428/24744
摘要： A composite structural panel is formed of a single composite face sheet with a stiffener grid adhesively attached to one side of the face sheet. The stiffener grid if formed of an interlocked set of parallel first elongated grid channels extending in a first direction and parallel second elongated grid channels extending in a second direction. Each grid channel is a hollow channel section including two shear walls formed of a shear wall composite material having woven bidirectional shear wall fiber reinforcement cloth embedded in a shear wall matrix, and a cap extending between the top of each of the two shear walls. The cap is formed of a cap composite material of composite material having unidirectional cap fiber reinforcement embedded in a cap matrix, with the unidirectional cap fiber reinforcement extending parallel to the direction of elongation of the grid channel.
摘要翻译：复合结构板由具有粘合地附着在面板的一侧的加强筋的单个复合面板形成。如果由在第一方向上延伸的互锁的一组平行的第一细长网格通道形成并且在第二方向上延伸的平行的第二细长栅格通道的加强栅格。每个格栅通道是一个中空的通道部分，包括由剪切壁复合材料形成的两个剪切壁，剪切壁复合材料具有嵌入在剪切壁基体中的编织双向剪切壁纤维增强布，以及在两个剪力壁各自的顶部之间延伸的盖。盖由复合材料的帽复合材料形成，其具有嵌入盖矩阵中的单向盖纤维增强物，单向盖纤维增强体平行于网格通道的延伸方向延伸。

3. 发明授权

US5863365A Method of manufacturing composite articles 失效
标题翻译：复合制品的制造方法
公开(公告)号：US5863365A
公开(公告)日：1999-01-26
申请号：US846722
申请日：1997-04-30
申请人： Cory R. Bird
发明人： Cory R. Bird
IPC分类号： B29C37/00 , B29C70/34 , B29C70/54 , B32B31/20
CPC分类号： B29C37/0064 , B29C70/345 , B29C70/547
摘要： A composite article is prepared by positioning composite material precursor between a layup tool and a sculpted block of an open-celled foam material. The block has a first face sculpted to define a first face of the composite article. A pressure is applied between the layup tool and the block, and thence to the composite material precursor. Simultaneously with the pressure application, the assembly is heated to compact and cure the composite material. The open-celled foam block acts both as a breather material to allow gas to escape from the compacting composite material and a bleeder material to receive resin that is forced out of the composite material under pressure.
摘要翻译：通过将复合材料前体放置在铺层工具和开孔泡沫材料的雕刻块之间来制备复合制品。该块具有雕刻以形成复合制品的第一面的第一面。在铺层工具和块之间施加压力，然后施加到复合材料前体上。在施加压力的同时，将组件加热以压实并固化复合材料。开孔泡沫块既可以作为通气材料，也可以使气体从压实复合材料中逸出，还可以使用泄放材料以接收在压力下被迫离开复合材料的树脂。

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