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:
May. 10, 2022

Filed:

Jun. 26, 2019
Applicants:

Rolls-royce North American Technologies Inc., Indianapolis, IN (US);

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

Inventors:

Linnea Taketa, Indianapolis, IN (US);

John Munson, Indianapolis, IN (US);

Ted J. Freeman, Danville, IN (US);

Assignees:

Rolls-Royce North American Technologies Inc., Indianapolis, IN (US);

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 11/00 (2006.01); F01D 17/16 (2006.01); F04D 27/02 (2006.01); F04D 19/02 (2006.01); F04D 29/16 (2006.01); F01D 5/28 (2006.01); F01D 9/04 (2006.01); F01D 11/02 (2006.01); F01D 17/14 (2006.01); F16J 15/3288 (2016.01); F04D 29/08 (2006.01); F04D 27/00 (2006.01); F01D 11/12 (2006.01);
U.S. Cl.
CPC ...
F01D 11/005 (2013.01); F01D 5/28 (2013.01); F01D 9/041 (2013.01); F01D 11/00 (2013.01); F01D 11/02 (2013.01); F01D 11/025 (2013.01); F01D 17/148 (2013.01); F01D 17/162 (2013.01); F01D 17/165 (2013.01); F04D 19/02 (2013.01); F04D 27/0246 (2013.01); F04D 29/164 (2013.01); F01D 11/122 (2013.01); F04D 27/002 (2013.01); F04D 29/083 (2013.01); F05B 2240/571 (2013.01); F05D 2240/56 (2013.01); F16J 15/3288 (2013.01);
Abstract

A turbomachinery component of a gas turbine engine is disclosed having a number of techniques of reducing the effects of a gap flow between an airfoil member of the gas turbine engine and a wall of the gas turbine engine. The airfoil member can be variable and in one form is a variable turbine vane. In one embodiment a brush seal is included between the vane and the wall. In another form a wear surface is disposed between the vane and the wall. In yet another form a moveable member capable of being actuated to change position can be disposed between the vane and the wall to alter the size of a gap between the two.


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