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:
Aug. 08, 2023

Filed:

Oct. 21, 2020
Applicant:

Textron Innovations Inc., Providence, RI (US);

Inventors:

Eric A. Sinusas, Euless, TX (US);

Erik John Oltheten, Fort Worth, TX (US);

Carlos Alexander Fenny, Fort Worth, TX (US);

Assignee:

Textron Innovations Inc., Providence, RI (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 27/08 (2023.01); B64C 27/20 (2023.01); B64C 27/82 (2006.01); B64C 27/00 (2006.01);
U.S. Cl.
CPC ...
B64C 27/08 (2013.01); B64C 27/00 (2013.01); B64C 27/20 (2013.01); B64C 27/82 (2013.01); B64C 2027/8281 (2013.01);
Abstract

A propulsion system for a rotorcraft includes a first fan assembly including a plurality of first fan blades, a second fan assembly including a plurality of second fan blades and a drive system adapted to provide torque to the first and second fan blades. The first fan blades have a larger rotational inertia than the second fan blades. The second fan blades are adapted to experience a larger angular acceleration than the first fan blades in response to torque from the drive system, thereby providing responsive thrust control for the rotorcraft.


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