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:
Mar. 03, 2026

Filed:

Jan. 03, 2025
Applicant:

Rtx Corporation, Farmington, CT (US);

Inventors:

Sohail Mohammed, Manchester, CT (US);

Scot Webb, Gales Ferry, CT (US);

Assignee:

RTX Corporation, Farmington, CT (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F01D 5/06 (2006.01); F01D 5/02 (2006.01); F01D 25/16 (2006.01);
U.S. Cl.
CPC ...
F01D 5/025 (2013.01); F01D 5/063 (2013.01); F01D 5/066 (2013.01); F01D 25/16 (2013.01); F05D 2220/32 (2013.01); F05D 2240/24 (2013.01); F05D 2240/54 (2013.01); F05D 2240/60 (2013.01);
Abstract

An axial compressor rotor assembly includes a plurality of rotor disks extending axially along and circumferentially about a central axis between an upstream end and a downstream end. The rotor disks extend radially between an inner radial hub and an outer radial rim, and axially between a forward rim end and a rearward rim end. An airfoil extends spanwise from each of the rotor disks. A first rotor disk is disposed forward of a second rotor disk. The second rotor disk includes an interstage shaft. The interstage shaft includes an outer radial end, an inner radial end, and an arm. The arm extending axially from an outer surface of the interstage shaft to a distal end. The rearward rim end of the first rotor disk is fixedly joined to the distal end of the arm, for example, by inertia welding.


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