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:
Jan. 23, 2024

Filed:

Sep. 30, 2022
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

Daniel S. Rogers, Lyman, ME (US);

Timothy J. Harding, Wethersfield, CT (US);

Joseph Micucci, Scarborough, ME (US);

Paul M. Lutjen, Kennebunkport, ME (US);

Assignee:

RTX Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 11/12 (2006.01); F01D 25/00 (2006.01);
U.S. Cl.
CPC ...
F01D 11/12 (2013.01); F01D 25/005 (2013.01); F05D 2240/56 (2013.01); F05D 2250/38 (2013.01); F05D 2260/30 (2013.01); F05D 2300/6033 (2013.01);
Abstract

There is a blade outer air seal positioned to be radially outward of blades in the rotating blade row relative to the rotational axis. There is at least one brush seal having bristles extending from a mount location radially inward to contact a sealing surface on the blade outer air seal. An angle is defined between the bristles and relative to the sealing surface having a radially inward extending component, and with an axial component in a direction toward a leading edge attachment feature and a trailing edge attachment feature, and the angle is less than 90° on a side of the brush seal opposite the leading edge and trailing edge mount hooks. A gas turbine engine component is also disclosed.


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