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    Hybrid aerogel rigid ceramic fiber insulation and method of producing same
    1.
    发明授权
    Hybrid aerogel rigid ceramic fiber insulation and method of producing same 有权
    混合气凝胶硬质陶瓷纤维绝缘及其制造方法

    公开(公告)号：US06770584B2

    公开(公告)日：2004-08-03

    申请号：US10222651

    申请日：2002-08-16

    申请人： Andrea O. Barney ,  Vann Heng ,  Kris Shigeko Oka ,  Maryann Santos ,  Alfred A. Zinn ,  Michael Droege

    发明人： Andrea O. Barney ,  Vann Heng ,  Kris Shigeko Oka ,  Maryann Santos ,  Alfred A. Zinn ,  Michael Droege

    IPC分类号： C04B3580

    CPC分类号： C04B41/009 ,  C04B14/064 ,  C04B14/302 ,  C04B30/02 ,  C04B41/4582 ,  Y10T428/249928 ,  Y10T428/249929 ,  Y10T442/2148 ,  Y10T442/2664 ,  Y10T442/2975 ,  C04B14/4625 ,  C04B14/4631 ,  C04B20/0064 ,  C04B22/0013 ,  C04B41/5022 ,  C04B41/5031 ,  C04B41/5035

    摘要： A hybrid insulation material comprises of porous ceramic substrate material impregnated with nanoporous material and method of making the same is the topic of this invention. The porous substrate material has bulk density ranging from 6 to 20 lb/ft3 and is composed of about 60 to 80 wt % silica (SiO2) 20 to 40 wt % alumina (Al2O3) fibers, and with about 0.1 to 1.0 wt % boron-containing constituent as the sintering agent. The nanoporous material has density ranging from 1.0 to 10 lb/ft3 and is either fully or partially impregnated into the substrate to block the pores, resulting in substantial reduction in conduction via radiation and convention. The nanoporous material used to impregnate the fiber substrate is preferably formed from a precursor of alkoxysilane, alcohol, water, and an acid or base catalyst for silica aerogels, and from a precursor of aluminum alkoxide, alcohol, water, and an acid or base catalyst for alumina aerogels.

    摘要翻译： 一种混合绝缘材料包括浸渍有纳米多孔材料的多孔陶瓷衬底材料及其制造方法是本发明的主题。 多孔基材材料的堆积密度为6至20lb / ft 3，并且由约60至80wt％的二氧化硅（SiO 2）20至40wt％的氧化铝（Al 2 O 3）纤维和约0.1至1.0wt ％含硼组分作为烧结剂。 纳米多孔材料的密度范围为1.0至10lb / ft 3，并且完全或部分地浸渍到基底中以阻挡孔，导致通过辐射和惯例显着降低传导。 用于浸渍纤维基材的纳米多孔材料优选由烷氧基硅烷，醇，水和用于二氧化硅气凝胶的酸或碱催化剂的前体，以及来自烷氧基铝，醇，水和酸或碱催化剂的前体形成 用于氧化铝气凝胶。

    Aeroshell thermal protection system and method
    4.
    发明授权
    Aeroshell thermal protection system and method 有权
    Aeroshell热保护系统及方法

    公开(公告)号：US08864073B1

    公开(公告)日：2014-10-21

    申请号：US13192431

    申请日：2011-07-27

    申请人： Ben Y. Won ,  Peter A. Hogenson ,  Vann Heng ,  Mary M. Litwinski ,  Robert J. Perez ,  Caroline Neri Kim

    发明人： Dae H. Kim ,  Ben Y. Won ,  Peter A. Hogenson ,  Vann Heng ,  Mary M. Litwinski ,  Robert J. Perez

    IPC分类号： B64C1/38 ,  B64G1/58

    CPC分类号： B64C1/38 ,  B64G1/14 ,  B64G1/58

    摘要： A thermal protection system for a vehicle may include a substantially rigid, relatively thin outer aeroshell, a relatively low density insulation layer, and a resiliently compressible conformal layer. The vehicle may include a substructure. The aeroshell may be configured to be fastened to the substructure. The insulation layer may be disposed against the aeroshell. The conformal layer may be disposable against the insulation layer. The conformal layer may be compressively preloaded against the substructure when the aeroshell is fastened to the substructure.

    摘要翻译： 用于车辆的热保护系统可以包括基本上刚性的，较薄的外部气囊，相对低密度的绝缘层和可弹性压缩的保形层。 车辆可以包括子结构。 气囊可以被配置为紧固到子结构。 绝缘层可以抵靠气囊设置。 保形层可以是一次性抵抗绝缘层。 当气溶胶被固定到子结构体上时，共形层可以压缩地预加载到子结构上。

    Rigid insulation and method of producing same
    9.
    发明授权
    Rigid insulation and method of producing same 有权
    刚性绝缘及其制造方法

    公开(公告)号：US06716782B2

    公开(公告)日：2004-04-06

    申请号：US10222622

    申请日：2002-08-16

    申请人： Vann Heng ,  Karrie Ann Hinkle ,  Mary Ann Santos

    发明人： Vann Heng ,  Karrie Ann Hinkle ,  Mary Ann Santos

    IPC分类号： C04B3580

    CPC分类号： C04B35/806 ,  C04B30/02 ,  C04B35/62635 ,  C04B38/0038 ,  C04B2111/00379 ,  C04B2111/00982 ,  C04B2235/3821 ,  C04B2235/5224 ,  C04B2235/5232 ,  C04B2235/526 ,  C04B2235/5264 ,  C04B2235/5268 ,  C04B2235/77 ,  C04B2235/94 ,  C04B2235/9607 ,  Y10T428/249928 ,  Y10T428/249929 ,  C04B14/323 ,  C04B14/4625 ,  C04B14/4631 ,  C04B40/0071 ,  C04B40/0268

    摘要： A porous ceramic fiber insulating material and method of making a material having a combination of silica (SiO2) and alumina (Al2O3) fibers, and boron-containing powders is the topic of the new invention. The insulative material is composed of about 60 wt % to about 80 wt % silica fibers, about 20 wt % to about 40 wt % alumina fibers, and about 0.1 wt % to about 1.0 wt % boron-containing powders. A specific boron-containing powder used for this invention is boron carbide powder which provide boron-containing by-products, which aid in fusion and sintering of the silica and alumina fibers. The material is produced by forming an aqueous slurry, blending and chopping the fibers via a shear mixer, orienting the fibers in the in-plane direction, draining water from the fibers, pressing the fibers into a billet, heating the fibers to remove residual water, and firing the billet to fuse the fibers of the material. After sintering, bulk density of the new insulation material ranges from 6 to 20 lb/ft3.

    摘要翻译： 多孔陶瓷纤维绝缘材料和制备具有二氧化硅（SiO 2）和氧化铝（Al 2 O 3）纤维和含硼粉末的组合的材料的方法是本发明的主题。 绝缘材料由约60重量％至约80重量％的二氧化硅纤维，约20重量％至约40重量％的氧化铝纤维和约0.1重量％至约1.0重量％的含硼粉末组成。 用于本发明的特定的含硼粉末是提供含硼副产物的碳化硼粉末，其有助于二氧化硅和氧化铝纤维的熔融和烧结。 该材料通过形成含水浆料，通过剪切混合器共混和切割纤维来制造，将纤维定向在面内方向，从纤维中排出水，将纤维压制成坯料，加热纤维以除去残留的水 ，并烧制坯料以熔化材料的纤维。 烧结后，新型绝缘材料的体积密度范围为6至20磅/英尺3。

    Air foil having a hybrid leading edge construction
    10.
    发明授权
    Air foil having a hybrid leading edge construction 失效
    具有混合前缘结构的气翼

    公开(公告)号：US06367740B1

    公开(公告)日：2002-04-09

    申请号：US09572382

    申请日：2000-05-16

    申请人： Scott E. Johnson ,  Vann Heng ,  Guillermo Mas

    发明人： Scott E. Johnson ,  Vann Heng ,  Guillermo Mas

    IPC分类号： B64C338

    CPC分类号： B64C3/36 ,  B64C3/28

    摘要： A leading edge component for reducing drag and improving heat sink properties of an air foil. The leading edge component includes a composite tile component with a predetermined aerodynamic shape and a metallic lip portion with high thermal conductivity. The metallic lip portion is secured to a forwardmost edge portion of the composite tile component to thereby form a leading edge of the air foil. The leading edge component is better able to withstand the structural stresses and extremely high temperatures that result while travelling at hypersonic speeds, without a significant increase in weight to the air foil with which the leading edge component is used.

    摘要翻译： 用于减少阻力并改善气翼的散热性能的前沿部件。 前缘部件包括具有预定空气动力学形状的复合瓦片部件和具有高导热性的金属唇部分。 金属唇部固定在复合瓷砖部件的最前缘部分上，从而形成空气箔的前缘。 前缘部件能够更好地承受在超音速行驶时产生的结构应力和极高的温度，而不会使用前缘部件使用的气翼的重量显着增加。