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, 2020

Filed:

Oct. 14, 2016
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Thomas Ory Moniz, Loveland, OH (US);

Daniel Robert Dwyer, West Chester, OH (US);

Mark John Laricchiuta, West Chester, OH (US);

Jeffrey Donald Clements, Mason, OH (US);

Brandon Wayne Miller, Liberty Township, OH (US);

Assignee:

GENERAL ELECTRIC COMPANY, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F04D 29/66 (2006.01); F04D 29/32 (2006.01); F01D 9/04 (2006.01); F04D 29/54 (2006.01); F02C 3/04 (2006.01); F02K 3/06 (2006.01); F04D 29/38 (2006.01); F04D 29/52 (2006.01);
U.S. Cl.
CPC ...
F04D 29/663 (2013.01); F01D 9/041 (2013.01); F02C 3/04 (2013.01); F02K 3/06 (2013.01); F04D 29/324 (2013.01); F04D 29/325 (2013.01); F04D 29/384 (2013.01); F04D 29/522 (2013.01); F04D 29/542 (2013.01); F04D 29/665 (2013.01); F05D 2220/36 (2013.01); F05D 2220/80 (2013.01); F05D 2260/961 (2013.01); Y02T 50/673 (2013.01);
Abstract

A gas turbine engine includes a fan section having a single-stage fan, a core turbine engine, and a nacelle at least partially surrounding the fan of the fan section and the core turbine engine. The gas turbine engine also includes an outlet guide vane extending between a casing of the core turbine engine and the nacelle. The gas turbine engine is configured to define an acoustic ratio greater than or equal to 2.3, with the acoustic ratio being a ratio of an axial spacing between the trailing edge of the fan blade and the leading edge of the outlet guide vane at a radial location seventy-five percent (75%) along the span of the fan blade to the axial width of the fan blade also at the radial location seventy-five percent (75%) along the span of the fan blade.


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