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. 26, 2019

Filed:

Dec. 29, 2014
Applicant:

Hamilton Sundstrand Corporation, Windsor Locks, CT (US);

Inventors:

Craig M. Beers, Wethersfield, CT (US);

Kevin M. Rankin, Windsor, CT (US);

Assignee:

Hamilton Sundstrand Corporation, Charlotte, NC (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
C23C 4/129 (2016.01); B64D 13/08 (2006.01); B64D 13/02 (2006.01); B22D 25/02 (2006.01); F01D 9/04 (2006.01); C23C 4/06 (2016.01); F04D 29/32 (2006.01); B64D 13/06 (2006.01); F04D 25/04 (2006.01);
U.S. Cl.
CPC ...
C23C 4/129 (2016.01); B22D 25/02 (2013.01); B64D 13/02 (2013.01); B64D 13/08 (2013.01); C23C 4/06 (2013.01); F01D 9/045 (2013.01); B64D 2013/0648 (2013.01); F04D 25/04 (2013.01); F04D 29/321 (2013.01); F04D 29/325 (2013.01); F05D 2230/90 (2013.01); F05D 2250/62 (2013.01); F05D 2300/2263 (2013.01);
Abstract

A first stage turbine nozzle includes a first stage hub portion extending axially along a central axis, a first stage disk portion attached to the first stage hub portion and centered on the central axis, and a plurality of first stage vanes positioned radially around and attached to the first stage disk portion. Each vane extends a vane height H away from the first stage disk portion and each vane has a first end positioned at a diameter D away from the central axis. The first stage turbine nozzle also includes a plurality of first stage throats defined between radially adjacent first stage vanes. Each first stage throat has a throat width W between radially adjacent first stage vanes. The first stage turbine nozzle also includes a coating on a sidewall of each first stage vane.


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