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16 条记录 (耗时 0.025 秒)

    ELECTROCHROMIC DEVICE
    4.
    发明公开
    ELECTROCHROMIC DEVICE 审中-公开
    电致变色器件

    公开(公告)号：EP2329317A1

    公开(公告)日：2011-06-08

    申请号：EP09791864.3

    申请日：2009-08-25

    申请人： PPG Industries Ohio, Inc.

    发明人： FINLEY, James, J. ,  SCHWENDEMAN, Irina G. ,  POLCYN, Adam D. ,  HARRIS, Caroline S.

    IPC分类号： G02F1/155

    CPC分类号： G02F1/155 ,  B82Y20/00 ,  G02F1/1523 ,  G02F1/1525 ,  G02F2001/1515 ,  G02F2202/36

    摘要： An electrochromic device (10) includes a first substrate (12) spaced from a second substrate (14). A first conductive member (16) is formed over at least a portion of the first substrate (12). A first electrochromic electrode (18) comprising a tungsten oxide coating is formed over at least a portion of the first conductive member (16). A second conductive member (20) is formed over at least a portion of the second substrate (14). A second electrochromic electrode (22) is formed over at least a portion of the second conductive member (20). An ionic liquid (24) is positioned between the first electrode (18) and the second electrode (22). In one aspect of the invention, the ionic liquid (24) can include nanoparticies of metals or metal oxides. In a further aspect of the invention, the second conductive member (20) and second electrode (22) can be formed by a single material.

    DEFORMABLE AIRCRAFT WINDOW
    5.
    发明公开
    DEFORMABLE AIRCRAFT WINDOW 审中-公开

    公开(公告)号：EP3372489A1

    公开(公告)日：2018-09-12

    申请号：EP18167192.6

    申请日：2014-08-05

    申请人： PPG Industries Ohio, Inc.

    发明人： MCCARTHY, Dennis P. ,  BLEVINS, Calvin, B. ,  HARRIS, Caroline S. ,  GOODWIN, George B. ,  GU, YaBei

    IPC分类号： B64C1/14

    摘要： An aircraft window assembly (10) includes a first panel (12) having a first surface (14) and a second surface (16). In a first state in which there is no pressure difference between the first surface (14) and the second surface (16), the first panel (12) has a cross-sectional shape selected from planar, outwardly convex, or inwardly convex. In a second state in which there is a pressure difference between first surface (14) and the second surface (16), the first panel (12) has an outwardly convex cross-sectional shape.

    DEFORMABLE AIRCRAFT WINDOW
    6.
    发明公开
    DEFORMABLE AIRCRAFT WINDOW 审中-公开

    公开(公告)号：EP3677501A1

    公开(公告)日：2020-07-08

    申请号：EP20152806.4

    申请日：2014-08-05

    申请人： PPG Industries Ohio, Inc.

    发明人： MCCARTHY, Dennis P. ,  BLEVINS, Calvin B. ,  HARRIS, Caroline S. ,  GOODWIN, George B. ,  GU, YaBei

    IPC分类号： B64C1/14 ,  B29C33/00

    摘要： An aircraft window assembly (10) includes a first panel (12) having a first surface (14) and a second surface (16). In a first state in which there is no pressure difference between the first surface (14) and the second surface (16), the first panel (12) has a cross-sectional shape selected from planar, outwardly convex, or inwardly convex. In a second state in which there is a pressure difference between first surface (14) and the second surface (16), the first panel (12) has an outwardly convex cross-sectional shape. The assembly (10) comprises a wire grid (102) embedded in the first panel (12).

    LITHIUM CONTAINING GLASS WITH HIGH AND LOW OXIDIZED IRON CONTENT, METHOD OF MAKING SAME AND PRODUCTS USING SAME
    8.
    发明公开
    LITHIUM CONTAINING GLASS WITH HIGH AND LOW OXIDIZED IRON CONTENT, METHOD OF MAKING SAME AND PRODUCTS USING SAME 审中-公开
    含锂玻璃有高有低含量的氧化铁，方法其生产和产品

    公开(公告)号：EP3145882A1

    公开(公告)日：2017-03-29

    申请号：EP15725201.6

    申请日：2015-05-15

    申请人： PPG Industries Ohio, Inc.

    发明人： GOODWIN, George B. ,  ARBAB, Mehran ,  HARRIS, Caroline S. ,  SHELESTAK, Larry J. ,  BLEVINS, Calvin B. ,  HARTMANN, James V.

    IPC分类号： C03C3/083 ,  B32B17/10 ,  C03C3/087 ,  C03C3/095 ,  C03C4/10 ,  G02B23/00

    CPC分类号： C03C3/087 ,  B32B17/10045 ,  B32B17/10119 ,  B32B17/10761 ,  B32B2605/18 ,  C03C3/083 ,  C03C3/095 ,  C03C4/082 ,  C03C4/10

    摘要： A low infrared absorbing lithium glass includes FeO in the range of 0.0005-0.015 wt.%, more preferably 0.001-0.010 wt.%, and a redox ratio in the range of 0.005-0.15, more preferably in the range of 0.005-0.10. The glass can be chemically tempered and used to provide a ballistic viewing cover for night vision goggles or scope. A method is provided to change a glass making process from making a high infrared absorbing lithium glass having FeO in the range of 0.02 to 0.04 wt.% and a redox ratio in the range of 0.2 to 0.4 to the low infrared absorbing lithium glass by adding additional oxidizers to the batch materials. A second method is provided to change a glass making process from making a low infrared absorbing lithium glass to the high infrared absorbing lithium glass by adding additional reducers to the batch material. In one embodiment of the invention the oxidizer is CeO
    2 . An embodiment of the invention covers a glass made according to the method.

    摘要翻译： 低红外吸收锂玻璃包括在的FeO的0.0005-0.015％（重量），更优选地从0001至0010重量％的范围内，并且在0.005-0.10范围内，以0.005-0.15范围内的氧化还原比，更优选。 玻璃可以是化学回火和用于为夜视护目镜或范围提供一个弹道观看盖。 提供了一种方法，以从制备在0点02分的范围内具有的FeO高红外线吸收锂玻璃0时04重量％和在0.2至0.4的低红外吸收锂玻璃通过增加氧化还原比改变玻璃制造过程 附加氧化剂到批料材料。 提供第二方法从通过添加额外的还原剂到所述批料制备低红外线吸收玻璃的高红外线吸收锂玻璃锂改变玻璃制造过程。 在本发明的一个实施方案中，氧化剂是氧化铈。 本发明的一个实施例覆盖雅丁的方法制成的玻璃。

    AIRCRAFT TRANSPARENCY WITH SOLAR CONTROL PROPERTIES
    10.
    发明公开
    AIRCRAFT TRANSPARENCY WITH SOLAR CONTROL PROPERTIES 审中-公开
    随着太阳能系统控制功能的飞机透明

    公开(公告)号：EP2440403A2

    公开(公告)日：2012-04-18

    申请号：EP10782069.8

    申请日：2010-06-10

    申请人： PPG Industries Ohio, Inc.

    发明人： RASHID, Ali ,  BUHAY, Harry ,  HARRIS, Caroline S. ,  BASIL, John D. ,  HUNIA, Robert M.

    IPC分类号： B32B15/04

    摘要： An aircraft transparency includes a first stretched acrylic ply and a second stretched acrylic ply. A coating stack having solar control properties is applied over at least a portion of one or more of the major surfaces. The coating stack includes a first primer layer comprising an epoxy amino siloxane-containing material. A solar coating having at least three metallic silver layers is formed over at least a portion of the first primer layer. A protective coating including silica and alumina is formed over at least a portion of the solar control coating. A topcoat including a polysiloxane material is formed over at least a portion of the protective coating. An overcoat is formed over at least a portion of the topcoat and includes a diamond-like carbon type coating.