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. 22, 2024

Filed:

May. 24, 2023
Applicant:

The Boeing Company, Arlington, VA (US);

Inventor:

Kenneth W. Young, Bear, DE (US);

Assignee:

The Boeing Company, Arlington, VA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/28 (2006.01); C23C 24/04 (2006.01); B33Y 10/00 (2015.01); B33Y 70/00 (2020.01); B33Y 80/00 (2015.01);
U.S. Cl.
CPC ...
C23C 24/04 (2013.01); F01D 5/288 (2013.01); B33Y 10/00 (2014.12); B33Y 70/00 (2014.12); B33Y 80/00 (2014.12); F05D 2230/31 (2013.01); F05D 2230/90 (2013.01); F05D 2240/303 (2013.01); F05D 2300/13 (2013.01); F05D 2300/611 (2013.01);
Abstract

A system and method for fabricating a protective leading-edge structure for an airfoil includes system includes a mandrel and a cold spray additive manufacturing apparatus. The cold spray additive manufacturing apparatus is configured to deposit a metallic powder on a tool surface of the mandrel to form an inner layer, intermediate layers, and an outer layer of the leading-edge structure. The inner layer forms an inner surface of the leading-edge structure. The outer layer forms an outer surface of the leading-edge structure. The intermediate layers form a thickness of the leading-edge structure. The inner surface of the leading-edge structure is configured to be coupled to the airfoil such that the outer surface of the leading-edge structure forms a portion of a leading edge and a portion of an aerodynamic surface of the airfoil.


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