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:
May. 16, 2023

Filed:

Apr. 08, 2021
Applicant:

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

Inventors:

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

John Richard McCullough, Weatherford, TX (US);

Assignee:

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

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64U 30/20 (2023.01); B64D 31/06 (2006.01); B64C 29/02 (2006.01); B64D 27/24 (2006.01); B64C 27/52 (2006.01); B64C 39/02 (2023.01); G05D 1/08 (2006.01); B64U 10/10 (2023.01); B64U 10/25 (2023.01); B64U 50/13 (2023.01); B64U 50/19 (2023.01);
U.S. Cl.
CPC ...
B64D 31/06 (2013.01); B64C 27/52 (2013.01); B64C 29/02 (2013.01); B64C 39/024 (2013.01); B64D 27/24 (2013.01); G05D 1/0858 (2013.01); B64U 10/10 (2023.01); B64U 10/25 (2023.01); B64U 30/20 (2023.01); B64U 50/13 (2023.01); B64U 50/19 (2023.01);
Abstract

An aircraft has multiple independent yaw authority mechanisms. The aircraft includes an airframe having first and second wings with at least first and second pylons extending therebetween and with a plurality of tail members extending therefrom each having an active control surface. A two-dimensional distributed thrust array is coupled to the airframe that includes a plurality of propulsion assemblies each having a rotor assembly and each operable for thrust vectoring. A flight control system is operable to independently control each of the propulsion assemblies. A first yaw authority mechanism includes differential speed control of rotor assemblies rotating clockwise compared to rotor assemblies rotating counterclockwise. A second yaw authority mechanism includes differential longitudinal control surface maneuvers of control surfaces of two symmetrically disposed tail members. A third yaw authority mechanism includes differential thrust vectoring of propulsion assemblies.


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