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:
Oct. 21, 2025

Filed:

Dec. 29, 2023
Applicant:

Lockheed Martin Corporation, Bethesda, MD (US);

Inventors:

Yuriy Gmirya, Woodbridge, CT (US);

Bruce P. Plasse, Woodbridge, CT (US);

Assignee:

Lockheed Martin Corporation, Bethesda, MD (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/12 (2006.01); B64C 27/10 (2023.01); F16B 7/04 (2006.01); F16C 3/02 (2006.01); F16H 1/20 (2006.01); F16H 57/00 (2012.01);
U.S. Cl.
CPC ...
B64C 27/12 (2013.01); B64C 27/10 (2013.01); F16B 7/0413 (2013.01); F16C 3/02 (2013.01); F16H 1/20 (2013.01); F16H 57/0025 (2013.01); F16C 2326/43 (2013.01);
Abstract

A coaxial rotary-wing aircraft including a first rotor rotatable about a first axis in a first direction, a second rotor rotatable about the first axis in a second direction to provide lift, and a gearbox. The gearbox includes a first gear oriented to rotate about an axis, a second gear spaced from the first gear and oriented to rotate about the axis, and a shaft assembly extending between the first gear and the second gear. The shaft assembly includes a shaft, a lock mechanism, and a retaining extension. The shaft has a first end coupled with the first gear and a second end coupled with the second gear, the second end including at least one recess formed on an end face. The lock mechanism is removably coupled to the second end of the shaft.


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