Preparation of nanoporous metal foam from high nitrogen transition metal complexes
    1.
    发明申请
    Preparation of nanoporous metal foam from high nitrogen transition metal complexes 审中-公开
    从高氮过渡金属络合物制备纳米多孔金属泡沫

    公开(公告)号:US20070142643A1

    公开(公告)日:2007-06-21

    申请号:US11604644

    申请日:2006-11-27

    CPC classification number: B22F3/1121 B22F2998/00 B22F1/0018

    Abstract: High surface area monolithic foams of essentially pure metal were prepared. Salts of the corresponding metal were prepared as loose powders, pressed into shapes, ignited under an inert atmosphere, and then heated under an atmosphere containing hydrogen to form nanostructured metal foam monoliths of essentially pure metal having a very high surface area.

    Abstract translation: 制备基本上纯金属的高表面积整体泡沫。 制备相应金属的盐作为松散粉末,压制形状,在惰性气氛下点燃,然后在含有氢的气氛下加热,形成具有非常高的表面积的基本上纯的金属的纳米结构金属泡沫整料。

    Spooling pyrotechnic device
    6.
    发明授权

    公开(公告)号:US09062943B2

    公开(公告)日:2015-06-23

    申请号:US13431841

    申请日:2012-03-27

    Applicant: Darren Naud

    Inventor: Darren Naud

    CPC classification number: F42B4/22 F42B4/06 F42B4/24 F42B4/26 F42B4/30

    Abstract: A pyrotechnic device including a combustion chamber including a wall, the combustion chamber containing combustible powder; an ignition source adapted to ignite said combustible powder within said combustion chamber; wherein the wall of the combustion chamber is adapted to burst at a predetermined pressure caused by combustion of the combustible powder; wherein the combustion chamber is disposed within a launch structure beneath a projectile and wherein a preselected amount of free space volume is disposed between said combustion chamber and said projectile.

    Spooling Pyrotechnic Device
    7.
    发明申请

    公开(公告)号:US20130255523A1

    公开(公告)日:2013-10-03

    申请号:US13431841

    申请日:2012-03-27

    Applicant: Darren Naud

    Inventor: Darren Naud

    CPC classification number: F42B4/22 F42B4/06 F42B4/24 F42B4/26 F42B4/30

    Abstract: A pyrotechnic device including a combustion chamber including a wall, the combustion chamber containing combustible powder; an ignition source adapted to ignite said combustible powder within said combustion chamber; wherein the wall of the combustion chamber is adapted to burst at a predetermined pressure caused by combustion of the combustible powder; wherein the combustion chamber is disposed within a launch structure beneath a projectile and wherein a preselected amount of free space volume is disposed between said combustion chamber and said projectile.

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