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:
Nov. 01, 2022

Filed:

Dec. 04, 2015
Applicant:

L3harris Latitude Llc, Melbourne, FL (US);

Inventors:

Justin Armer, Tucson, AZ (US);

Carlos Murphy, Tucson, AZ (US);

Jason Michael K. Douglas, Tucson, AZ (US);

Assignee:

L3HARRIS LATITUDE LLC, Melbourne, FL (US);

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 29/00 (2006.01); B64C 39/02 (2006.01); B64C 5/02 (2006.01); B64C 17/00 (2006.01);
U.S. Cl.
CPC ...
B64C 29/0025 (2013.01); B64C 5/02 (2013.01); B64C 17/00 (2013.01); B64C 39/024 (2013.01); B64C 2201/021 (2013.01); B64C 2201/024 (2013.01); B64C 2201/108 (2013.01);
Abstract

A vertical take-off and landing aircraft includes a fixed wing airframe having opposed first and second wings extending from first and second sides, respectively, of a fuselage having opposed leading and trailing extremities, and a tail assembly located behind the trailing extremity. Vertical take-off and landing (VTOL) thrust rotors are mounted to the airframe providing vertical lift to the aircraft, and a forward thrust rotor is mounted to the airframe for providing forward thrust to the aircraft. At least one of VTOL thrust rotors is laterally tilted with respect to the airframe for providing vertical lift and yaw control authority to the aircraft.


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