Aqueous coating composition
    51.
    发明授权
    Aqueous coating composition 失效
    水性涂​​料组合物

    公开(公告)号:US3993612A

    公开(公告)日:1976-11-23

    申请号:US559770

    申请日:1975-03-19

    摘要: In an aqueous coating composition comprising a vinyl polymer emulsion prepared by subjecting a vinyl monomer to emulsion polymerization in an aqueous medium in the presence of maleinized polybutadiene used as a dispersion stabilizer, an improvement which is characterized in that at least one copolymer is further incorporated, said copolymer being composed of (A) at least one monomer prepared by reacting one glycidyl ester of acrylic acid and methacrylic acid with at least one fatty acid of drying oil fatty acid and semi-drying oil fatty acid, (B) at least one .alpha.,.beta.-ethylenically unsaturated acid and (C) at least one unsaturated monomer containing substantially no carboxyl group and having a Q value of at least 0.1 as determined by Q-e theory.

    摘要翻译: 在包含乙烯基聚合物乳液的水性涂料组合物中,其改进在于进一步引入至少一种共聚物,该乙烯基聚合物乳液是通过使乙烯基单体在含水介质中进行乳液聚合而制备的,所述聚合物乳液在用作分散稳定剂的马来化聚丁二烯存在下, 所述共聚物由(A)至少一种通过丙烯酸缩水甘油酯和甲基丙烯酸与干性油脂肪酸和半干性油脂肪酸的至少一种脂肪酸反应制备的单体,(B)至少一种α ,β-烯键式不饱和酸和(C)至少一种不含羧基的不饱和单体,并通过Qe理论确定Q值至少为0.1。

    Method for curing a coating film
    53.
    发明授权
    Method for curing a coating film 失效
    固化涂膜的方法

    公开(公告)号:US3936368A

    公开(公告)日:1976-02-03

    申请号:US93466

    申请日:1970-11-27

    CPC分类号: C09D167/08 C09D5/4423

    摘要: A method for curing a coating film wherein a filmforming, polymerizable, organic coating material is electrodeposited upon an electroconductive object as an anode immersed in an aqueous dispersion of an acidic alkyd resin modified with conjugated unsaturated fatty acid and/or oil, wherein the acidic alkyd resin has an oil length in the range of 10 to 60 wt % and a resin acid value in the range of 30 to 100, being neutralized with water soluble bases, and then the curing coating film thus obtained by applying ionizing radiation.

    摘要翻译: 一种用于固化涂膜的方法,其中成膜可聚合的有机涂层材料电沉积在浸渍在用共轭不饱和脂肪酸和/或油改性的酸性醇酸树脂的水性分散体中的作为阳极的导电物体上,其中酸性醇酸树脂 树脂的油长度在10〜60重量%的范围内,树脂酸值在30〜100的范围内,用水溶性碱中和,然后通过施加电离辐射得到固化涂膜。

    Field effect transistor and method for fabricating the same
    54.
    发明授权
    Field effect transistor and method for fabricating the same 有权
    场效应晶体管及其制造方法

    公开(公告)号:US08188520B2

    公开(公告)日:2012-05-29

    申请号:US13104537

    申请日:2011-05-10

    IPC分类号: H01L29/66

    摘要: A method for fabricating a field effect transistor includes: forming an insulating film provided on a semiconductor layer, the insulating film having an opening via which a surface of the semiconductor layer is exposed and including silicon oxide; forming a Schottky electrode on the insulating film and in the opening, the Schottky electrode having an overhang portion and having a first contact layer that is provided in a region contacting the insulating film and contains oxygen, and a second contact layer that is provided on the first contact layer and contains a smaller content of oxygen than that of the first contact layer; and removing the insulating film by a solution including hydrofluoric acid.

    摘要翻译: 一种用于制造场效应晶体管的方法,包括:形成设置在半导体层上的绝缘膜,所述绝缘膜具有暴露所述半导体层的表面并且包括氧化硅的开口; 在所述绝缘膜上和所述开口中形成肖特基电极,所述肖特基电极具有突出部分,并且具有设置在与所述绝缘膜接触并包含氧的区域中的第一接触层,以及设置在所述绝缘膜上的第二接触层 第一接触层并且含有比第一接触层的氧更小的氧含量; 并通过包含氢氟酸的溶液除去绝缘膜。

    Latch device of cockpit door of an aircraft
    55.
    发明申请
    Latch device of cockpit door of an aircraft 有权
    飞机驾驶舱门的锁定装置

    公开(公告)号:US20080111025A1

    公开(公告)日:2008-05-15

    申请号:US11905519

    申请日:2007-10-02

    IPC分类号: B64C1/14

    摘要: A latch device for detecting pressure reduction of a cockpit in an aircraft and releasing a bolt and a stopper device are provided so as to prevent a cockpit door from unexpectedly opening by an impact. A main latch device 100 of the cockpit door has a frame 112 fixed to a door panel, and a latch base 120 is mounted to the frame 112 capable of pivotal rotation with a pin 122 as a fulcrum. A bolt 132 is inserted into a catch in conjunction with a door handle 130. A holding/releasing portion 150 holds the latch base 120. When a pressure difference occurs between a cockpit 4 and a cabin 5, a pressure-sensing piston 160 is pushed in, a trigger 170 and a flapper 180 are rotated and the latch base 120 is released. A stopper device 190 regulates movement of the trigger 170 by movement of an inertial piston 192 when an impact force is applied from the cabin 5 side.

    摘要翻译: 用于检测飞行器中的驾驶舱的减压并释放螺栓和止动装置的闩锁装置被设置成防止驾驶舱门被冲击意外地打开。 驾驶舱门的主闩锁装置100具有固定到门板的框架112,并且闩锁基座120安装到能够以销122作为支点枢转旋转的框架112。 螺栓132与门把手130一起插入到卡扣中。 保持/释放部分150保持闩锁基座120。 当驾驶舱4和驾驶舱5之间发生压力差时,压力传感活塞160被推入,触发器170和挡板180旋转并且闩锁底座120被释放。 止动装置190通过惯性活塞192的移动来调节触发器170的运动,当从机舱5侧施加冲击力时。

    Epi-illumination microscope and fluorescence filter set
    56.
    发明授权
    Epi-illumination microscope and fluorescence filter set 有权
    Epi照明显微镜和荧光滤光片组

    公开(公告)号:US07285787B2

    公开(公告)日:2007-10-23

    申请号:US11097351

    申请日:2005-04-04

    IPC分类号: G01K1/08 G01J3/30

    摘要: A microscope has a light source that emits light to illuminate a sample, a first wavelength selection member that selectively transmits the light from the light source, a light splitter that reflects the light from the first wavelength selection member to epi-illuminate the sample and transmits the light emitted from the sample, and a second wavelength selection member that selectively transmits the light transmitted through the light splitter. The light splitter is constituted of a transparent member and a dichroic mirror coat disposed on the transparent member. The dichroic mirror coat is constituted of a stacked layer that efficiently reflects light having a wavelength selected by the first wavelength selection member and a stacked layer that reflects light on a short wavelength side from the light selected by the first wavelength selection member, light on a long wavelength side, light of the same band, or combined light.

    摘要翻译: 显微镜具有发出光以照射样品的光源,选择性地透射来自光源的光的第一波长选择部件,将来自第一波长选择部件的光反射到外部照射样品并透射的光分离器 从样品发射的光和选择性地透射透过分光器的光的第二波长选择构件。 光分路器由透明构件和设置在透明构件上的分色镜面构成。 二向色镜面由层叠层构成,该叠层有效地反射由第一波长选择部件选择的波长的光和从短波长侧的光反射从第一波长选择部件所选择的光的层叠层, 长波长侧,相同波段的光或组合光。

    Semiconductor device with built-in scan test circuit
    57.
    发明申请
    Semiconductor device with built-in scan test circuit 审中-公开
    半导体器件内置扫描测试电路

    公开(公告)号:US20060156132A1

    公开(公告)日:2006-07-13

    申请号:US11274482

    申请日:2005-11-16

    IPC分类号: G01R31/28

    摘要: The clock cycle during the shift operation is set shorter than the clock cycle during the capture operation in the scan test circuit. For example, the clock cycle during the shift operation is set to 20 nano second, while the clock cycle during the capture operation is set to 100 nano second. The clock is fed from a LSI tester outside of the LSI through the clock terminal CLK. The cycle of the clock can be switched to synchronize with the change of the scan enable signal SCANEN by the LSI tester. The time for shift operation can be shortened in this invention, leading to the shorter scan test time.

    摘要翻译: 在扫描测试电路中,在移位操作期间的时钟周期被设置为短于捕获操作期间的时钟周期。 例如,在移位操作期间的时钟周期设置为20纳秒,而在捕获操作期间的时钟周期设置为100纳秒。 时钟由LSI外部的LSI测试仪通过时钟端CLK供电。 时钟的周期可以切换为与LSI测试仪的扫描使能信号SCANEN的改变同步。 在本发明中可以缩短换档操作的时间,从而缩短扫描测试时间。

    Cockpit door of aircraft
    59.
    发明授权
    Cockpit door of aircraft 失效
    飞机的驾驶舱门

    公开(公告)号:US06976658B2

    公开(公告)日:2005-12-20

    申请号:US10747309

    申请日:2003-12-30

    IPC分类号: B64C1/14 B64D45/00

    摘要: A cockpit door comprises a hinge 20 provided to one surface and a latch device provided to the other side that can be operated only from the cockpit side. To the inside of a door panel is disposed a reinforcement member 110 formed by laminating multiple layers of sheets with thermoplastic adhesives, the sheets formed by laminating aromatic polyamide fiber onto a honeycomb panel and processing the same into sheet form. A titanium alloy reinforcement plate 400 is disposed to cover the gap G1 between the door body and flap 60. Mounting portions 150 and 160 are provided to the rim of the reinforcement member body 110, and rivet holes 180 are provided thereto. The mounting portion is bent 90 degrees and fixed to the frame by rivets.

    摘要翻译: 驾驶舱门包括设置在一个表面上的铰链20和设置在仅能从驾驶舱侧操作的另一侧的闩锁装置。 在门板的内部设置有通过将热塑性粘合剂层叠多层片而形成的加强部件110,该片材通过将芳族聚酰胺纤维层压在蜂窝板上而形成片状。 钛合金加强板400设置成覆盖门体和折翼60之间的间隙G 1 1。 安装部分150和160设置在加强构件主体110的边缘上,并且向其提供铆钉孔180。 安装部分弯曲90度,并通过铆钉固定在框架上。