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:
Feb. 28, 2017

Filed:

Jul. 28, 2015
Applicant:

Honeywell International Inc., Morristown, NJ (US);

Inventor:

Bill Macelroy, Greer, SC (US);

Assignee:

HONEYWELL INTERNATIONAL INC., Morris Plains, NJ (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 29/44 (2006.01); F01D 9/04 (2006.01); F01D 25/28 (2006.01);
U.S. Cl.
CPC ...
F01D 9/047 (2013.01); F01D 9/04 (2013.01); F01D 9/041 (2013.01); F01D 25/28 (2013.01); F05D 2220/30 (2013.01); F05D 2230/21 (2013.01); F05D 2230/237 (2013.01); F05D 2240/128 (2013.01); F05D 2270/3061 (2013.01);
Abstract

Embodiments of a method for controllably reducing of the flow area of a turbine nozzle component are provided, as are embodiments of turbine nozzle components having reduced flow areas. In one embodiment, the method includes the steps of obtaining a turbine nozzle component having a plurality of turbine nozzle flow paths therethrough, positioning braze preforms in the plurality of turbine nozzle flow paths and against a surface of the turbine nozzle component, and bonding the braze preforms to the turbine nozzle component to achieve a controlled reduction in the flow area of the turbine nozzle flow paths.


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