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:
Jan. 17, 2023

Filed:

Mar. 11, 2021
Applicant:

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

Inventors:

Karl Hugo Schroeder, Southlake, TX (US);

Joseph R. Carpenter, Jr., Burleson, TX (US);

Assignee:

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

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64C 29/00 (2006.01); B64D 27/24 (2006.01); B64D 35/02 (2006.01); B64C 11/00 (2006.01); B64D 41/00 (2006.01); B60L 50/60 (2019.01); B60L 15/20 (2006.01); B64D 31/00 (2006.01);
U.S. Cl.
CPC ...
B64C 29/0033 (2013.01); B60L 15/20 (2013.01); B60L 50/60 (2019.02); B64C 11/001 (2013.01); B64D 27/24 (2013.01); B64D 31/00 (2013.01); B64D 35/02 (2013.01); B64D 41/00 (2013.01); B60L 2200/10 (2013.01); B64C 2211/00 (2013.01);
Abstract

A ducted propulsion assembly for an aircraft includes a duct and a plurality of stators. The distal ends of the stators are coupled to the duct. The ducted propulsion assembly includes a line replaceable centerbody assembly isostatically coupled to the proximal ends of the stators. The line replaceable centerbody assembly includes one or more electric motors driving an output driveshaft. The ducted propulsion assembly also includes a proprotor assembly interchangeably coupled to and rotatable with the output driveshaft of the line replaceable centerbody assembly. The proprotor assembly is rotatable in a rotational plane to generate thrust.


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