Title:
航空機タイヤ圧力センサ共振ループリンク
Document Type and Number:
Japanese Patent JP6550458
Kind Code:
B2
Abstract:
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.
Inventors:
Lampin, Jeff
Goniyovsky, Igor
Goniyovsky, Igor
Application Number:
JP2017510402A
Publication Date:
July 24, 2019
Filing Date:
August 24, 2015
Export Citation:
Assignee:
Erdec Corporation
International Classes:
G01L17/00; B60C23/02; B60C23/04; B64C25/36
Domestic Patent References:
| JP2011515269A | ||||
| JP2005538625A | ||||
| JP2007145322A | ||||
| JP7230587A | ||||
| JP2002264617A | ||||
| JP2004274754A |
Foreign References:
| WO2013149187A1 | ||||
| US20050046558 | ||||
| US4389884 | ||||
| US20060164214 |
Attorney, Agent or Firm:
Ryoichi Takaoka
Nao Oda
Akiyo Iwahori
Kaoru Takahashi
Nao Oda
Akiyo Iwahori
Kaoru Takahashi