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:
Jul. 01, 2025

Filed:

Nov. 17, 2023
Applicant:

Rolls-royce Corporation, Indianapolis, IN (US);

Inventors:

Michael Nesteroff, Indianapolis, IN (US);

Mark E. Whitlock, Indianapolis, IN (US);

Nathanael Cooper, Indianapolis, IN (US);

Jonathan Acker, Indianapolis, IN (US);

Assignee:

Rolls-Royce Corporation, Indianapolis, IN (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F04D 29/42 (2006.01); F01D 11/16 (2006.01); F01D 11/22 (2006.01); F01D 17/12 (2006.01); F04D 29/46 (2006.01);
U.S. Cl.
CPC ...
F01D 11/22 (2013.01); F01D 11/16 (2013.01); F01D 17/12 (2013.01); F04D 29/4206 (2013.01); F04D 29/464 (2013.01); F05D 2230/60 (2013.01);
Abstract

A compressor assembly for a gas turbine engine includes a shroud assembly, an outer case assembly, and a plurality of locating bolt assemblies. The shroud assembly extends circumferentially around the engine axis. The outer case assembly includes an outer case that extends circumferentially around the axis and a plurality of fasteners that couple the shroud assembly with the outer case. The plurality of locating bolt assemblies extend into the outer case and abut the shroud assembly at a predetermined axial location to axially locate the shroud assembly.


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