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    • 4. 发明授权
    • Composite truss armor
    • 复合桁架装甲
    • US08272309B1
    • 2012-09-25
    • US13370256
    • 2012-02-09
    • Robert W. CumberlandAlan J. JacobsenAdam F. GrossWilliam B. Carter
    • Robert W. CumberlandAlan J. JacobsenAdam F. GrossWilliam B. Carter
    • F41H5/02
    • F41H5/0492F41H5/0414F41H5/0442
    • A composite truss armor and a method of manufacturing the same. The composite truss armor includes a filler material and a three-dimensional (3D) ordered truss structure. The 3D ordered truss structure includes: a plurality of first truss elements defined by a plurality of first self-propagating polymer waveguides and extending along a first direction; a plurality of second truss elements defined by a plurality of second self-propagating polymer waveguides and extending along a second direction; and a plurality of third truss elements defined by a plurality of third self-propagating polymer waveguides and extending along a third direction. The first, second, and third ordered truss elements interpenetrate each other at a plurality of nodes to form a continuous material. The first, second, and third truss elements define an open space. The filler material occupies at least a portion of the open space, and the 3D ordered truss structure is self-supporting.
    • 一种复合桁架装甲及其制造方法。 复合桁架装甲包括填充材料和三维(3D)有序桁架结构。 3D有序桁架结构包括:由多个第一自传播聚合物波导限定并沿着第一方向延伸的多个第一桁架元件; 由多个第二自传播聚合物波导限定并沿着第二方向延伸的多个第二桁架元件; 以及由多个第三自传播聚合物波导限定并沿着第三方向延伸的多个第三桁架元件。 第一,第二和第三有序的桁架元件在多个节点处相互渗透以形成连续材料。 第一,第二和第三桁架元件定义了一个开放空间。 填充材料占据开放空间的至少一部分,并且3D有序桁架结构是自支撑的。
    • 5. 发明授权
    • Composite structures for storing thermal energy
    • 用于储存热能的复合结构
    • US07938989B1
    • 2011-05-10
    • US12589262
    • 2009-10-20
    • Adam F. GrossRonald M. FinnilaAlan J. JacobsenRobert CumberlandSky L. Skeith
    • Adam F. GrossRonald M. FinnilaAlan J. JacobsenRobert CumberlandSky L. Skeith
    • G02B1/12
    • F28D20/023Y02E60/145
    • A composite structure for storing thermal energy. In one embodiment, an apparatus for storing thermal energy includes: a thermal storage material and a three-dimensional structure. The three-dimensional structure includes: a plurality of first truss elements defined by a plurality of first self-propagating polymer waveguides and extending along a first direction; a plurality of second truss elements defined by a plurality of second self-propagating polymer waveguides and extending along a second direction; and a plurality of third truss elements defined by a plurality of third self-propagating polymer waveguides and extending along a third direction. The first, second, and third truss elements interpenetrate each other at a plurality of nodes to form a continuous material. The first, second, and third truss elements define an open space. The thermal storage material occupies at least a portion of the open space, and the three-dimensional structure is self-supporting.
    • 一种用于储存热能的复合结构。 在一个实施例中,用于存储热能的装置包括:热存储材料和三维结构。 三维结构包括:由多个第一自传播聚合物波导限定并沿着第一方向延伸的多个第一桁架元件; 由多个第二自传播聚合物波导限定并沿着第二方向延伸的多个第二桁架元件; 以及由多个第三自传播聚合物波导限定并沿着第三方向延伸的多个第三桁架元件。 第一,第二和第三桁架元件在多个节点处相互渗透以形成连续材料。 第一,第二和第三桁架元件定义了一个开放空间。 储热材料占据开放空间的至少一部分,并且三维结构是自支撑的。
    • 7. 发明授权
    • Composite structures for storing thermal energy
    • 用于储存热能的复合结构
    • US07653276B1
    • 2010-01-26
    • US12075033
    • 2008-03-06
    • Adam F. GrossRonald M. FinnilaAlan J. JacobsenRobert CumberlandSky L. Skeith
    • Adam F. GrossRonald M. FinnilaAlan J. JacobsenRobert CumberlandSky L. Skeith
    • G02B6/26G02B6/255
    • F28D20/023Y02E60/145
    • A composite structure for storing thermal energy. In one embodiment, an apparatus for storing thermal energy includes: a thermal storage material and a three-dimensional structure. The three-dimensional structure includes: a plurality of first truss elements defined by a plurality of first self-propagating polymer waveguides and extending along a first direction; a plurality of second truss elements defined by a plurality of second self-propagating polymer waveguides and extending along a second direction; and a plurality of third truss elements defined by a plurality of third self-propagating polymer waveguides and extending along a third direction. The first, second, and third truss elements interpenetrate each other at a plurality of nodes to form a continuous material. The first, second, and third truss elements define an open space. The thermal storage material occupies at least a portion of the open space, and the three-dimensional structure is self-supporting.
    • 一种用于储存热能的复合结构。 在一个实施例中,用于存储热能的装置包括:热存储材料和三维结构。 三维结构包括:由多个第一自传播聚合物波导限定并沿第一方向延伸的多个第一桁架元件; 由多个第二自传播聚合物波导限定并沿着第二方向延伸的多个第二桁架元件; 以及由多个第三自传播聚合物波导限定并沿着第三方向延伸的多个第三桁架元件。 第一,第二和第三桁架元件在多个节点处相互渗透以形成连续材料。 第一,第二和第三桁架元件定义了一个开放空间。 储热材料占据开放空间的至少一部分,并且三维结构是自支撑的。
    • 8. 发明申请
    • SELF DECONTAMINATING CHEMICAL AND BIOLOGICAL AGENT RESISTANT COATING
    • 自我去除化学和生物耐药性涂料
    • US20090298967A1
    • 2009-12-03
    • US12131808
    • 2008-06-02
    • Lynn G. TaylorNancy W. CarlsonAdam F. Gross
    • Lynn G. TaylorNancy W. CarlsonAdam F. Gross
    • C09D5/14C09D5/00
    • C09D175/04A62D5/00A62D2101/02C09D5/14C09D5/1612
    • The disclosure provides for a self decontaminating coating and method. The coating comprises a polyurethane component having a solids content in the range of about 10 weight percent to about 100 weight percent and having at least one volume percent free space, a chemical active, and a biological active. In another disclosed embodiment, a method of reducing the transportation of chemical contaminants and biological contaminants is provided comprising the steps of providing a self decontaminating coating comprising a polyurethane component having a polyurethane component having a solids content in the range of about 10 weight percent to about 100 weight percent and having at least one volume percent free space, a chemical active, and a biological active, and applying the coating to a surface of an aircraft, rotorcraft, vehicle, item of equipment, or architectural structure.
    • 本公开提供了一种自净化涂层和方法。 该涂层包含固体含量在约10重量%至约100重量%范围内且具有至少一个体积百分比自由空间的聚氨酯组分,化学活性物质和生物活性物质。 在另一个公开的实施方案中,提供了减少化学污染物和生物污染物的运输的方法,包括以下步骤:提供自净化涂层,其包含聚氨酯组分,所述聚氨酯组分具有约10重量%至约 100重量%并具有至少一个体积百分比的自由空间,化学活性物质和生物活性物质,并将该涂层施加到飞行器,旋翼飞行器,车辆,设备项目或建筑结构的表面上。