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:
Feb. 14, 2017

Filed:

Nov. 27, 2013
Applicant:

Rolls-royce Corporation, Indianapolis, IN (US);

Inventors:

Bronwyn Power, Brownsburg, IN (US);

Roy D. Fulayter, Avon, IN (US);

Jonathan M. Rivers, Indianapolis, IN (US);

Assignee:

Rolls-Royce Corporation, Indianapolis, IN (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 19/02 (2006.01); F01D 5/14 (2006.01); F01D 5/20 (2006.01); F02C 3/00 (2006.01); F02C 9/16 (2006.01);
U.S. Cl.
CPC ...
F04D 19/028 (2013.01); F01D 5/143 (2013.01); F01D 5/20 (2013.01); F02C 3/00 (2013.01); F02C 9/16 (2013.01); F05D 2250/231 (2013.01); F05D 2250/232 (2013.01); F05D 2250/293 (2013.01); F05D 2250/70 (2013.01); Y02T 50/673 (2013.01);
Abstract

A flow path surface of a gas turbine engine at the location of a bladed component is disclosed in which the flow path surface includes a cylindrical upstream side and a conical downstream side. The bladed component is located at the intersection of the cylindrical upstream side and the conical downstream side. The cylindrical upstream side can extend from a leading edge of the bladed component, or a point upstream of it, to a location between the leading edge and trailing edge of the component. The conical downstream side can extend past the trailing edge of the bladed component. The bladed component can be a fan blade or a compressor blade.


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