Spin-on-glass anti-reflective coatings for photolithography
    12.
    发明申请
    Spin-on-glass anti-reflective coatings for photolithography 有权
    旋光玻璃防反射涂层,用于光刻

    公开(公告)号:US20020128388A1

    公开(公告)日:2002-09-12

    申请号:US10076846

    申请日:2002-02-14

    Abstract: Anti-reflective coating materials for deep ultraviolet photolithography include one or more organic light-absorbing compounds incorporated into spin-on-glass materials. Suitable absorbing compounds are strongly absorbing over wavelength ranges around wavelengths such as 365 nm, 248 nm, and 193 nm that may be used in photolithography. A method of making absorbing spin-on-glass materials includes combining one or more organic absorbing compounds with alkoxysilane or halosilane reactants during synthesis of the spin-on-glass materials.

    Abstract translation: 用于深紫外光刻的抗反射涂层材料包括掺入旋涂玻璃材料中的一种或多种有机光吸收化合物。 合适的吸收化合物在可用于光刻的诸如365nm,248nm和193nm的波长附近的波长范围上是强吸收的。 制造吸收旋涂玻璃材料的方法包括在旋涂玻璃材料的合成期间将一种或多种有机吸收化合物与烷氧基硅烷或卤代硅烷反应物组合。

    Low temperature burnout screen printing frit vehicle

    公开(公告)号:US20010008110A1

    公开(公告)日:2001-07-19

    申请号:US09792921

    申请日:2001-02-26

    CPC classification number: C03C8/16

    Abstract: A method for making a glass frit paste is provided. First, nitrocellulose is dissolved in a high vapor pressure solvent of the nitrocellulose to make a solution. A portion of the solution is then mixed with alpha-terpineol to form a vehicle. Glass frit is mixed with the vehicle and then ground to form the paste. During the grinding step most of the high vapor pressure solvent evaporates. The resulting paste has a composition comprising about 0.3-12.0 wt. % nitrocellulose, about 0.5-2.0 wt. % of a high vapor pressure solvent of said nitrocellulose, about 14.0-25.0 wt. % alpha-terpineol, and the remainder glass frit.

    Armor systems
    16.
    发明申请
    Armor systems 失效
    护甲系统

    公开(公告)号:US20030200861A1

    公开(公告)日:2003-10-30

    申请号:US09908224

    申请日:2001-07-18

    Abstract: An armor system useful, for example, as a shroud, comprising a first pliable, cut resistant fibrous layer and a second pliable fibrous layer is disclosed. The first layer is arranged to receive an impact from a large projectile prior to the second layer and engages the projectile to slow its velocity. The second layer is substantially coextensive with the first and dissipates the incoming energy of the impact to resist complete penetration of the second layer by the projectile, preferably by deforming in response to the impact. Both layers comprise fibers having a tensile modulus of at least about 200 g/d, and an energy-to-break of at least about 8 J/g and a tenacity equal to or greater than about 10 g/d. In another embodiment, the layers are reversed relative to the impact face of the system so that the second layer becomes the first layer and is resistant to projectiles impacting the system, while the first layer becomes the second layer and resists deformation of the system by projectile impacts. Any projectile which completely penetrates the first layer is engaged by the second layer to slow its velocity and prevent complete penetration of the second layer. This armor system provides excellent ballistic resistance with enhanced deformation control.

    Abstract translation: 公开了一种可用于例如护罩的装甲系统,其包括第一柔韧的,耐切割的纤维层和第二柔韧的纤维层。 第一层被设置为在第二层之前接收来自大型抛射体的冲击,并且与放射体接合以减慢其速度。 第二层与第一层基本上共同延伸并且消散冲击的进入能量,以抵抗抛射体完全穿透第二层,优选地通过响应于冲击而变形。 两层均包含拉伸模量为至少约200g / d,断裂能为至少约8J / g,强度等于或大于约10g / d的纤维。 在另一个实施例中,层相对于系统的冲击面反转,使得第二层变成第一层,并且抵抗撞击系统的弹丸,而第一层变成第二层并且通过射弹抵抗系统的变形 影响。 完全穿透第一层的任何抛射体都被第二层接合,以减缓其速度并阻止第二层的完全穿透。 该装甲系统提供优异的防弹性,增强变形控制。

    METAL/CERAMIC COMPOSITE MOLDING MATERIAL
    17.
    发明申请
    METAL/CERAMIC COMPOSITE MOLDING MATERIAL 失效
    金属/陶瓷复合材料

    公开(公告)号:US20030125426A1

    公开(公告)日:2003-07-03

    申请号:US09898111

    申请日:2001-07-01

    Abstract: A composite molding compound comprising a combination of metal and ceramic powders is disclosed. The powders are combined with a binder, a liquid carrier and other processing additives in a manner to provide uniform distribution of two phases in a material format that facilitates the molding of complex parts at relatively low pressures and temperatures using conventional injection molding machines. The products formed from these molding compounds may be designed with tailored physical and mechanical properties such as thermal conductivity, thermal expansion coefficient, density, elastic modulus and wear properties.

    Abstract translation: 公开了包含金属和陶瓷粉末的组合的复合模塑料。 粉末与粘合剂,液体载体和其它加工添加剂结合,以便以使用常规注射成型机在相对低的压力和温度下成型复合部件的材料形式均匀分布两相。 由这些模塑料形成的产品可以设计成具有定制的物理和机械性能,例如导热性,热膨胀系数,密度,弹性模量和磨损性能。

    Sizeless yarn, a method of making it and a method of using it
    19.
    发明申请
    Sizeless yarn, a method of making it and a method of using it 失效
    无瑕纱,其制作方法和使用方法

    公开(公告)号:US20020189703A1

    公开(公告)日:2002-12-19

    申请号:US10126229

    申请日:2002-04-18

    Abstract: A yarn having good entanglement and good quality, preferably a multifilament polyamide yarn, a method for making the yarn, and a woven fabric made from the yarn wherein the yarn comprises the following properties: the yarn length per defect is greater than or equal to about 3000 meters per defect; the maximum skip length is less than or equal to about 120 millimeters; the ratio between yarn length per defect to maximum skip length is greater than or equal to about 50; the entanglements per meter times the average entanglement strength is greater than or equal to about 120; and the yarn can be woven sizeless. The yarn of the invention is useful in the sizeless weaving of fabric used in air bags.

    Abstract translation: 具有良好的缠结和良好品质的纱线,优选多丝聚酰胺纱线,纱线制造方法和由纱线制成的机织织物,其中纱线具有以下特性:每个缺陷的纱线长度大于或等于约 缺陷3000米; 最大跳跃长度小于或等于约120毫米; 每个缺陷的纱线长度与最大跳过长度的比率大于或等于约50; 平均缠结强度每米的缠结大于或等于约120; 而纱线可以编织无边。 本发明的纱线在用于气囊的织物的无缝编织中是有用的。

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