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:
Sep. 13, 2016

Filed:

Jul. 29, 2014
Applicant:

Goodrich Corporation, Charlotte, NC (US);

Inventor:

Brian Keith Zell, Dayton, OH (US);

Assignee:

GOODRICH CORPORATION, Charlotte, NC (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 25/42 (2006.01); G01D 5/22 (2006.01); G01R 19/00 (2006.01); B60T 7/04 (2006.01); B60T 8/17 (2006.01); B60T 8/32 (2006.01);
U.S. Cl.
CPC ...
B64C 25/42 (2013.01); B60T 7/042 (2013.01); B60T 8/1703 (2013.01); B60T 8/325 (2013.01); G01D 5/2291 (2013.01); G01R 19/0084 (2013.01);
Abstract

An aircraft brake system may include a linear variable differential transformer ('LVDT'). A brake control unit ('BCU') may measure an output voltage from the LVDT. The BCU may include a hardware module, a software module, and an offset module. The hardware module may include a preprogrammed threshold voltage. The output voltage may be measured, and an offset voltage may be determined and stored in the offset module. The software module may measure the sum of the output voltage and the offset voltage. In response to the hardware module and the software module indicating that the threshold voltage has been reached, the BCU may allow braking of the aircraft.


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