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. 14, 2020

Filed:

Jan. 16, 2018
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Jason Elliott, Huntington, IN (US);

Daniel C. Falk, Middletown, CT (US);

Myron L. Klein, Higganum, CT (US);

Assignee:

Raytheon Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/16 (2006.01); F01D 5/26 (2006.01); F01D 5/28 (2006.01); F01D 25/06 (2006.01); F02K 3/06 (2006.01);
U.S. Cl.
CPC ...
F01D 5/26 (2013.01); F01D 5/16 (2013.01); F01D 5/28 (2013.01); F01D 25/06 (2013.01); F02K 3/06 (2013.01); F05D 2220/323 (2013.01); F05D 2220/3212 (2013.01); F05D 2230/00 (2013.01); F05D 2240/24 (2013.01); F05D 2260/96 (2013.01); F05D 2300/173 (2013.01); F05D 2300/174 (2013.01);
Abstract

In one exemplary embodiment, a turbofan engine comprises a fan section. A core section includes a turbine section arranged fluidly downstream from the compressor section. A combustor is arranged fluidly between the compressor and turbine sections. The fan and core sections are configured to produce a thrust in a range 27,000-35,000 pounds-f (120,102-156,688 N). An airfoil is arranged in the fan section. The airfoil has first and second modes each having a frequency. The first mode has the lowest frequency, and the second mode has the second lowest frequency wherein the second mode frequency is 140 Hz or less at a redline engine speed.


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