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. 17, 2021

Filed:

Oct. 03, 2017
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Sandra Beverly Kolvick, Simpsonville, SC (US);

Kevin Leon Bruce, Greer, SC (US);

Antoine Mastroianni, Bourogne, FR;

Danielle Werner, Esko, MN (US);

Hubert Karol Wojtowicz, Warsaw, PL;

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
F01D 25/28 (2006.01); B25B 5/00 (2006.01); B25B 5/10 (2006.01); B25B 27/14 (2006.01); F01D 5/12 (2006.01); F01D 5/30 (2006.01);
U.S. Cl.
CPC ...
F01D 25/285 (2013.01); B25B 5/003 (2013.01); B25B 5/101 (2013.01); B25B 27/14 (2013.01); F01D 5/12 (2013.01); F01D 5/3007 (2013.01); F05D 2230/64 (2013.01); F05D 2230/68 (2013.01); F05D 2230/70 (2013.01);
Abstract

Embodiments of the present disclosure can provide an apparatus for circumferentially separating turbine blades. An apparatus according to the present disclosure may include: a length-adjustable elongate member having opposing first and second ends; a first clasp coupled to the first end of the length-adjustable elongate member, the first clasp shaped to at least partially engage an airfoil profile of a first turbine blade positioned circumferentially adjacent to a dovetail slot, relative to a centerline axis of the turbomachine; and a second clasp coupled to the second end of the length-adjustable elongate member, the second clasp shaped to at least partially engage an airfoil profile of a second turbine blade circumferentially positioned adjacent to the dovetail slot, the first and second turbine blades being circumferentially adjacent to the dovetail slot at opposing circumferential ends thereof.


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