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:
Dec. 26, 2017

Filed:

Oct. 31, 2016
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

John Pietrobon, Outremont, CA;

Remy Synnott, St-Jean-sur-Richelieu, CA;

Assignee:

PRATT & WHITNEY CANADA CORP., Longueuil, QC, CA;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 11/08 (2006.01); F01D 25/12 (2006.01); F01D 9/04 (2006.01); F01D 11/24 (2006.01);
U.S. Cl.
CPC ...
F01D 11/08 (2013.01); F01D 9/041 (2013.01); F01D 11/24 (2013.01); F01D 25/12 (2013.01); F05D 2220/32 (2013.01); F05D 2240/30 (2013.01); F05D 2250/141 (2013.01); F05D 2250/191 (2013.01); F05D 2250/231 (2013.01); F05D 2260/201 (2013.01);
Abstract

An integrated shroud structure surrounds a circumferential array of stator vanes and a circumferential array of rotor blades of a gas turbine engine. The shroud structure includes a plurality of vane shroud segments and a plurality of blade shroud segments. The blade shroud segments integrally extend downstream from the vane shroud segments and each pair of circumferentially adjacent blade shroud segments defines an inter-segment gap. At least one slot extends axially from a location downstream of the vane shroud segments to an aft end of the blade shroud segment. The inter-segment gaps and slots are sealed by a sealing band mounted around the full circumference of the integrated shroud structure.


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