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:
Aug. 18, 2020

Filed:

Jun. 29, 2018
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Ella Yakobov, Montreal, CA;

James R. Jarvo, Saint Bruno, CA;

Roja Tabar, Longueuil, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 11/30 (2006.01); F02C 9/22 (2006.01); F02C 6/20 (2006.01);
U.S. Cl.
CPC ...
B64C 11/301 (2013.01); F02C 9/22 (2013.01); F02C 6/20 (2013.01); F05D 2260/70 (2013.01); F05D 2260/96 (2013.01); F05D 2270/304 (2013.01); F05D 2270/804 (2013.01);
Abstract

Herein provided are systems and methods for synchrophasing multi-engine aircraft. A phonic wheel is coupled to a first propeller of a first engine of the aircraft. A sensor is disposed and configured for producing a signal in response to passage of first and second position markers on the phonic wheel. A control system is communicatively coupled to the sensor for obtaining the signal, and configured for: determining an expected delay between two subsequent signal pulses of the signal; identifying from within the plurality of signal pulses a particular pulse associated with the second position marker; determining, based on a particular time at which the particular pulse associated with the second position marker was produced, that a rotational position of the first propeller corresponds to a reference position at the particular time; and performing at least one synchrophasing operation for the aircraft based on the rotational position of the first propeller.


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