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:
Mar. 28, 2023

Filed:

Jan. 18, 2021
Applicants:

Luc Van Bavel, Quebec, CA;

Michael Derman, Bend, OR (US);

Inventors:

Luc Van Bavel, Quebec, CA;

Michael Derman, Bend, OR (US);

Assignee:

Other;

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 27/02 (2006.01); B64D 27/24 (2006.01); B64D 27/26 (2006.01); F01D 15/10 (2006.01); B64U 50/19 (2023.01);
U.S. Cl.
CPC ...
B64D 27/24 (2013.01); B64D 27/02 (2013.01); B60L 2200/10 (2013.01); B60Y 2400/112 (2013.01); B64D 27/26 (2013.01); B64D 2027/026 (2013.01); B64D 2221/00 (2013.01); B64U 50/19 (2023.01); F01D 15/10 (2013.01); Y02T 50/60 (2013.01);
Abstract

Some apparatus embodiments include an aircraft having a hybrid parallel electric propulsion system including two internal combustion engines and an electric propulsion system including two electric motors electrically connected to an electric power module. The electric power module is optionally configured for attachment to a bottom side of a fuselage. Each of the electric motors attaches to an aircraft wing outboard of the nearest internal combustion engine. The electric motors and internal combustion engines are operable independently of one another, providing for propulsion by the electric motors during flight and ground operations when the internal combustion engines may operate inefficiently. Some embodiments are implemented as a hybrid parallel electric propulsion retrofit package for adding an electric propulsion system to an aircraft previously equipped only with internal combustion engines.


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