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:
Apr. 14, 2026

Filed:

Aug. 29, 2023
Applicant:

Lockheed Martin Corporation, Bethesda, MD (US);

Inventors:

Daniel George Schuster, Bethlehem, CT (US);

David N. Schmaling, Southbury, CT (US);

Evan S. Tobin, Shelton, CT (US);

Eric M. Bogert, Wallingford, CT (US);

Assignee:

LOCKHEED MARTIN CORPORATION, Bethesda, MD (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/80 (2006.01); B64C 11/38 (2006.01); B64C 27/10 (2023.01); B64C 27/64 (2006.01); B64C 27/82 (2006.01);
U.S. Cl.
CPC ...
B64C 27/80 (2013.01); B64C 11/38 (2013.01); B64C 27/10 (2013.01); B64C 27/64 (2013.01); B64C 2027/8236 (2013.01);
Abstract

A rotor assembly for a rotary wing aircraft includes a rotor hub including a hub arm and a central opening. The rotor assembly further includes a hydraulic actuation cylinder positioned in the central opening, a pitch change shaft assembly including a pitch change shaft positioned partially within the hydraulic actuation cylinder, a pitch beam coupled to a distal end of the pitch change shaft and configured to be coupled to a rotor blade rotatably mounted to the hub arm. The rotor assembly additionally includes at least one guide rod coupled to the rotor hub and slidably coupled to an opening in the pitch change shaft.


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