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:
Jan. 26, 2021

Filed:

Jan. 10, 2018
Applicant:

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

Inventors:

Evangelos Livieratos, Manassas, VA (US);

Riley Griffin, Manassas, VA (US);

Nathan Varney, Manassas, VA (US);

Amanda Kaufman, Manassas, VA (US);

Assignee:
Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64D 27/24 (2006.01); B64D 27/04 (2006.01); B64C 27/08 (2006.01); F02B 41/04 (2006.01); F02D 13/02 (2006.01); F02N 11/04 (2006.01); B64C 39/02 (2006.01); F02B 63/04 (2006.01); B64D 27/02 (2006.01); F02B 75/34 (2006.01); F02D 29/06 (2006.01);
U.S. Cl.
CPC ...
B64D 27/24 (2013.01); B64C 27/08 (2013.01); B64C 39/024 (2013.01); B64D 27/04 (2013.01); F02B 41/04 (2013.01); F02D 13/0269 (2013.01); B64C 2201/027 (2013.01); B64C 2201/042 (2013.01); B64C 2201/044 (2013.01); B64D 2027/026 (2013.01); F02B 63/04 (2013.01); F02B 75/34 (2013.01); F02B 2275/32 (2013.01); F02D 29/06 (2013.01); F02N 11/04 (2013.01); Y02T 10/12 (2013.01); Y10S 903/903 (2013.01);
Abstract

A hybrid-electric aerial vehicle is disclosed comprising: an airframe; a plurality of longitudinal booms extending radially from the airframe; a passively charged internal combustion engine operatively coupled with a fuel tank, a generator operatively coupled with the passively charged internal combustion engine; a battery bank operatively coupled with the generator; and a plurality of motors. The passively charged internal combustion engine has an intake engine valve, an exhaust engine valve, and a combustion chamber, wherein the intake engine valve is delayed to provide an expansion ratio in the combustion chamber that is greater than a compression ratio in the combustion chamber. Each of said plurality of motors may be positioned at a distal end of one of said plurality of longitudinal booms and be operatively coupled with a propeller, wherein the plurality of motors is electrically coupled with the battery bank and the generator.


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