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:
Aug. 20, 2019

Filed:

Feb. 23, 2017
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Brandon ALlanson Reynolds, Cincinnati, OH (US);

Aaron Michael Dziech, Dry Ridge, KY (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 9/04 (2006.01); F02C 3/14 (2006.01); F23R 3/00 (2006.01); F01D 5/06 (2006.01); F01D 25/24 (2006.01); F23R 3/10 (2006.01); F23R 3/60 (2006.01); F01D 5/14 (2006.01); F01D 5/28 (2006.01); F01D 9/02 (2006.01);
U.S. Cl.
CPC ...
F02C 3/14 (2013.01); F01D 5/06 (2013.01); F01D 5/143 (2013.01); F01D 5/282 (2013.01); F01D 5/284 (2013.01); F01D 9/023 (2013.01); F01D 9/041 (2013.01); F01D 9/044 (2013.01); F01D 25/24 (2013.01); F01D 25/243 (2013.01); F01D 25/246 (2013.01); F23R 3/002 (2013.01); F23R 3/10 (2013.01); F23R 3/60 (2013.01); F05D 2220/32 (2013.01); F05D 2230/50 (2013.01); F05D 2230/60 (2013.01); F05D 2240/35 (2013.01); F05D 2300/6033 (2013.01); F23R 2900/00017 (2013.01); F23R 2900/00018 (2013.01); Y02T 50/672 (2013.01);
Abstract

Methods for assembling flow path structures having one or more unitary components are provided. For example, one method for assembling a flow path assembly of a gas turbine engine comprises stacking axially adjacent components within a generally annular outer wall of the flow path assembly. The flow path assembly defines a flow path through a combustion section and at least a portion of a turbine section of the gas turbine engine. The outer wall defines an outer boundary of the flow path, and the axially adjacent components defining at least a portion of an inner boundary of the flow path. The outer wall is a unitary outer wall that includes a combustor portion extending through the combustion section and a turbine portion extending through at least a first turbine stage of the turbine section. The combustor and turbine portions are integrally formed as a single unitary structure.


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