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:
Jun. 09, 2026

Filed:

Sep. 07, 2023
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Daniel Alecu, Brampton, CA;

David Menheere, Norval, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 3/06 (2006.01); F02C 3/067 (2006.01); F02C 3/14 (2006.01); F02C 7/143 (2006.01); F02C 7/36 (2006.01); F02C 9/18 (2006.01); F02K 1/12 (2006.01); F02K 3/072 (2006.01); F02K 3/077 (2006.01);
U.S. Cl.
CPC ...
F02C 3/06 (2013.01); F02C 3/145 (2013.01); F02C 7/143 (2013.01); F02C 7/36 (2013.01); F02C 9/18 (2013.01); F02K 1/1207 (2013.01); F02K 3/072 (2013.01); F02K 3/077 (2013.01); F02C 3/067 (2013.01); F05D 2260/213 (2013.01); F05D 2260/40311 (2013.01); F05D 2260/606 (2013.01);
Abstract

Dual bypass gas turbine engines and associated methods are provides. A dual bypass turbofan gas turbine engine includes counter-rotating first and second fans through which ambient air is received and propelled in an aft direction; a first bypass duct receiving first bypass air including a first portion of the propelled air; a second bypass duct receiving second bypass air including a second portion of the propelled air; a core gas path receiving core air including a third portion of the propelled air; a compressor pressurizing the core air; an intercooler facilitating heat removal from the pressurized core air; a combustor in which the pressurized core air is mixed with fuel and ignited to generate a stream of combustion gas; a turbine extracting energy from the combustion gas; and a differential gear train apportioning an input torque received from the turbine between the first fan and the second fan.


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