Title:
Airplane tire pressure loop link
Document Type and Number:
Japanese Patent JP6178403
Kind Code:
B2
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.
Inventors:
Lampin, Jeff
Goni Ski, Igal
Goni Ski, Igal
Application Number:
JP2015503660A
Publication Date:
August 09, 2017
Filing Date:
March 29, 2013
Export Citation:
Assignee:
Erdec Corporation
International Classes:
B60C23/04; B64C25/36; G01L17/00
Domestic Patent References:
| JP2011515269A | ||||
| JP5340831A |
Foreign References:
| US20040075022 |
Attorney, Agent or Firm:
Sakaki Morishita
Previous Patent: Freeze-drying of synthetic Liposome lung surfer Kanthant
Next Patent: CURRENT COLLECTOR FOR RAILWAY VEHICLE
Next Patent: CURRENT COLLECTOR FOR RAILWAY VEHICLE