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:
Aug. 04, 2020

Filed:

Nov. 22, 2016
Applicant:

Honeywell International Inc., Morris Plains, NJ (US);

Inventors:

Cristian Anghel, Oro Valley, AZ (US);

Eric Blumer, Scottsdale, AZ (US);

Assignee:

HONEYWELL INTERNATIONAL INC., Morris Plains, NJ (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 27/24 (2006.01); B64D 31/00 (2006.01); B64D 35/04 (2006.01); B64C 29/00 (2006.01); B64D 27/10 (2006.01); B64D 35/02 (2006.01); B64D 27/02 (2006.01);
U.S. Cl.
CPC ...
B64D 27/24 (2013.01); B64C 29/0033 (2013.01); B64D 27/10 (2013.01); B64D 31/00 (2013.01); B64D 35/02 (2013.01); B64D 35/04 (2013.01); B64D 2027/026 (2013.01); B64D 2221/00 (2013.01); Y02T 50/64 (2013.01);
Abstract

A hybrid electric aircraft propulsion system at least includes a motor with induction effect to drive a propeller or propulsion fan. The motor is directly supplied from the electrical output of a generator. The generator is driven by a variable speed engine and as such the generator has a output frequency proportional to the speed of the engine. A controller is operatively coupled to the motor, the generator and the engine. The controller is operable to control a speed of the engine and the excitation of the generator to provide an output at a target voltage and frequency to drive the motor at a desired torque and speed.


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