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. 16, 2026

Filed:

Apr. 04, 2023
Applicant:

Rtx Corporation, Farmington, CT (US);

Inventors:

Michael E. Mccune, Colchester, CT (US);

Jason Husband, South Glastonbury, CT (US);

Frederick M. Schwarz, Glastonbury, CT (US);

Daniel Bernard Kupratis, Wallingford, CT (US);

Gabriel L. Suciu, Glastonbury, CT (US);

William K. Ackermann, East Hartford, CT (US);

Assignee:

RTX CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 3/06 (2006.01); F02C 3/107 (2006.01); F02C 7/36 (2006.01); F04D 29/053 (2006.01);
U.S. Cl.
CPC ...
F02K 3/06 (2013.01); F02C 3/107 (2013.01); F02C 7/36 (2013.01); F04D 29/053 (2013.01); F05D 2240/60 (2013.01); F05D 2260/4031 (2013.01); F05D 2260/40311 (2013.01); F05D 2300/501 (2013.01);
Abstract

A turbofan engine includes a propulsor section that has a propulsor shaft in driving engagement with a propulsor. An epicyclic gear system has a gear mesh lateral stiffness and a gear mesh transverse stiffness. A gear system input defines a gear system input lateral stiffness and a gear system input transverse stiffness. The gear system input lateral stiffness is less than 5% of the gear mesh lateral stiffness. A first turbine section rotates at a first speed, and a second turbine rotates at a second speed that is faster than the first speed. A first performance quantity is defined as the product of the first speed squared and the first area of the first turbine, a second performance quantity is defined as the product of the second speed squared and the second area of the second turbine, and a performance quantity ratio is between 0.5 and 1.5.


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