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:
Nov. 26, 2019

Filed:

Jan. 19, 2017
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Thomas Veitch, Toronto, CA;

Karan Anand, Mississauga, CA;

Peter Townsend, Mississauga, CA;

Tibor Urac, Mississauga, CA;

Terry Brownridge, St-Lambert, CA;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F04D 29/52 (2006.01); F04D 29/16 (2006.01); F04D 29/32 (2006.01); F04D 29/64 (2006.01); F04D 29/68 (2006.01);
U.S. Cl.
CPC ...
F04D 29/526 (2013.01); F04D 29/164 (2013.01); F04D 29/324 (2013.01); F04D 29/644 (2013.01); F04D 29/685 (2013.01); F05D 2250/294 (2013.01); F05D 2250/61 (2013.01);
Abstract

A gas turbine engine is described having a rotor with a plurality of rotor blades each extending radially between a blade root to a blade tip and axially between a leading edge and a trailing edge. An annular casing body housing the rotor blades includes an abradable segment of the inner surface facing the blade tips and having an abradable member. The abradable segment having one or more annular grooves, extending into the casing body from an inner surface thereof, and including an edge groove axially aligned with and facing the leading edge or the trailing edge of the rotor blades. The edge groove extends axially between a first position on the inner surface upstream of the leading edge or the trailing edge, and a second position on the inner surface downstream of the leading edge or the trailing edge.


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