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:
Jul. 12, 2022

Filed:

Nov. 18, 2019
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Winston Gregory Smiddy, Manchester, CT (US);

San Quach, Southington, CT (US);

Matthew D. Parekh, Farmington, CT (US);

Jeffrey T. Morton, Manchester, CT (US);

Assignee:

Raytheon Technologies Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 11/10 (2006.01); F01D 25/14 (2006.01);
U.S. Cl.
CPC ...
F01D 11/10 (2013.01); F01D 25/14 (2013.01); F05D 2240/11 (2013.01); F05D 2250/71 (2013.01); F05D 2260/202 (2013.01);
Abstract

A gas turbine engine includes one of a turbine section and a compressor section having multiple stages. At least one of the stages defines an outer diameter comprised of a plurality of circumferentially arranged blade outer air seals. Each blade outer air seal is spaced from each adjacent blade outer air seal in the plurality of circumferentially arranged blade outer air seals via a mateface gap. The mateface gap is oblique to a radius of the gas turbine engine, such that air entering the mateface gap is directed to an inner diameter surface of at least one of the blade outer air seals in the plurality of blade outer air seals.


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