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11 条记录 (耗时 0.01 秒)

    Light-emitting deceleration and stopping indicator for motor vehicles
    1.
    发明公开
    Light-emitting deceleration and stopping indicator for motor vehicles 失效
    梅尔德惯性转换器，包括传感器及其支持的单元，以及安装变压器的电动车辆的发光减速和停止指示器

    公开(公告)号：EP0299933A3

    公开(公告)日：1990-06-20

    申请号：EP88830297.3

    申请日：1988-07-12

    申请人： B.P.T. S.p.A.

    发明人： Plozner, Lisio

    IPC分类号： H01H29/00 ,  B60Q1/44

    CPC分类号： B60Q1/447 ,  B60Q1/302 ,  G01P15/135 ,  H01H29/002

    摘要： The transducer (10) includes a casing (12) which defines an essentially L-shaped cavity having a substantially horizontal lower arm (16) and a substantially vertical ascending arm (18); a volume of mercury (A) which, in the rest condition, occupies the lower arm (16) and essentially does not occupy the ascending arm (18); an input electrode (30) which penetrates the lower arm (16) from the outside and is permanently immersed in the mercury (A), and a series of separate output electrodes (28₁ ... 28₇) which are spaced along the ascending arm (18) and can be reached in succession by the mercury (A) when it rises in the ascending arm (18) due to an inertial force directed along the lower arm (16) towards the ascending arm (18). The indicator (50) includes an elongate hollow body (52) provided with means (58) for fixing to the bodywork of a motor vehicle and carrying an array of electrical light units (92 1S ...92 6S , 92 1D ...92 6D ) spaced along its length. These units are aligned transverse the vehicle and face rearwardly with respect to the direction of travel. An inertial transducer such as that defined above is mounted in the hollow body (52) and its output electrodes are each connected to at least one of the light units.

    BLUNT IMPACT INDICATOR METHODS
    2.
    发明授权
    BLUNT IMPACT INDICATOR METHODS 有权
    挫伤影响指示剂方法

    公开(公告)号：EP2977737B1

    公开(公告)日：2018-02-14

    申请号：EP15174164.2

    申请日：2015-06-26

    申请人： The Boeing Company

    发明人： GEORGESON, Gary E. ,  TAPIA, William Joseph

    IPC分类号： G01N27/90 ,  B64F5/60 ,  G01M5/00 ,  G01P15/06 ,  H01H29/00 ,  H01H35/14 ,  G01L5/00

    CPC分类号： G01L1/247 ,  B64F5/60 ,  G01L5/0052 ,  G01L5/14 ,  G01M5/0083 ,  G01N3/00 ,  G01N27/90 ,  G01P15/06 ,  H01H29/002 ,  H01H35/146

    摘要： Systems and methods using fluid-filled hollow microspheres to assist in monitoring or indicating high-energy blunt impacts on structures such as aircraft. A multiplicity of microspheres may be adhered to or embedded in a coating applied on a surface of a substrate (e.g., a tape or an appliqué), which substrate in turn can be adhered to a surface of a structure to be monitored. The microspheres are designed to rupture at one or more specified pressure thresholds. In some embodiments, the microspheres are filled with electrically conductive fluid which, if released from ruptured microsphere, changes the electromagnetic state of the substrate. In response to the detection of a sufficiently large change in the electromagnetic state of the substrate, a blunt impact indication is generated. The impact site may then undergo nondestructive inspection.

    Impact switch
    5.
    发明公开
    Impact switch 失效
    冲击开关。

    公开(公告)号：EP0133861A2

    公开(公告)日：1985-03-13

    申请号：EP84100067.2

    申请日：1984-01-04

    申请人： Yeoman, Richard E.

    发明人： Yeoman, Richard E.

    IPC分类号： H01H29/00 ,  H01H35/14

    CPC分类号： H01H29/002

    摘要： A resettable impact switch is disclosed having a housing (12), a first terminal (22) and a second terminal (26) secured to the housing, and a moveable conductor (44) maintained in contact at one end with a reservoir of mercury and at the opposite end with the second terminal (26). The reservoir of mercury is, in turn, in contact with said first terminal (22), allowing the conduction of current through the switch when the moveable conductor (44) is connected to said second terminal (26) and said reservoir of mercury, as during normal operation thereof. Upon a predetermined level of impact imparted to said switch or upon inversion thereof, the connection between the conductor (44) and mercury is broken, thereby opening the switch. The switch is maintained open until a resetting operation is performed. The connection between the opposite end of the conductor can also be broken to de-activate the switch.

    BLUNT IMPACT INDICATOR METHODS
    6.
    发明公开
    BLUNT IMPACT INDICATOR METHODS 审中-公开
    挫伤影响指示剂方法

    公开(公告)号：EP3312580A2

    公开(公告)日：2018-04-25

    申请号：EP17206396.8

    申请日：2015-06-26

    申请人： The Boeing Company

    发明人： GEORGESON, Gary E. ,  TAPIA, William Joseph

    IPC分类号： G01L5/00 ,  B64F5/00 ,  G01N3/00 ,  G01L5/14 ,  G01M5/00 ,  G01N27/20 ,  G01P15/06 ,  H01H29/00 ,  H01H35/14

    CPC分类号： G01L1/247 ,  B64F5/60 ,  G01L5/0052 ,  G01L5/14 ,  G01M5/0083 ,  G01N3/00 ,  G01N27/90 ,  G01P15/06 ,  H01H29/002 ,  H01H35/146

    摘要： Systems and methods using fluid-filled hollow microspheres to assist in monitoring or indicating high-energy blunt impacts on structures such as aircraft. A multiplicity of microspheres may be adhered to or embedded in a coating applied on a surface of a substrate (e.g., a tape or an appliqué), which substrate in turn can be adhered to a surface of a structure to be monitored. The microspheres are designed to rupture at one or more specified pressure thresholds. In some embodiments, the microspheres are filled with electrically conductive fluid which, if released from ruptured microsphere, changes the electromagnetic state of the substrate. In response to the detection of a sufficiently large change in the electromagnetic state of the substrate, a blunt impact indication is generated. The impact site may then undergo nondestructive inspection.

    摘要翻译： 系统和方法使用流体填充空心微球来帮助监测或指示对飞机等结构的高能量钝器冲击。 多个微球体可以粘附或嵌入施加在基底（例如，带或贴花）表面上的涂层中，该基底又可以粘附到待监测的结构的表面。 微球体被设计成在一个或多个指定的压力阈值下破裂。 在一些实施例中，微球体填充有导电流体，如果从破裂的微球体释放，导电流体改变基体的电磁状态。 响应于检测到衬底的电磁状态的足够大的变化，生成钝性冲击指示。 然后影响地点可能会进行无损检查。

    BLUNT IMPACT INDICATOR METHODS
    7.
    发明公开
    BLUNT IMPACT INDICATOR METHODS 有权
    INDIKATORVERFAHRENFÜRSTUMPFEEINSCHLÄGE

    公开(公告)号：EP2977737A2

    公开(公告)日：2016-01-27

    申请号：EP15174164.2

    申请日：2015-06-26

    申请人： The Boeing Company

    发明人： GEORGESON, Gary E. ,  TAPIA, William Joseph

    IPC分类号： G01L5/00 ,  B64F5/00 ,  G01N3/00 ,  G01L5/14 ,  G01M5/00 ,  G01N27/20 ,  G01P15/06 ,  H01H29/00 ,  H01H35/14

    CPC分类号： G01L1/247 ,  B64F5/60 ,  G01L5/0052 ,  G01L5/14 ,  G01M5/0083 ,  G01N3/00 ,  G01N27/90 ,  G01P15/06 ,  H01H29/002 ,  H01H35/146

    摘要： Systems and methods using fluid-filled hollow microspheres to assist in monitoring or indicating high-energy blunt impacts on structures such as aircraft. A multiplicity of microspheres may be adhered to or embedded in a coating applied on a surface of a substrate (e.g., a tape or an appliqué), which substrate in turn can be adhered to a surface of a structure to be monitored. The microspheres are designed to rupture at one or more specified pressure thresholds. In some embodiments, the microspheres are filled with electrically conductive fluid which, if released from ruptured microsphere, changes the electromagnetic state of the substrate. In response to the detection of a sufficiently large change in the electromagnetic state of the substrate, a blunt impact indication is generated. The impact site may then undergo nondestructive inspection.

    摘要翻译： 使用流体填充的中空微球体的系统和方法来协助监测或指示对诸如飞机的结构的高能量钝影响。 多个微球体可以粘附或嵌入施加在基底（例如，带或贴布）的表面上的涂层中，该基底又可以粘附到要监测的结构的表面。 微球被设计为在一个或多个指定的压力阈值下破裂。 在一些实施方案中，微球填充有导电流体，如果从破裂的微球释放，则改变基底的电磁状态。 响应于检测到基板的电磁状态的足够大的变化，产生钝的冲击指示。 然后可以对撞击部位进行非破坏性检查。

    Light-emitting deceleration and stopping indicator for motor vehicles
    8.
    发明公开
    Light-emitting deceleration and stopping indicator for motor vehicles 失效
    LichtaussendendeVerzögerungs-和StopanzeigevorrichtungfürMotorfahrzeuge。

    公开(公告)号：EP0299933A2

    公开(公告)日：1989-01-18

    申请号：EP88830297.3

    申请日：1988-07-12

    申请人： B.P.T. S.p.A.

    发明人： Plozner, Lisio

    IPC分类号： H01H29/00 ,  B60Q1/44

    CPC分类号： B60Q1/447 ,  B60Q1/302 ,  G01P15/135 ,  H01H29/002

    摘要： The transducer (10) includes a casing (12) which defines an essentially L-shaped cavity having a substantially horizontal lower arm (16) and a substantially vertical ascending arm (18); a volume of mercury (A) which, in the rest condition, occupies the lower arm (16) and essentially does not occupy the ascending arm (18); an input electrode (30) which penetrates the lower arm (16) from the outside and is permanently immersed in the mercury (A), and a series of separate output electrodes (28₁ ... 28₇) which are spaced along the ascending arm (18) and can be reached in succession by the mercury (A) when it rises in the ascending arm (18) due to an inertial force directed along the lower arm (16) towards the ascending arm (18).
    The indicator (50) includes an elongate hollow body (52) provided with means (58) for fixing to the bodywork of a motor vehicle and carrying an array of electrical light units (92 1S ...92 6S , 92 1D ...92 6D ) spaced along its length. These units are aligned transverse the vehicle and face rearwardly with respect to the direction of travel. An inertial transducer such as that defined above is mounted in the hollow body (52) and its output electrodes are each connected to at least one of the light units.

    摘要翻译： 传感器（10）包括限定基本上L形的空腔的壳体（12），其具有基本上水平的下臂（16）和基本上垂直的上升臂（18）; 在静止状态下占据下臂（16）并且基本上不占据上臂（18）的一定量的汞（A）; 输入电极（30），其从外部贯穿下臂（16）并永久地浸入在水银（A）中;以及一系列分离的输出电极（281 ... 287），其沿上升臂 18），并且当由于沿着下臂（16）朝向上升臂（18）引导的惯性力而在上升臂（18）中升高时，汞（A）可以连续地达到。 指示器（50）包括细长的中空本体（52），其具有用于固定到机动车辆的车身并且携带一排电子灯单元（921S ... 926S，921D ... 926D）的装置（58） 沿着它的长度。 这些单元横向于车辆并且相对于行进方向向后面对准。 如上所述的惯性换能器安装在中空体（52）中，其输出电极各自连接至至少一个光单元。