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    • 4. 发明授权
    • ESD protective device
    • ESD保护装置
    • US09590417B2
    • 2017-03-07
    • US14267483
    • 2014-05-01
    • Murata Manufacturing Co., Ltd.
    • Yoshihito Otsubo
    • H02H1/00H02H9/04H01T4/12H05K9/00H05K1/02
    • H02H9/04H01T4/12H02H9/044H05K1/0259H05K9/0067H05K9/0079
    • Inside an insulating multilayer substrate 12 in which a plurality of insulating layers are laminated, a cavity portion 13, at least one pair of discharge electrodes 14 and 15, and conductor portions 34 and 35 are formed. The discharge electrodes 14 and 15 are connected to external electrodes 18 and 19 and have facing portions 14a and 15a which are formed along an inner surface of the cavity portion 13 and which face each other with a space provided therebetween. The conductor portions 34 and 35 are formed to cover at least one of facing front ends 14s and 15s of the facing portions 14a and 15a of the discharge electrodes 14 and 15 when viewed in a lamination direction of the insulating layers, a facing direction of the facing portions 14a and 15a, or a direction perpendicular both to the lamination direction and the facing direction.
    • 在层叠有多个绝缘层的绝缘多层基板12的内部形成有空腔部13,至少一对放电电极14,15以及导体部34,35。 放电电极14和15连接到外部电极18和19,并且具有沿着空腔部分13的内表面形成并且彼此面对并设置有间隙的面对部分14a和15a。 导体部分34和35形成为覆盖放电电极14和15的面对部分14a和15a的面向前端14s和15s中的至少一个,当从绝缘层的层叠方向观察时, 面对部分14a和15a,或者与层叠方向和面向方向垂直的方向。
    • 10. 发明申请
    • Aircraft with Electrically Conductive Nanocoating
    • 具有导电纳米涂层的飞机
    • US20140252164A1
    • 2014-09-11
    • US13789269
    • 2013-03-07
    • BELL HELICOPTER TEXTRON INC.
    • Daniel P. SottiauxHunter Davis
    • H01B5/14B64D45/02
    • H01B5/14B64C27/35B64D45/02C09D5/24H05K9/0079
    • A device has a first electrically conductive component, a second electrically conductive component, and an electrically conductive nanocoating (ECN) electrically connecting the first electrically conductive component to the second electrically conductive component. An aircraft has an engine, a fuselage, and a device having a first electrically conductive component, a second electrically conductive component, and an electrically conductive nanocoating (ECN) electrically connecting the first electrically conductive component to the second electrically conductive component. A method of providing an electrical conduction path includes providing a first electrically conductive component, providing a second electrically conductive component, and decreasing an electrical resistance between the first electrically conductive component and the second electrically conductive component using an electrically conductive nanocoating (ECN).
    • 器件具有第一导电部件,第二导电部件和将第一导电部件电连接到第二导电部件的导电纳米涂覆(ECN)。 飞机具有发动机,机身以及具有第一导电部件,第二导电部件和将第一导电部件电连接到第二导电部件的导电纳米涂层(ECN)的装置。 提供导电路径的方法包括提供第一导电部件,提供第二导电部件,以及使用导电纳米涂层(ECN)减小第一导电部件和第二导电部件之间的电阻。