Processing

Please wait...

Settings

Settings

Goto Application

1. WO2013149187 - AIRCRAFT TIRE PRESSURE LOOP LINK

Publication Number WO/2013/149187
Publication Date 03.10.2013
International Application No. PCT/US2013/034675
International Filing Date 29.03.2013
IPC
B60C 23/04 2006.01
BPERFORMING OPERATIONS; TRANSPORTING
60VEHICLES IN GENERAL
CVEHICLE TYRES; TYRE INFLATION; TYRE CHANGING; CONNECTING VALVES TO INFLATABLE ELASTIC BODIES IN GENERAL; DEVICES OR ARRANGEMENTS RELATED TO TYRES
23Devices for measuring, signalling, controlling, or distributing tyre pressure or temperature, specially adapted for mounting on vehicles; Arrangement of tyre inflating devices on vehicles, e.g. of pumps, of tanks; Tyre cooling arrangements
02Signalling devices actuated by tyre pressure
04mounted on the wheel or tyre
CPC
B60C 2200/02
BPERFORMING OPERATIONS; TRANSPORTING
60VEHICLES IN GENERAL
CVEHICLE TYRES TYRE INFLATION; TYRE CHANGING OR REPAIRING; REPAIRING, OR CONNECTING VALVES TO, INFLATABLE ELASTIC BODIES IN GENERAL; DEVICES OR ARRANGEMENTS RELATED TO TYRES
2200Tyres specially adapted for particular applications
02for aircrafts
B60C 23/043
BPERFORMING OPERATIONS; TRANSPORTING
60VEHICLES IN GENERAL
CVEHICLE TYRES TYRE INFLATION; TYRE CHANGING OR REPAIRING; REPAIRING, OR CONNECTING VALVES TO, INFLATABLE ELASTIC BODIES IN GENERAL; DEVICES OR ARRANGEMENTS RELATED TO TYRES
23Devices for measuring, signalling, controlling, or distributing tyre pressure or temperature, specially adapted for mounting on vehicles; Arrangement of tyre inflating devices on vehicles, e.g. of pumps or of tanks; Tyre cooling arrangements
02Signalling devices actuated by tyre pressure
04mounted on the wheel or tyre
0408transmitting the signals by non-mechanical means from the wheel or tyre to a vehicle body mounted receiver
0422characterised by the type of signal transmission means
0427Near field transmission with inductive or capacitive coupling means
043using transformer type signal transducers, e.g. rotary transformers
Applicants
  • ELDEC CORPORATION [US]/[US]
  • LAMPING, Jeff [US]/[US] (US)
  • GONIODSKY, Igal [US]/[US] (US)
Inventors
  • LAMPING, Jeff
  • GONIODSKY, Igal
Agents
  • JAMES W. PAUL
Priority Data
13/436,61630.03.2012US
Publication Language English (EN)
Filing Language English (EN)
Designated States
Title
(EN) AIRCRAFT TIRE PRESSURE LOOP LINK
(FR) LIAISON EN BOUCLE DE PRESSION DE PNEU D'AVION
Abstract
(EN)
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.
(FR)
Liaison en boucle de pression de pneu d'avion formée d'une première et d'une seconde boucle métallique simple raccordées par des axes métalliques espacés et parallèles, et qui procure un couplage de champ magnétique entre un enroulement de moyeu de roue et un enroulement de capteur de pression de pneu pour fournir une communication électromagnétique entre une unité de commande connectée à l'enroulement de moyeu de roue et un capteur de pression de pneu relié à l'enroulement de capteur de pression de pneu. Le courant induit dans la première boucle métallique simple parcourt la distance du bord de l'enroulement d'essieu de roue à la périphérie de la jante de roue vers la seconde boucle de métal unique, qui génère le flux dans l'enroulement de récepteur capteur de pression de pneu nécessaire pour alimenter le capteur de pression de pneu.
Latest bibliographic data on file with the International Bureau