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:
Aug. 22, 2023

Filed:

Aug. 11, 2021
Applicants:

General Electric Company, Schenectady, NY (US);

Atlantic Plant Maintenance, Inc., Pasadena, TX (US);

Inventors:

Joanna Sylwia Pilichowska, Warsaw, PL;

Piotr Krzysztof Dzieciol, Warsaw, PL;

Szymon Perkowski, Warsaw, PL;

Daniel John Moroney, Sketty Swansea, GB;

Eric Wayne Hendricks, Soperton, GA (US);

Assignees:

General Electric Company, Schenectady, NY (US);

Atlantic Plant Maintenance, Inc., Pasadena, TX (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F01D 25/28 (2006.01); F01D 5/00 (2006.01);
U.S. Cl.
CPC ...
F01D 25/285 (2013.01); F01D 5/005 (2013.01); F05D 2220/30 (2013.01); F05D 2230/60 (2013.01); F05D 2230/70 (2013.01); F05D 2230/80 (2013.01); F05D 2240/24 (2013.01);
Abstract

An apparatus for removing or installing a turbine blade from a turbine of a turbomachine is disclosed. The apparatus can include: an operative head configured to engage an axial sidewall of a turbine blade base. An actuator is configured to move the operative head to selectively engage the axial sidewall of the turbine blade base and impart an axial force against the turbine blade base to remove or install the turbine blade. A support gantry is configured to position the actuator substantially vertically above the turbine blade in position in the turbomachine. Among other advantages, the support gantry allows adjustment of the apparatus for different turbines, and use of the head on more than one stage of any given turbine.


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