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:
Feb. 01, 2022

Filed:

Sep. 01, 2020
Applicant:

Solar Turbines Incorporated, San Diego, CA (US);

Inventors:

David A. Burton, San Diego, CA (US);

Kwok-Kwong Ben Tse, San Diego, CA (US);

David Lau, San Diego, CA (US);

Assignee:

Solar Turbines Incorporated, San Diego, CA (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 9/04 (2006.01); F01D 5/02 (2006.01); F01D 9/06 (2006.01); F01D 17/16 (2006.01); F01D 25/24 (2006.01);
U.S. Cl.
CPC ...
F01D 5/027 (2013.01); F01D 9/042 (2013.01); F01D 9/06 (2013.01); F01D 17/162 (2013.01); F01D 25/246 (2013.01);
Abstract

A stator assembly, at a compressor mid-plane in a gas turbine engine, to be mounted around a rotor disc, enables access to the rotor disc (e.g., for trim balancing), without requiring disassembly of the stator assembly and/or a compressor case in which the stator assembly is housed, via a removable stator vane. The stator assembly may comprise vane apertures, aligned along a radial axis, that hold the removable stator vane when inserted into the stator assembly, and provide a radial pathway to the rotor disc, when the removable stator vane is removed from the stator assembly. In addition, a case access assembly may seal the removable stator vane in place within a compressor case when engaged, and provide access to the removable stator vane and radial pathway through the compressor case when disengaged. This enables trim balancing of a mid-plane compressor rotor assembly through the stator assembly and compressor case.


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