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:
Jan. 03, 2017

Filed:

Mar. 28, 2014
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Andrew R. Marshall, Grand Valley, CA;

David Menheere, Norval, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F04D 29/56 (2006.01); B33Y 10/00 (2015.01); F01D 5/14 (2006.01); F01D 17/16 (2006.01); F04D 29/02 (2006.01); F04D 29/16 (2006.01); B33Y 80/00 (2015.01); F01D 11/12 (2006.01);
U.S. Cl.
CPC ...
B33Y 10/00 (2014.12); B33Y 80/00 (2014.12); F01D 5/143 (2013.01); F01D 17/162 (2013.01); F04D 29/023 (2013.01); F04D 29/164 (2013.01); F04D 29/563 (2013.01); F01D 11/12 (2013.01); F05D 2230/31 (2013.01); F05D 2300/514 (2013.01); F05D 2300/603 (2013.01); F05D 2300/608 (2013.01); F05D 2300/613 (2013.01); Y10T 29/49245 (2015.01);
Abstract

A variable vane assembly for a gas turbine engine compressor and method of manufacturing same is described. A plurality of projections the inner and/or outer shroud which protruded into the annular gas path such as to ensure that a radial clearance gap, defined between the projections and a vane airfoil overhang portion, remains substantially constant throughout a substantial portion of the vane pivot arc of the variable vane. The method includes forming one cavities within the shroud, the cavities isolated from the annular gas path and disposed radially beneath at least each of the projections, and providing one or more structural reinforcing elements within the cavities.


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