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:
Apr. 26, 2022

Filed:

Apr. 03, 2020
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 29/00 (2006.01); B64C 11/28 (2006.01); B64D 35/00 (2006.01); B64C 27/50 (2006.01); B64C 39/02 (2006.01); B64C 39/06 (2006.01); B64D 1/08 (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 has an airframe with first and second wings having first and second pylons extending therebetween. A distributed propulsion system attached to the airframe includes at least first, second, third and fourth propulsion assemblies that are independently controlled by a flight control system. A pod assembly is coupled to the airframe. In a VTOL flight mode, the first and second propulsion assemblies are forward of the pod assembly and the third and fourth propulsion assemblies are aft of the pod assembly. In a forward flight mode, the first and second propulsion assemblies are below the pod assembly and the third and fourth propulsion assemblies are above the pod assembly. In both the VTOL and forward flight modes, the first and fourth propulsion assemblies generate thrust having a first direction while the second and third propulsion assemblies generate thrust having a second direction that is different from the first direction.


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