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:
Oct. 12, 2021

Filed:

Apr. 30, 2019
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Mark Eugene Noe, West Chester, OH (US);

Shawn Michael Pearson, Niskayuna, NY (US);

Joshua Tyler Mook, Loveland, OH (US);

Brandon ALlanson Reynolds, Cincinnati, OH (US);

Jonathan David Baldiga, Amesbury, MA (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F23R 3/00 (2006.01); F01D 5/06 (2006.01); F01D 5/22 (2006.01); F01D 9/04 (2006.01); F01D 9/02 (2006.01); F01D 25/24 (2006.01); F02C 3/14 (2006.01); F02C 7/22 (2006.01);
U.S. Cl.
CPC ...
F23R 3/002 (2013.01); F01D 5/06 (2013.01); F01D 5/225 (2013.01); F01D 9/023 (2013.01); F01D 9/04 (2013.01); F01D 25/246 (2013.01); F02C 3/14 (2013.01); F02C 7/22 (2013.01); F05D 2220/32 (2013.01); F05D 2230/53 (2013.01); F05D 2240/35 (2013.01); F05D 2300/6033 (2013.01); F23R 2900/00018 (2013.01); Y02T 50/60 (2013.01);
Abstract

Gas turbine engines, as well as outer walls and flow path assemblies of gas turbine engines, are provided. For example, an outer wall of a flow path comprises a combustor portion extending through a combustion section, and a turbine portion extending through at least a first turbine stage of a turbine section. The combustor and turbine portions are integrally formed as a single unitary structure that defines an outer boundary of the flow path. As another example, a flow path assembly comprises a combustor dome positioned a forward end of a combustor; an outer wall extending from the combustor dome through at least a first turbine stage; and an inner wall extending from the combustor dome through at least a combustion section. The combustor dome extends radially from the outer wall to the inner wall and is integrally formed with the outer and inner walls as a single unitary structure.


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