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. 05, 2021

Filed:

Jun. 21, 2017
Applicant:

Mitsubishi Hitachi Power Systems Americas, Inc., Lake Mary, FL (US);

Inventor:

Justin Chartier, Savannah, GA (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/30 (2006.01); F01D 25/28 (2006.01); B23P 19/10 (2006.01); B23P 19/04 (2006.01);
U.S. Cl.
CPC ...
F01D 25/285 (2013.01); B23P 19/10 (2013.01); F01D 5/3007 (2013.01); B23P 19/04 (2013.01); F01D 25/28 (2013.01); F05D 2230/60 (2013.01); F05D 2230/64 (2013.01);
Abstract

Devices, systems and methods of the present disclosure can include a guide for installing an airfoil component in a slotted component of a gas turbine engine. The guide can comprise a guide body, a guide slot and an alignment appendage. The guide body can comprise a slot-facing side, an entry side, and a radially outer side surface connecting the slot-facing side and the entry side. The guide slot can extend from the entry side to the slot-facing side and can penetrate the radially outer side surface. The guide slot can have a silhouette matching that of a root portion of the airfoil component. The alignment appendage can extend from the guide body and can have a geometry for axial engagement with a circumferential feature of the slotted component into which the airfoil component is to be installed.


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