发明名称 |
Aircraft tire pressure loop link |
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. |
申请公布号 |
US8059014(B2) |
申请公布日期 |
2011.11.15 |
申请号 |
US20090409432 |
申请日期 |
2009.03.23 |
申请人 |
LAMPING JEFF;FINEFROCK MARK;ELDEC CORPORATION |
发明人 |
LAMPING JEFF;FINEFROCK MARK |
分类号 |
G08B21/00 |
主分类号 |
G08B21/00 |
代理机构 |
|
代理人 |
|
主权项 |
|
地址 |
|