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. 07, 2026

Filed:

Jan. 10, 2024
Applicant:

Lockheed Martin Corporation, Bethesda, MD (US);

Inventors:

Kevin A. Laitenberger, Beacon Falls, CT (US);

Claude George Matalanis, Monroe, CT (US);

Yair Preiss, Norwalk, CT (US);

Joseph Thomas Palombo, Richmondville, NY (US);

Andrew Hunt, League City, TX (US);

Assignee:

LOCKHEED MARTIN CORPORATION, Bethesda, MD (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/35 (2006.01); B64C 27/72 (2006.01); F16C 19/49 (2006.01);
U.S. Cl.
CPC ...
B64C 27/35 (2013.01); B64C 27/72 (2013.01); F16C 19/49 (2013.01); F16C 2326/43 (2013.01);
Abstract

A rotor assembly for a rotary wing aircraft includes a rotor hub, a rotor blade coupling coupled to the rotor hub, a hub extender coupled to the rotor hub, and a first bearing assembly. The first bearing assembly includes a clevis coupled to the hub extender and including two arms, each arm including a clevis opening, two cylindrical bearings, each cylindrical bearing extending through one of the clevis openings, a spherical bearing positioned between the two arms and coupled to the rotor blade coupling, and a first pin extending through the two cylindrical bearings and the spherical bearing.


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