The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
Mar. 30, 2021

Filed:

Aug. 28, 2017
Applicant:

Hydro-aire, Inc., Burbank, CA (US);

Inventor:

Andrew Brett Slatkin, Tarzana, CA (US);

Assignee:

Hydro-Aire, Inc., Burbank, CA (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 25/42 (2006.01); B60T 8/32 (2006.01); B60T 8/88 (2006.01); B60T 8/172 (2006.01); B60T 17/22 (2006.01); B60T 8/17 (2006.01); F16D 66/02 (2006.01); G01P 3/488 (2006.01); B60T 13/66 (2006.01); B60T 8/171 (2006.01); F16D 66/00 (2006.01);
U.S. Cl.
CPC ...
B60T 8/885 (2013.01); B60T 8/171 (2013.01); B60T 8/1703 (2013.01); B60T 8/1725 (2013.01); B60T 13/662 (2013.01); B60T 17/22 (2013.01); B64C 25/42 (2013.01); F16D 66/028 (2013.01); G01P 3/488 (2013.01); B60T 8/325 (2013.01); B60T 8/329 (2013.01); B60T 2270/413 (2013.01); F16D 2066/003 (2013.01);
Abstract

A wheel speed measuring device for an aircraft braking system uses dual technology packaged in a single transducer that incorporates the robust and reliable variable reluctance technology along with a secondary package for measuring position and velocity bi-directionally for low speed and taxi operations. The transducer of the present invention is preferably incorporated into the envelope of the axle to allow both retrofit on existing aircraft and to maintain existing axle design and configuration.


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