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. 24, 2019

Filed:

Jul. 14, 2017
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventor:

Eric J. Ward, West Palm Beach, FL (US);

Assignee:

United Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 11/08 (2006.01); F16J 15/3292 (2016.01); F01D 11/00 (2006.01); F16J 15/00 (2006.01); F16J 15/3232 (2016.01); F01D 5/06 (2006.01); F02C 7/28 (2006.01);
U.S. Cl.
CPC ...
F16J 15/3292 (2013.01); F01D 11/003 (2013.01); F16J 15/002 (2013.01); F16J 15/3232 (2013.01); F01D 5/06 (2013.01); F02C 7/28 (2013.01);
Abstract

A gas turbine engine includes a first rotor shaft and a second rotor shaft around the first rotor shaft. A knife edge seal is radially between the first rotor shaft and the second rotor shaft, and is connected to one of the first rotor shaft or the second rotor shaft. The knife edge seal is sized radially to form a gap between the knife edge seal and the other of the first rotor shaft or the second rotor shaft. A plurality of blades having a general airfoil shape is between the first rotor shaft and the second rotor shaft proximate the knife edge seal. The plurality of blades is connected to the first rotor shaft or the second rotor shaft, and a second gap is formed radially between the plurality of blades and the other of the first rotor shaft or the second rotor shaft.


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