Aircraft tire pressure loop link
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United States of America Patent
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May 27, 2014
Grant Date -
Mar 21, 2013
app pub date -
Oct 8, 2012
filing date -
Mar 21, 2008
priority date (Note) -
In Force
status (Latency Note)
Importance
Abstract
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.
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