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. 10, 2023

Filed:

Jan. 07, 2022
Applicant:

Raytheon Technologies Corporation, Farmington, CT (US);

Inventors:

Daniel A. Bales, Avon, CT (US);

Dmitri Novikov, Avon, CT (US);

Robert C. Dolan, Coventry, CT (US);

Eric W. Malmborg, Amston, CT (US);

Steven T. Gordon, Glastonbury, CT (US);

Assignee:

RTX Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/30 (2006.01); B23K 1/00 (2006.01); F01D 5/14 (2006.01); F04D 29/38 (2006.01); B23K 101/00 (2006.01);
U.S. Cl.
CPC ...
F01D 5/3061 (2013.01); B23K 1/0018 (2013.01); F01D 5/147 (2013.01); F04D 29/388 (2013.01); B23K 2101/001 (2018.08); F05D 2230/232 (2013.01); F05D 2240/301 (2013.01);
Abstract

An airfoil for a gas turbine engine includes a first portion joined to a second portion along an interface such that at least the first portion establishes an airfoil section and the second portion establishes a root section. The airfoil section includes an airfoil body that extends between leading and trailing edges in a chordwise direction, between pressure and suction sides separated in a thickness direction, and from the root section to a tip portion in a spanwise direction. A recessed region extends inwardly from at least one of the pressure and suction sides. The airfoil body includes at least one rib that bounds a respective pocket within a perimeter of the recessed region. The recessed region and the at least one rib are dimensioned to extend across the interface. A cover skin is coupled to the airfoil body along the at least one rib to enclose the recessed region.


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