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. 15, 2024

Filed:

Mar. 28, 2022
Applicant:

Lockheed Martin Corporation, Bethesda, MD (US);

Inventors:

Byung-Young Min, Trumbull, CT (US);

Vera Klimchenko, Silver Spring, MD (US);

Annie Gao, Norwalk, CT (US);

Alexander F. Dunn, Easton, CT (US);

Claude George Matalanis, Monroe, CT (US);

Brian Ernest Wake, Monroe, CT (US);

Assignee:

LOCKHEED MARTIN CORPORATION, Bethesda, MD (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 27/46 (2006.01); B64C 27/467 (2006.01); B64C 27/473 (2006.01);
U.S. Cl.
CPC ...
B64C 27/467 (2013.01); B64C 27/473 (2013.01);
Abstract

A rotary wing aircraft includes a single main rotor hub configured to receive a rotor blade. The rotor blade includes a blade root, a blade tip, and a blade body. The blade body includes a leading edge and a trailing edge and defines a feathering axis. The leading edge and the trailing edge each include a first portion and a second portion that extend toward a first direction and a second portion, respectively. At a given radial location along the feathering axis, a local twist angle changes from a positive value to a negative value, a chord length decreases in value, a distance between the trailing edge and the feathering axis decreases in value, and the first portion of the leading edge extends toward the first direction. The rotor blade assembly also includes a trailing edge assembly having a trailing edge flap configured to be selectively deployed by an actuator.


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