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:
Sep. 26, 2023

Filed:

Aug. 31, 2020
Applicant:

Lockheed Martin Corporation, Bethesda, MD (US);

Inventors:

Timothy F. Lauder, Oxford, CT (US);

Mark W. Scott, Bethany, CT (US);

Michael Strauss, New Haven, CT (US);

Jonathan D. Hartman, Southington, CT (US);

Assignee:

Lockheed Martin Corporation, Bethesda, MD (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/14 (2006.01); B64D 27/24 (2006.01); B64C 27/10 (2023.01); B64D 27/02 (2006.01);
U.S. Cl.
CPC ...
B64C 27/14 (2013.01); B64C 27/10 (2013.01); B64D 27/24 (2013.01); B64D 2027/026 (2013.01);
Abstract

An aircraft includes an airframe, and a coaxial main rotor assembly including a static mast and an upper rotor assembly and a lower rotor assembly rotatable about a main rotor axis defined by the static mast. The upper rotor assembly and the lower rotor assembly are independently rotatable about the static mast. A propulsion system includes at least one propulsion source for directly driving at least one of the upper rotor assembly and the lower rotor assembly and a flight control system is operably coupled to the propulsion system. The flight control system is operable to independently control a rotational speed of the upper rotor assembly and the lower rotor assembly relative to the static mast.


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