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:
Dec. 21, 2021

Filed:

Jul. 30, 2019
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Nicholas Joseph Kray, Mason, OH (US);

Steven Mark Ballman, West Chester, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/06 (2006.01); F01D 5/02 (2006.01); F01D 11/00 (2006.01); F04D 29/32 (2006.01);
U.S. Cl.
CPC ...
F01D 5/066 (2013.01); F01D 5/026 (2013.01); F01D 11/001 (2013.01); F04D 29/321 (2013.01); F05D 2230/60 (2013.01); F05D 2240/24 (2013.01); F05D 2240/55 (2013.01); F05D 2240/60 (2013.01); F05D 2260/31 (2013.01);
Abstract

A gas turbine engine defining a radial direction is provided. The gas turbine engine includes a tie shaft; a compressor section including a last rotor stage, the compressor section assembled to a first portion of the tie shaft; a separable shaft disposed between the compressor section and the tie shaft, the separable shaft having a radial outward portion and a radial inward portion, the radial outward portion of the separable shaft in contact with a portion of the last rotor stage at an interface; and a seal assembly operable with a portion of the separable shaft proximate the radial inward portion.


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