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:
Oct. 13, 2020

Filed:

Aug. 01, 2016
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Kevin W. White, Jupiter, FL (US);

Henry K. Webster, Jupiter, FL (US);

Jonathan Ariel Scott, Southington, CT (US);

Randall J. Brown, East Windsor, CT (US);

Alan D. Lees, Manchester, CT (US);

Assignee:

Raytheon Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 11/00 (2006.01); F16J 15/08 (2006.01); F01D 9/02 (2006.01); F02C 3/14 (2006.01); F02C 7/28 (2006.01);
U.S. Cl.
CPC ...
F01D 11/003 (2013.01); F01D 9/023 (2013.01); F01D 11/005 (2013.01); F02C 3/14 (2013.01); F02C 7/28 (2013.01); F16J 15/0887 (2013.01); F05D 2220/32 (2013.01); F05D 2230/60 (2013.01); F05D 2240/35 (2013.01); Y02T 50/672 (2013.01); Y02T 50/675 (2013.01);
Abstract

An annular finger seal includes a base portion defining a base edge of the annular finger seal and having a center pass-through aperture. The base edge may be substantially continuous. The annular finger seal may also include a finger portion defining a finger edge of the annular finger seal and including a plurality of fingers. The finger edge may be segmented by gaps disposed between adjacent fingers of the plurality of fingers. A gas turbine engine includes a combustor section, a turbine section, and an annular finger seal. The annular finger seal includes a plurality of fingers and the annular finger seal is disposed at an adjoining interface between the combustor section and the turbine section. The annular finger seal may be mounted to the turbine section and may engage a radially inward facing surface, relative to the engine central longitudinal axis, of the combustor section.


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