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:
Nov. 08, 2022

Filed:

Jan. 10, 2020
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

Brandon W. Spangler, Vernon, CT (US);

Carey Clum, East Hartford, CT (US);

Matthew A. Devore, Rocky Hill, CT (US);

Assignee:

RAYTHEON TECHNOLOGIES CORPORATION, Farmington, CT (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/18 (2006.01); F01D 9/06 (2006.01); F02C 7/18 (2006.01);
U.S. Cl.
CPC ...
F01D 5/186 (2013.01); F01D 5/188 (2013.01); F01D 5/189 (2013.01); F01D 9/065 (2013.01); F02C 7/18 (2013.01); F05D 2240/122 (2013.01); F05D 2260/20 (2013.01); F05D 2260/202 (2013.01); F05D 2260/2212 (2013.01); Y02T 50/60 (2013.01);
Abstract

A gas turbine engine component comprises a body having a leading edge, a trailing edge, and a radial span. One internal channel in the body provides an upstream supply pressure. Another internal channel in body receives the upstream supply pressure and provides a downstream supply pressure. At least one axial rib separates an internal area adjacent to the trailing edge into a plurality of individual cavities. At least one pressure regulating feature is located at an entrance to at least one individual cavity entrance to control downstream supply pressure to the trailing edge. Exits formed in the trailing edge communicate with an exit pressure. The rib and pressure regulating features cooperate such that the downstream supply pressure mimics the exit pressure along the radial span.


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