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. 27, 2026

Filed:

Sep. 26, 2023
Applicant:

Chromalloy Gas Turbine Llc, Palm Beach Gardens, FL (US);

Inventors:

James Whitton, East Burke, VT (US);

Zachary Oras, Riverview, FL (US);

Zachary Hopkins, San Diego, CA (US);

Assignee:

Chromalloy Gas Turbine LLC, Palm Beach Gardens, FL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B22F 7/06 (2006.01); B22F 5/04 (2006.01); B22F 10/40 (2021.01); B22F 10/66 (2021.01); B33Y 40/20 (2020.01);
U.S. Cl.
CPC ...
B22F 7/062 (2013.01); B22F 5/04 (2013.01); B22F 10/40 (2021.01); B22F 10/66 (2021.01); B33Y 40/20 (2020.01); B22F 2007/068 (2013.01);
Abstract

Systems and methods are provided for repairing compressor blades using hybrid manufacturing. A mounting tool for use in repairing a turbine component includes a slot formed in the mounting tool. The slot is configured to receive the turbine component for securing the turbine component to the mounting tool. The mounting tool includes at least one fastener engageable with the turbine component and capable of retaining the turbine component within the slot; and at least a pair of support bases provided on the mounting tool. Each of the at least a pair of support bases is positioned adjacent a respect edge of the turbine component when the turbine component is retained in the mounting tool. Each of the at least a pair of support bases is configured for additively building a sacrificial support on each of the at least a pair of support bases for enabling repair of the turbine component.


Find Patent Forward Citations

Whitton, James. (2026). Systems and methods for repairing compressor blades using hybrid manufacturing techniques (U.S. Patent No. 12533728). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/12533728

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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