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. 08, 2024

Filed:

Feb. 09, 2023
Applicant:

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

Inventors:

John Richard McCullough, Weatherford, TX (US);

Paul K. Oldroyd, Azle, TX (US);

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 29/02 (2006.01); B64C 11/28 (2006.01); B64C 27/50 (2006.01); B64C 29/00 (2006.01); B64C 39/02 (2023.01); B64C 39/06 (2006.01); B64D 1/08 (2006.01); B64D 35/00 (2006.01); B64D 25/12 (2006.01);
U.S. Cl.
CPC ...
B64C 29/0033 (2013.01); B64C 11/28 (2013.01); B64C 27/50 (2013.01); B64C 29/02 (2013.01); B64C 39/02 (2013.01); B64C 39/06 (2013.01); B64D 1/08 (2013.01); B64D 35/00 (2013.01); B64C 2211/00 (2013.01); B64D 25/12 (2013.01);
Abstract

An aircraft includes an airframe having at least one wing. A distributed propulsion system is attached to the airframe and includes first and second pluralities of propulsion assemblies. In a vertical takeoff and landing flight mode, each of the propulsion assemblies generates vertical thrust with rotor assemblies of the first plurality of propulsion assemblies rotating in a horizontal plane and rotor assemblies of the second plurality of propulsion assemblies rotating in a parallel horizontal plane. In a forward flight mode, each of the propulsion assemblies generates forward thrust with the rotor assemblies of the first plurality of propulsion assemblies rotating in a vertical plane and the rotor assemblies of the second plurality of propulsion assemblies rotating in a parallel vertical plane. In both the vertical takeoff and landing flight mode and the forward flight mode, a pod assembly coupled to the airframe remains in a generally horizontal attitude.


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