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:
Apr. 16, 2019

Filed:

Sep. 09, 2016
Applicant:

Eaton Intelligent Power Limited, Dublin, IE;

Inventors:

John David Neely, Kentwood, MI (US);

John Mendenhall White, Strasburg, VA (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
H02P 6/17 (2016.01); H02P 6/00 (2016.01); H02P 23/14 (2006.01); F04B 49/20 (2006.01); F04B 49/06 (2006.01);
U.S. Cl.
CPC ...
H02P 6/17 (2016.02); F04B 49/20 (2013.01); H02P 6/00 (2013.01); H02P 23/14 (2013.01); F04B 49/065 (2013.01); H02P 2205/07 (2013.01);
Abstract

A system comprises an aircraft hydraulic system motor, a position sensor, and a programmable controller. The aircraft hydraulic system motor includes a rotor whose position is detected by the position sensor. The position sensor produces an output representative of that position. The programmable controller is configured to receive the output of the position sensor and calculate an estimated velocity of the aircraft hydraulic system motor based on the output of the position sensor. The calculation of the estimated velocity comprises determining both a high bandwidth velocity estimation and a low bandwidth velocity estimation. The programmable controller is additionally configured to compare the estimated velocity to a desired velocity and direct the aircraft hydraulic system motor to increase or decrease velocity based on the comparison.


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