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. 03, 2019

Filed:

Jun. 09, 2016
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Lazar Mitrovic, Longueuil, CA;

Keith Morgan, Westmount, CA;

Assignee:

PRATT & WHITNEY CANADA CORP., Longueuil, QC, CA;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F16H 1/20 (2006.01); F02C 7/36 (2006.01); B64D 35/00 (2006.01);
U.S. Cl.
CPC ...
F16H 1/20 (2013.01); B64D 35/00 (2013.01); F02C 7/36 (2013.01); F05D 2260/4031 (2013.01);
Abstract

A reduction gearbox for an aircraft engine, including an input pinion configured to be driven by the aircraft engine, a input gear meshed with the input pinion, a drive gear meshed with the input gear, an output pinion, and an output gear meshed with the output pinion and configured to drive an output shaft of the aircraft engine. The reduction gearbox is selectively configurable between an engaged configuration where the input gear and output pinion are drivingly engaged and a disengaged configuration where the input gear is rotatable independently of the output pinion. The output shaft may drive a propeller and the gearbox may include a propeller brake. A method of driving a generator of a turboprop engine is also discussed.


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