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:
Sep. 12, 2023

Filed:

Oct. 04, 2019
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Lawrence A. Binek, Glastonbury, CT (US);

David W. Morganson, Marlborough, CT (US);

Assignee:

Raytheon Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 9/02 (2006.01); F01D 9/04 (2006.01); F23R 3/00 (2006.01); F23R 3/50 (2006.01); B22F 10/40 (2021.01); B22F 10/64 (2021.01); B33Y 10/00 (2015.01); B33Y 80/00 (2015.01);
U.S. Cl.
CPC ...
F01D 9/044 (2013.01); B22F 10/40 (2021.01); B22F 10/64 (2021.01); F01D 9/023 (2013.01); F01D 9/041 (2013.01); F23R 3/002 (2013.01); F23R 3/50 (2013.01); B33Y 10/00 (2014.12); B33Y 80/00 (2014.12); F05D 2230/30 (2013.01); F05D 2240/12 (2013.01); F05D 2240/35 (2013.01); F05D 2300/1723 (2013.01); F23R 2900/00018 (2013.01);
Abstract

A method of manufacturing a turbine vane within an engine case includes additively manufacturing a combustor liner within an engine case, additively manufacturing a support structure attached to the combustor liner at a radially distal position, and additively manufacturing the turbine vane attached to the support structure at an inwardly adjacent position to the radially distal position.


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