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. 19, 2021

Filed:

Apr. 08, 2019
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Daniel Patrick Kerns, Mason, OH (US);

Brandon Alianson Reynolds, Cincinnati, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 11/04 (2006.01); F23R 3/00 (2006.01); F01D 9/04 (2006.01); F01D 25/12 (2006.01); F01D 25/00 (2006.01); F02C 3/14 (2006.01); F01D 9/02 (2006.01); F23R 3/50 (2006.01); F01D 11/00 (2006.01); F23R 3/60 (2006.01);
U.S. Cl.
CPC ...
F01D 11/04 (2013.01); F01D 9/023 (2013.01); F01D 9/041 (2013.01); F01D 9/042 (2013.01); F01D 11/005 (2013.01); F01D 25/005 (2013.01); F01D 25/12 (2013.01); F02C 3/14 (2013.01); F23R 3/002 (2013.01); F23R 3/50 (2013.01); F23R 3/60 (2013.01); F05D 2220/32 (2013.01); F05D 2240/35 (2013.01); F05D 2260/20 (2013.01); F05D 2300/6033 (2013.01); F23R 2900/00018 (2013.01); Y02T 50/60 (2013.01);
Abstract

Flow path assemblies for gas turbine engines are provided. For example, a flow path assembly comprises an inner wall defining an inner boundary of a flow path and a plurality of pockets therein, and a unitary outer wall defining an outer boundary of the flow path. The unitary outer wall includes combustor and turbine portions that are integrally formed as a single unitary structure. The flow path assembly further comprises a plurality of nozzle airfoils that each have an inner end radially opposite an outer end and define an internal cavity for receipt of a flow of cooling fluid. The inner end of each nozzle airfoil is received in one of the plurality of inner wall pockets and defines an outlet for the flow of cooling fluid to flow from the internal cavity to the pocket, which forms a fluid curtain to discourage fluid leakage from the flow path.


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