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:
Aug. 06, 2019

Filed:

May. 29, 2015
Applicant:

Pratt & Whitney Canada Corp., Longueuil, CA;

Inventors:

Kari Heikurinen, Oakville, CA;

Ron Dutton, Guelph, CA;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/12 (2006.01); F01D 5/14 (2006.01); F04D 29/32 (2006.01); F04D 29/54 (2006.01); F02C 3/04 (2006.01); F04D 19/02 (2006.01); F04D 29/38 (2006.01);
U.S. Cl.
CPC ...
F01D 5/141 (2013.01); F01D 5/142 (2013.01); F02C 3/04 (2013.01); F04D 19/022 (2013.01); F04D 29/324 (2013.01); F04D 29/384 (2013.01); F04D 29/544 (2013.01); F05D 2220/32 (2013.01); F05D 2240/303 (2013.01); F05D 2240/306 (2013.01); F05D 2250/70 (2013.01); F05D 2250/73 (2013.01);
Abstract

A compressor airfoil of a gas turbine engine includes a pressure side and a suction side of the airfoil extending downstream from a stagnation point, the suction side including a suction side surface portion within a leading edge region, and a main suction side airfoil surface downstream from the suction side surface portion and extending contiguously therewith. The suction side surface portion having a compound curvature profile which includes at least a leading edge having a first curvature profile and a chamfered surface having a second curvature profile different from the first curvature profile. The chamfered surface being contiguous with and extending immediately downstream from the leading edge. The first curvature profile being curved. The second curvature profile of the chamfered surface being substantially flat and defining a substantially straight-line profile in a cross-section transverse to the span-wise axis of the airfoil.


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