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:
Jul. 05, 2022

Filed:

Mar. 27, 2020
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventor:

Lazar Mitrovic, Longueuil, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16H 1/28 (2006.01); B64C 11/46 (2006.01); B64D 35/02 (2006.01); F02C 7/36 (2006.01); F16H 57/02 (2012.01); F16H 57/08 (2006.01); F16H 1/32 (2006.01);
U.S. Cl.
CPC ...
B64C 11/46 (2013.01); B64D 35/02 (2013.01); F02C 7/36 (2013.01); F16H 1/28 (2013.01); F16H 57/02 (2013.01); F16H 57/08 (2013.01); F05D 2220/323 (2013.01); F05D 2260/40311 (2013.01); F16H 1/32 (2013.01); F16H 2001/2872 (2013.01); F16H 2057/02043 (2013.01);
Abstract

An aircraft includes first and second engines, one or more aircraft rotors associated with the first and second engines, a first epicyclic gearbox having: a) an output operatively connected at least one of the one or more aircraft rotors, and b) an input defined by a sun gear of the first epicyclic gearbox; and a second epicyclic gearbox having: a) an output operatively connected to at least one of the one or more aircraft rotors, and b) an input defined by a sun gear of the second epicyclic gearbox. Output of the first epicyclic gearbox is defined by the carrier. Output of the second epicyclic gearbox is defined by its ring gear. A multi-engine aircraft and a method of operating a multi-engine aircraft are also described.


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