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:
Jun. 14, 2022

Filed:

Dec. 20, 2018
Applicant:

United Technologies Corporation, Farmington, CT (US);

Inventors:

Dennis M. Moura, South Windsor, CT (US);

Carey Clum, East Hartford, CT (US);

Assignee:

RAYTHEON TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F23R 3/00 (2006.01); F23M 5/08 (2006.01); F23M 5/04 (2006.01); F23R 3/60 (2006.01);
U.S. Cl.
CPC ...
F23R 3/002 (2013.01); F23M 5/04 (2013.01); F23M 5/08 (2013.01); F23R 3/60 (2013.01); F05D 2240/35 (2013.01); F05D 2260/201 (2013.01); F05D 2260/607 (2013.01); F23R 2900/00004 (2013.01); F23R 2900/00017 (2013.01); F23R 2900/03043 (2013.01); F23R 2900/03044 (2013.01); F23R 2900/03045 (2013.01);
Abstract

A gas turbine engine component assembly is provided. The gas turbine engine component assembly comprising: a first component having a first surface and a second surface; a threaded stud including a first end and a second end opposite the first end, the threaded stud extending from the second surface of the first component; and a faired body operably secured to the threaded stud, wherein the faired body is shaped to redirect the airflow in a lateral direction parallel to the second surface of the first component such that a cross flow is generated.


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