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. 18, 2022

Filed:

Feb. 24, 2020
Applicant:

Aurora Flight Sciences Corporation, Manassas, VA (US);

Inventor:

Tony Shuo Tao, Somerville, MA (US);

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64C 29/00 (2006.01); B64C 1/14 (2006.01); B64C 39/08 (2006.01); B64C 9/00 (2006.01); B64C 11/28 (2006.01); B64C 23/02 (2006.01); B64D 27/20 (2006.01); B64D 27/24 (2006.01);
U.S. Cl.
CPC ...
B64C 29/0025 (2013.01); B64C 1/1407 (2013.01); B64C 9/00 (2013.01); B64C 11/28 (2013.01); B64C 23/02 (2013.01); B64C 39/08 (2013.01); B64D 27/20 (2013.01); B64D 27/24 (2013.01); B64C 2009/005 (2013.01);
Abstract

Fixed-wing short-takeoff-and-landing aircraft and related methods. The aircraft comprise an airframe comprising a rear wing assembly and a forward wing assembly positioned forward of the rear wing assembly, a rear plurality of blowing rotor assemblies operatively coupled to the rear wing assembly that are configured to blow air across the rear wing assembly to induce lift in the rear wing assembly, and a forward plurality of blowing rotor assemblies that are operatively coupled to the forward wing assembly and configured to blow air across the forward wing assembly to induce lift in the forward wing assembly. The methods comprise inducing lift in a forward wing assembly by blowing air across the forward wing assembly with a forward plurality of blowing rotor assemblies and inducing lift in a rear wing assembly by blowing air across a rear wing assembly with a rear plurality of blowing rotor assemblies.


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