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. 22, 2023

Filed:

Feb. 14, 2018
Applicant:

Bell Helicopter Textron Inc., Fort Worth, TX (US);

Inventors:

Carlos Alexander Fenny, Fort Worth, TX (US);

John Robert Wittmaak, Jr., Newark, TX (US);

Mike John Ryan, Colleyville, TX (US);

Joseph Scott Drennan, Dallas, TX (US);

Assignee:

TEXTRON INNOVATIONS INC., Providence, RI (US);

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 27/24 (2006.01); B64C 29/00 (2006.01); F01D 15/10 (2006.01); B64D 27/02 (2006.01);
U.S. Cl.
CPC ...
B64D 27/24 (2013.01); B64C 29/0033 (2013.01); F01D 15/10 (2013.01); B64D 2027/026 (2013.01); F05D 2220/328 (2013.01); F05D 2220/76 (2013.01); Y02T 50/60 (2013.01);
Abstract

The present invention includes a hybrid propulsion system for an aircraft comprising: one or more turboshaft engines that provide shaft power and are capable of providing thrust; at least one of: one or more electrical generators or one or more hydraulic pumps connected to a shaft of the one or more turboshaft engines; and at least two rotatable nacelles, each nacelle housing at least one of: one or more electric motors or one or more hydraulic motors each connected to a proprotor, wherein the electric motor is electrically connected to the electric generator, or the hydraulic motor is connected to the hydraulic pump, respectively, wherein the proprotors provide lift whenever the aircraft is in vertical takeoff and landing and stationary flight, and provide thrust whenever the aircraft is in forward flight.


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