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公开(公告)号:US20060107516A1
公开(公告)日:2006-05-25
申请号:US11051488
申请日:2005-02-04
申请人: Brian Joseph , Robert Nolte , Matthew Rowe , James Witzgall , Gregg Wolfe
发明人: Brian Joseph , Robert Nolte , Matthew Rowe , James Witzgall , Gregg Wolfe
IPC分类号: B23P13/04
CPC分类号: C22C47/00 , Y10T29/49995
摘要: The present invention provides for assemblies comprising metal matrix composite bars where the bars only intermittently have mutual contact. Minimally two bars of metal matrix composite are joined, for example by lap joints, or by the use of incorporated tabs and slots or over-lapping slots, at areas of mutual contact to form the assemblies. The metal matrix composite assemblies of the present invention may be readily assembled to provide structures, supports, or sub-assemblies, and the like, that may exhibit high strength and stiffness coupled with relatively low mass. Additionally, such assemblies may withstand exposure to elevated temperatures higher than can be tolerated by polymeric composites. Such assemblies are expected to be particularly suitable for lightweight, stiff support structures for space booms, satellite structures, mirror backings, solar panel supports, wall reinforcement, and the like.
摘要翻译: 本发明提供了包括金属基质复合棒的组件,其中棒仅间歇地具有相互接触。 最少两个金属基质复合材料棒例如通过搭接接头连接,或者通过使用结合的凸片和槽或叠合槽,在相互接触的区域处连接以形成组件。 本发明的金属基复合组件可以容易地组装以提供结构,支撑件或子组件等,其可以表现出高度和刚度以及相对较低的质量。 此外,这种组件可承受暴露于高于聚合物复合材料可耐受的升高的温度。 预期这种组件特别适用于用于空间吊杆,卫星结构,镜子背衬,太阳能电池板支撑件,墙壁加强件等的轻型,刚性支撑结构。
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公开(公告)号:US20050238868A1
公开(公告)日:2005-10-27
申请号:US11000521
申请日:2004-12-01
申请人: Brian Joseph , Douglas Merriman , Robert Nolte , Matthew Rowe
发明人: Brian Joseph , Douglas Merriman , Robert Nolte , Matthew Rowe
CPC分类号: B32B3/12 , B32B3/20 , B32B5/18 , B32B15/01 , B32B15/04 , B32B15/20 , B32B2305/024 , B32B2311/24 , C22C49/00 , C22C2204/00 , Y10T428/249927 , Y10T428/249929 , Y10T428/249971 , Y10T428/249974 , Y10T428/249986 , Y10T428/24999 , Y10T428/31678
摘要: A lightweight, high strength structure is described where a core material has a first and second metal matrix composite layer on surfaces of the core material. A sandwich type structure may be formed. The core material may be a solid material, a foam, a honeycomb structure, or may be a channeled material. The metal matrix composite layers may include fiber reinforced metal matrix composites.
摘要翻译: 描述了一种轻质的高强度结构,其中芯材在芯材表面上具有第一和第二金属基复合层。 可以形成夹层型结构。 核心材料可以是固体材料,泡沫,蜂窝结构,或者可以是沟道材料。 金属基复合层可包括纤维增强金属基复合材料。
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公开(公告)号:US07498077B2
公开(公告)日:2009-03-03
申请号:US11000521
申请日:2004-12-01
IPC分类号: B32B3/26
CPC分类号: B32B3/12 , B32B3/20 , B32B5/18 , B32B15/01 , B32B15/04 , B32B15/20 , B32B2305/024 , B32B2311/24 , C22C49/00 , C22C2204/00 , Y10T428/249927 , Y10T428/249929 , Y10T428/249971 , Y10T428/249974 , Y10T428/249986 , Y10T428/24999 , Y10T428/31678
摘要: A lightweight, high strength structure is described where a core material has a first and second metal matrix composite layer on surfaces of the core material. A sandwich type structure may be formed. The core material may be a solid material, a foam, a honeycomb structure, or may be a channeled material. The metal matrix composite layers may include fiber reinforced metal matrix composites.
摘要翻译: 描述了一种轻质的高强度结构,其中芯材在芯材表面上具有第一和第二金属基复合层。 可以形成夹层型结构。 核心材料可以是固体材料,泡沫,蜂窝结构,或者可以是沟道材料。 金属基复合层可包括纤维增强金属基复合材料。
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公开(公告)号:US20050233128A1
公开(公告)日:2005-10-20
申请号:US10995517
申请日:2004-11-24
申请人: Brian Joseph , Robert Nolte , Matthew Rowe , James Witzgall , Gregg Wolfe
发明人: Brian Joseph , Robert Nolte , Matthew Rowe , James Witzgall , Gregg Wolfe
CPC分类号: B23K20/10 , B22F2998/00 , B23K1/19 , B23K31/02 , B23K2103/16 , Y10T428/249927 , C22C49/04
摘要: The present invention provides for assemblies comprising metal matrix composite bars where the bars only intermittently have mutual contact. Minimally two bars of metal matrix composite are joined, for example, by lap joints, or by the use of incorporated tabs and slots or over-lapping slots, at areas of mutual contact to form the assemblies. The metal matrix composite assemblies of the present invention may be readily assembled to provide structures, supports, or sub-assemblies, and the like, that may exhibit high strength and stiffness coupled with relatively low mass. Additionally, such assemblies may withstand exposure to elevated temperatures higher than can be tolerated by polymeric composites. Such assemblies are expected to be particularly suitable for lightweight, stiff support structures for space booms, satellite structures, mirror backings, solar panel supports, wall reinforcement, and the like.
摘要翻译: 本发明提供了包括金属基质复合棒的组件,其中棒仅间歇地具有相互接触。 金属基复合材料的最小的两个条例如通过搭接接头,或通过使用结合的凸片和槽或叠合槽,在相互接触的区域处连接以形成组件。 本发明的金属基复合组件可以容易地组装以提供结构,支撑件或子组件等,其可以表现出高度和刚度以及相对较低的质量。 此外,这种组件可承受暴露于高于聚合物复合材料可耐受的升高的温度。 预期这种组件特别适用于用于空间吊杆,卫星结构,镜子背衬,太阳能电池板支撑件,墙壁加强件等的轻型,刚性支撑结构。
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