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. 20, 2023

Filed:

Jun. 15, 2020
Applicants:

General Electric Company, Schenectady, NY (US);

Oliver Crispin Robotics Limited, Altrincham, GB;

Inventors:

Todd William Danko, Niskayuna, NY (US);

Ambarish Jayant Kulkarni, Glenville, NY (US);

Margeaux Wallace, Niskayuna, NY (US);

Hrishikesh Keshavan, Watervliet, NY (US);

Bernard Patrick Bewlay, Niskayuna, NY (US);

Byron Andrew Pritchard, Jr., Loveland, OH (US);

Michael Dean Fullington, West Chester, OH (US);

Andrew Crispin Graham, Badminton, GB;

Trevor Owen Hawke, Bristol, GB;

Julian Matthew Foxall, Bristol, GB;

Ahmed M ELKady, West Chester, OH (US);

Assignees:

General Electric Company, Schenectady, NY (US);

Oliver Crispin Robotics Limited, Altrincham, GB;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64F 5/40 (2017.01); B05B 15/68 (2018.01); B05B 15/70 (2018.01); B05B 12/12 (2006.01); G01N 21/88 (2006.01); G01N 21/954 (2006.01);
U.S. Cl.
CPC ...
B64F 5/40 (2017.01); B05B 12/124 (2013.01); B05B 15/68 (2018.02); B05B 15/70 (2018.02); G01N 21/8851 (2013.01); G01N 21/954 (2013.01);
Abstract

A method for inspecting and repairing a surface of a component of a gas turbine engine, the method including: inserting an inspection and repair tool into an interior of the gas turbine engine; inspecting the surface of the component with the inspection and repair tool; performing a repair of the surface of the component with the inspection and repair tool from within the interior of the gas turbine engine, the inspection and repair tool remaining within the interior of the gas turbine engine between inspecting the component and performing the repair of the surface of the component.


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