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    • 62. 发明授权
    • Water-dispersed coating composition comprising an acrylic graft polymer
containing carboxyl groups, hydroxyl and/or amide groups
    • 包含含有羧基,羟基和/或酰胺基团的丙烯酸接枝聚合物的水分散涂料组合物
    • US4329266A
    • 1982-05-11
    • US186557
    • 1980-09-12
    • Yukio SuzukiNaozumi IwasawaTadashi Watanabe
    • Yukio SuzukiNaozumi IwasawaTadashi Watanabe
    • C08F290/12C09D151/00C08L61/28
    • C08F290/126C09D151/003
    • A water-dispersed coating composition comprising (1) a dispersion of a water-dispersible form of an acrylic graft polymer containing carboxyl groups and hydroxyl and/or amide groups in an aqueous medium containing 60 to 90% by weight of water, and (2) an amino resin. The water-dispersible form of this polymer is obtained by neutralizing at least 50% of the carboxyl groups of the polymer with a basic substance. Prior to neutralization, the polymer has an acid value of 15 to 40 and a glass transition temperature of -10.degree. C. to 70.degree. C., and is produced by polymerizing (A) an acrylic copolymer and (B) a mixture of an alpha,beta-ethylenically unsaturated carboxylic acid and another copolymerizable unsaturated monomer. The copolymer (A) and the mixture (B) is selected so that either one of them has hydroxyl and/or amide groups and the difference between the acid value of the copolymer (A) and that of the mixture (B) is from 25 to 200. The present invention also provides a water-dispersed coating composition comprising a dispersion of a water-dispersible form of a self-curable acrylic graft polymer without an amino resin.
    • 一种水分散涂料组合物,其包含(1)含水分散体形式的含羧基和羟基和/或酰胺基的丙烯酸接枝聚合物在含有60-90%重量水的水性介质中的分散体,和(2) )氨基树脂。 该聚合物的水分散形式通过用碱性物质中和聚合物的至少50%的羧基而获得。 在中和之前,聚合物的酸值为15至40,玻璃化转变温度为-10℃至70℃,并通过聚合(A)丙烯酸共聚物和(B)将 α,β-烯属不饱和羧酸和另一种可共聚的不饱和单体。 选择共聚物(A)和混合物(B),使得它们中的任一个具有羟基和/或酰胺基,并且共聚物(A)和混合物(B)的酸值之间的差异为25 本发明还提供一种水分散涂料组合物,其包含不具有氨基树脂的可分散自由基的丙烯酸接枝聚合物的分散体。
    • 70. 发明申请
    • Latch device of cockpit door of an aircraft
    • 飞机驾驶舱门的锁定装置
    • US20080111025A1
    • 2008-05-15
    • US11905519
    • 2007-10-02
    • Fumiaki SakuTadashi WatanabeYasuo Sekikawa
    • Fumiaki SakuTadashi WatanabeYasuo Sekikawa
    • B64C1/14
    • B64C1/1469B64C2001/009B64D45/0015E05B51/023
    • 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.
    • 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。