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    AIRCRAFT TIRE PRESSURE LOOP LINK
    1.
    发明公开
    AIRCRAFT TIRE PRESSURE LOOP LINK 有权
    飞机轮胎压力磨削-LINK

    公开(公告)号：EP2271506A2

    公开(公告)日：2011-01-12

    申请号：EP09722476.0

    申请日：2009-03-23

    申请人： Eldec Corporation

    发明人： LAMPING, Jeff ,  FINEFROCK, Mark

    IPC分类号： B60C23/00 ,  G08B21/00

    CPC分类号： B60C23/0408 ,  B60C23/0413 ,  B60C23/0427 ,  B60C23/043 ,  B60C2200/02

    摘要： The aircraft tire pressure loop link is formed of first and second single metal loops connected by parallel spaced apart metal shafts, and provides for coupling a magnetic field between a wheel hub coil and a tire pressure sensor coil to provide electromagnetic communication between a control unit connect to the wheel hub coil and a tire pressure sensor connected to the tire pressure sensor coil. The current induced in the first single metal loop travels the distance from the edge of the wheel axle coil to the periphery of the of the wheel rim to the second single metal loop, which generates the flux in the tire pressure sensor receiver coil necessary to power the tire pressure sensor.

    AIRCRAFT TIRE PRESSURE SENSOR RESONANT LOOP LINK
    2.
    发明公开
    AIRCRAFT TIRE PRESSURE SENSOR RESONANT LOOP LINK 有权
    飞机轮胎压力传感器共振环链路

    公开(公告)号：EP3186098A1

    公开(公告)日：2017-07-05

    申请号：EP15760334.1

    申请日：2015-08-24

    申请人： Eldec Corporation

    发明人： LAMPING, Jeff ,  GONIODSKY, Igal

    IPC分类号： B60C23/04

    CPC分类号： B60C23/043 ,  B60C2200/02

    摘要： The aircraft tire pressure resonant loop link assembly electromagnetically couples a magnetic field between a wheel axle electromagnetic adapter transformer primary coil and a tire pressure sensor receiver coil for powering a tire pressure sensor, and includes a pair of spaced apart electrically conductive connecting arms, a single electrically conductive primary loop electrically connected to first ends of the connecting arms mounted adjacent to a secondary tire pressure sensor coil, and a circuit including a resonant tuning capacitor and a secondary coil with one or more electrically conductive loops at second ends of the connecting arms. The tire pressure sensor coil pair includes a transformer core, and secondary resonant coil pair also includes a transformer core.

    摘要翻译： 飞机轮胎压力谐振环路连杆组件电磁地耦合轮轴电磁适配器变压器初级线圈和用于为轮胎压力传感器供电的轮胎压力传感器接收器线圈之间的磁场，并且包括一对间隔开的导电连接臂，单个 电连接到与次级轮胎压力传感器线圈相邻安装的连接臂的第一端的导电主回路，以及包括谐振调谐电容器和次级线圈的电路，所述次级线圈在连接臂的第二端具有一个或多个导电回路。 轮胎压力传感器线圈对包括变压器芯，次级谐振线圈对还包括变压器芯。

    INDUCTIVE PROXIMITY SENSOR FOR DETECTING FERROMAGNETIC, NON-PERMEABLE OR MAGNET TARGETS
    4.
    发明授权
    INDUCTIVE PROXIMITY SENSOR FOR DETECTING FERROMAGNETIC, NON-PERMEABLE OR MAGNET TARGETS 无效
    接近传感器控制对于磁体，铁磁的或可渗透的目的地

    公开(公告)号：EP1264404B1

    公开(公告)日：2003-08-27

    申请号：EP01914594.5

    申请日：2001-02-28

    申请人： ELDEC CORPORATION

    发明人： WOOLSEY, Kevin ,  LAMPING, Jeff ,  MARLER, John ,  BURRESON, Bernie ,  KNUDSON, Steve

    IPC分类号： H03K17/95

    CPC分类号： G01B7/023 ,  H03K2217/94021

    摘要： A core (120; 120'; or 1220) of a proximity sensor (100; 1200; or 1500) is made of a highly permeable metal and is shaped and sized to operate as a saturable core proximity sensor, a variable reluctance proximity sensor, and an eddy current proximity sensor. The core (120; 120'; or 1220) has a cross-sectional shape including a head portion (220 or 1231), two legs (222 or 1232) extending from the head portion (220 or 1231), and two foot portions (224 or 1233) (feet) extending from the two legs (222 or 1232). The head portion (220 or 1231) forms a substantially planar section along the upper surface and is perpendicular to the sectional direction created by the two legs (222 or 1232). The sectional direction of the two legs (222 or 1232) are perpendicular to the sectional direction of the two feet (224 or 1233). The two feet (224 or 1233) are in a common plane along the bottom surface. Both foot portions are also parallel to the head portion. The cross-sectional shape of the core may further comprise two tail portions (1234) (tails), wherein each tail extends from one of the two foot (1233) portions in a direction toward the upper surface (1221).

    AIRCRAFT TIRE PRESSURE SENSOR RESONANT LOOP LINK
    6.
    发明授权
    AIRCRAFT TIRE PRESSURE SENSOR RESONANT LOOP LINK 有权

    公开(公告)号：EP3186098B1

    公开(公告)日：2018-06-20

    申请号：EP15760334.1

    申请日：2015-08-24

    申请人： Eldec Corporation

    发明人： LAMPING, Jeff ,  GONIODSKY, Igal

    IPC分类号： B60C23/04

    CPC分类号： B60C23/043 ,  B60C2200/02

    摘要： The aircraft tire pressure resonant loop link assembly electromagnetically couples a magnetic field between a wheel axle electromagnetic adapter transformer primary coil and a tire pressure sensor receiver coil for powering a tire pressure sensor, and includes a pair of spaced apart electrically conductive connecting arms, a single electrically conductive primary loop electrically connected to first ends of the connecting arms mounted adjacent to a secondary tire pressure sensor coil, and a circuit including a resonant tuning capacitor and a secondary coil with one or more electrically conductive loops at second ends of the connecting arms. The tire pressure sensor coil pair includes a transformer core, and secondary resonant coil pair also includes a transformer core.

    AIRCRAFT TIRE PRESSURE LOOP LINK
    7.
    发明公开
    AIRCRAFT TIRE PRESSURE LOOP LINK 审中-公开
    DRUCKREGELKREISVERBINDUNGFÜRFLUGZEUGREIFEN

    公开(公告)号：EP2830893A1

    公开(公告)日：2015-02-04

    申请号：EP13718429.7

    申请日：2013-03-29

    申请人： Eldec Corporation

    发明人： LAMPING, Jeff ,  GONIODSKY, Igal

    IPC分类号： B60C23/04

    摘要： The aircraft tire pressure loop link is formed of first and second single metal loops connected by parallel spaced apart metal shafts, and provides for coupling a magnetic field between a wheel hub coil and a tire pressure sensor coil to provide electromagnetic communication between a control unit connect to the wheel hub coil and a tire pressure sensor connected to the tire pressure sensor coil. The current induced in the first single metal loop travels the distance from the edge of the wheel axle coil to the periphery of the of the wheel rim to the second single metal loop, which generates the flux in the tire pressure sensor receiver coil necessary to power the tire pressure sensor.

    摘要翻译： 飞机轮胎压力回路连杆由平行间隔开的​​金属轴连接的第一和第二单个金属环形成，并且提供在轮毂线圈和轮胎压力传感器线圈之间耦合磁场，以提供控制单元连接之间的电磁通信 轮毂线圈和连接到轮胎压力传感器线圈的轮胎压力传感器。 在第一单个金属环中感应的电流从轮轴线圈的边缘到轮缘的周边的距离移动到第二单个金属环，其在轮胎压力传感器接收器线圈中产生通量，该通量需要功率 轮胎压力传感器。

    INDUCTIVE PROXIMITY SENSOR FOR DETECTING FERROMAGNETIC, NON-PERMEABLE OR MAGNET TARGETS
    8.
    发明公开
    INDUCTIVE PROXIMITY SENSOR FOR DETECTING FERROMAGNETIC, NON-PERMEABLE OR MAGNET TARGETS 无效
    接近传感器控制对于磁体，铁磁的或可渗透的目的地

    公开(公告)号：EP1264404A2

    公开(公告)日：2002-12-11

    申请号：EP01914594.5

    申请日：2001-02-28

    申请人： ELDEC CORPORATION

    发明人： WOOLSEY, Kevin ,  LAMPING, Jeff ,  MARLER, John ,  BURRESON, Bernie ,  KNUDSON, Steve

    IPC分类号： H03K17/95

    CPC分类号： G01B7/023 ,  H03K2217/94021

    摘要： A core (120; 120'; or 1220) of a proximity sensor (100; 1200; or 1500) is made of a highly permeable metal and is shaped and sized to operate as a saturable core proximity sensor, a variable reluctance proximity sensor, and an eddy current proximity sensor. The core (120; 120'; or 1220) has a cross-sectional shape including a head portion (220 or 1231), two legs (222 or 1232) extending from the head portion (220 or 1231), and two foot portions (224 or 1233) (feet) extending from the two legs (222 or 1232). The head portion (220 or 1231) forms a substantially planar section along the upper surface and is perpendicular to the sectional direction created by the two legs (222 or 1232). The sectional direction of the two legs (222 or 1232) are perpendicular to the sectional direction of the two feet (224 or 1233). The two feet (224 or 1233) are in a common plane along the bottom surface. Both foot portions are also parallel to the head portion. The cross-sectional shape of the core may further comprise two tail portions (1234) (tails), wherein each tail extends from one of the two foot (1233) portions in a direction toward the upper surface (1221).