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    • 4. 发明授权
    • Overvoltage protection element
    • 过电压保护元件
    • US08582264B2
    • 2013-11-12
    • US13023668
    • 2011-02-09
    • Rainer DurthChristian DeppingThomas Meyer
    • Rainer DurthChristian DeppingThomas Meyer
    • H02H3/20
    • H01T1/12H01C7/126
    • An overvoltage protection element with a housing, with at least one overvoltage limiting component which is located in the housing, with terminal elements for electrical connection of the overvoltage protection element to the current or signal path which is to be protected, and with a state display which has a display element for display of the state of the overvoltage protection element. A conclusion about the state of the overvoltage protection element is easily possible as a result of a thermally activatable, endothermic material being both in thermal contact with the overvoltage limiting component and also in mechanical contact with the display element of the state display. When the overvoltage limiting component is heated above a certain minimum temperature, expansion of the thermally activatable, endothermic material produces a change in position of the display element whose magnitude is a measure of the heating of the overvoltage limiting component.
    • 具有壳体的过电压保护元件,其具有位于壳体中的至少一个过电压限制部件,具有用于将过电压保护元件电连接到待保护的电流或信号路径的端子元件,并具有状态显示 其具有用于显示过电压保护元件的状态的显示元件。 由于可热激活的吸热材料与过电压限制部件热接触并且还与状态显示器的显示元件机械接触,所以关于过电压保护元件的状态的结论是容易的。 当过电压限制部件被加热到特定的最低温度以上时,可热活化的吸热材料的膨胀产生显示元件的位置变化,其大小是过电压限制部件的加热的量度。
    • 7. 发明申请
    • OVERVOLTAGE PROTECTION ELEMENT
    • 过电压保护元件
    • US20120229246A1
    • 2012-09-13
    • US13508219
    • 2010-11-05
    • Christian DeppingRainer DurthGernot FinisThomas MeyerAndreas Christ
    • Christian DeppingRainer DurthGernot FinisThomas MeyerAndreas Christ
    • H01H71/14
    • H01H37/36H01C7/12H01C7/126H01H1/20H01H37/04H01H37/46H01H37/74H01H37/767H01H2037/769H01T1/14
    • An overvoltage protection element with a housing, an overvoltage-limiting component arranged in the housing, and with two connection elements for electrically connecting the overvoltage protection element to the current or signal path to be protected, wherein, normally, the connection elements are each in electrically conductive contact with a pole of the overvoltage-limiting component. Reliable and effective electrical connection in the normal state and reliable isolation of a defective overvoltage-limiting component are ensured by the fact that a thermally expandable material is arranged within the housing in a way that, in the event of thermal overloading of the overvoltage-limiting component, the position of the overvoltage-limiting component is changed by expansion of the thermally expandable material relative to the position of the connection elements in a way that causes at least one pole of the overvoltage-limiting component to be out of electrically conductive contact with the corresponding connection element.
    • 具有壳体的过电压保护元件,布置在壳体中的过电压限制部件,以及用于将过电压保护元件电连接到待保护的电流或信号路径的两个连接元件,其中通常,连接元件分别位于 与过电压限制部件的极导电接触。 通过以下事实来确保正常状态下的可靠和有效的电连接以及有缺陷的过电压限制部件的可靠隔离:将热可膨胀材料布置在壳体内,使得在过压限制 通过使可热膨胀材料相对于连接元件的位置的膨胀以过电压限制部件的至少一极极脱离导电接触的方式改变过电压限制部件的位置 相应的连接元素。
    • 9. 发明授权
    • Aircraft provided with a tail plane including means for combating flutter
    • 飞机配备了一个尾翼,包括防止颤振的手段
    • US08814083B2
    • 2014-08-26
    • US13274544
    • 2011-10-17
    • Rodolphe LhermenaultThomas MeyerJean AzeauJulien Guitton
    • Rodolphe LhermenaultThomas MeyerJean AzeauJulien Guitton
    • B64C9/00
    • B64C1/26B64C2027/8281
    • An aircraft (1) provided with a tail boom (4) including a tail plane (100) provided with an airfoil surface (5), the airfoil surface (5) being provided with at least one stabilizer portion (11, 12) extending laterally outside the tail boom (4) and with a central portion (13) extending inside the tail boom (4), said stabilizer portion (11, 12) being implanted in an orifice (6, 7) of the tail boom (4) that is defined by a peripheral wall (6′, 7′), clearance (21, 22) existing between said stabilizer portion (11, 12) and said peripheral wall (6, 7). The aircraft includes combating means (30) for combating the flutter phenomenon, which means are provided with stiffener means (31, 32) exerting predetermined compressive stress on said stabilizer portion (11, 12), said stiffener means (31, 32) being arranged at the root of the stabilizer portion (11, 12).
    • 一种设置有尾悬臂(4)的飞行器(1),其包括设置有翼型表面(5)的尾翼(100),所述翼型表面(5)设置有至少一个侧向延伸的稳定器部分(11,12) 在尾悬臂(4)外部并且具有在尾悬臂(4)内部延伸的中心部分(13),所述稳定器部分(11,12)被植入尾部吊杆(4)的孔口(6,7)中, 由位于所述稳定器部分(11,12)和所述周壁(6,7)之间的周壁(6',7'),间隙(21,22)限定。 该飞机包括用于防止颤振现象的装置(30),该装置具有在所述稳定器部分(11,12)上施加预定压缩应力的加强装置(31,32),所述加强装置(31,32)被布置 在稳定器部分(11,12)的根部处。