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:
Apr. 11, 2023

Filed:

Feb. 08, 2021
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Richard Ivakitch, Scarborough, CA;

Daniel Poick, Mississauga, CA;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 17/16 (2006.01); F02C 7/06 (2006.01); F16C 33/04 (2006.01); F16C 33/06 (2006.01); F16C 33/08 (2006.01);
U.S. Cl.
CPC ...
F01D 17/162 (2013.01); F02C 7/06 (2013.01); F16C 33/04 (2013.01); F16C 33/043 (2013.01); F16C 33/06 (2013.01); F16C 33/08 (2013.01); F05D 2220/323 (2013.01); F05D 2240/12 (2013.01); F16C 2208/20 (2013.01); F16C 2208/58 (2013.01); F16C 2208/60 (2013.01); F16C 2360/23 (2013.01);
Abstract

A gas turbine engine, has: an annular gaspath extending around a central axis, the annular gaspath defined between a first casing and a second casing, the first casing defining pockets; and a variable guide vane assembly having: variable guide vanes circumferentially distributed around the central axis, the variable guide vanes having airfoils extending into the annular gaspath and extending between first and second pivot members at respective first and second ends of the airfoils, the variable guide vanes rotatable about respective spanwise axes, bushings received within the pockets of the first casing, the first pivot members of the variable guide vanes rollingly engaged to the bushings, and resilient members disposed radially between surfaces of the first casing and the bushings relative to the spanwise axes, the resilient members in abutment against both of the surfaces of the first casing and the bushings.


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