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:
Jun. 01, 2021

Filed:

Feb. 12, 2019
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Marc-Antoine Mailloux-Labrousse, Montreal, CA;

Othmane Leghzaouni, Brossard, CA;

Yves Roussel, Varennes, CA;

Max Bergeron-Fillion, St-Hubert, CA;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/30 (2006.01); F01D 25/28 (2006.01);
U.S. Cl.
CPC ...
F01D 5/3023 (2013.01); F01D 25/285 (2013.01); F05D 2220/32 (2013.01); F05D 2230/60 (2013.01); F05D 2240/24 (2013.01); F05D 2260/12 (2013.01); F05D 2260/36 (2013.01); F05D 2260/83 (2013.01);
Abstract

The gas turbine engine can have a first and second rotary components structurally joined to one another via a connector, a first spigot fit between the connector and the first rotary component, the first spigot fit forming an interference fit at a first operating condition and forming a gap at a second operating condition, a second spigot fit between the connector and the first rotary component, the second spigot fit forming an interference fit at the second operating condition and forming a gap at the first operating condition, the gas turbine engine being further configured to form a radial interference fit between the connector and the second rotary component in both the first and second operating conditions.


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