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:
Apr. 09, 2019

Filed:

Aug. 21, 2014
Applicant:

United Technologies Corporation, Hartford, CT (US);

Inventors:

Matthew Andrew Hough, West Hartford, CT (US);

Jeffrey S. Beattie, South Glastonbury, CT (US);

Assignee:

United Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/14 (2006.01); F01D 11/00 (2006.01); F01D 5/08 (2006.01); F01D 5/30 (2006.01); F01D 11/02 (2006.01); F01D 25/12 (2006.01);
U.S. Cl.
CPC ...
F01D 11/006 (2013.01); F01D 5/081 (2013.01); F01D 5/3015 (2013.01); F01D 11/003 (2013.01); F01D 11/005 (2013.01); F01D 11/008 (2013.01); F01D 11/02 (2013.01); F01D 25/12 (2013.01); F05D 2240/127 (2013.01); F05D 2240/55 (2013.01); F05D 2260/20 (2013.01); F05D 2260/2212 (2013.01);
Abstract

A gas turbine engine includes a turbine section that has a disk rotatable about an axis. The disk has circumferentially-spaced blade mounting features and radially outer rim surfaces extending circumferentially between the blade mounting features. Turbine blades are mounted circumferentially around the disk in the blade mounting features. Seals are arranged radially outwards of the disk adjacent the radially outer rim surfaces such that there are respective passages between the seals and the radially outer rim surfaces. The radially outer rim surfaces include radially-extending protrusions that extend into the respective passages.


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