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:
Jul. 14, 2020

Filed:

Aug. 29, 2017
Applicant:

The Boeing Company, Chicago, IL (US);

Inventor:

Mithra M. K. V. Sankrithi, Edmonds, WA (US);

Assignee:

The Boeing Company, Chicago, IL (US);

Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
B64D 27/00 (2006.01); B64D 27/24 (2006.01); B64D 41/00 (2006.01); F02K 3/06 (2006.01); F01D 15/10 (2006.01); H02K 7/18 (2006.01); B64C 11/30 (2006.01); B64D 27/16 (2006.01); F02K 5/00 (2006.01); F02K 3/072 (2006.01); B64D 27/02 (2006.01); F02K 1/66 (2006.01);
U.S. Cl.
CPC ...
B64D 27/24 (2013.01); B64C 11/30 (2013.01); B64D 27/16 (2013.01); B64D 41/00 (2013.01); F01D 15/10 (2013.01); F02K 3/06 (2013.01); F02K 3/072 (2013.01); F02K 5/00 (2013.01); H02K 7/1823 (2013.01); B64D 2027/026 (2013.01); F02K 1/66 (2013.01); F05D 2220/323 (2013.01); F05D 2220/324 (2013.01); F05D 2220/325 (2013.01); F05D 2220/327 (2013.01); F05D 2220/76 (2013.01); F05D 2260/42 (2013.01);
Abstract

Hybrid aircraft propulsors having electrically-driven augmentor fans are disclosed. An example apparatus includes a turbofan having a core engine and a ducted fan to be rotated via the core engine. The ducted fan includes a plurality of ducted fan blades arranged circumferentially around the core engine and circumscribed by a nacelle. The example apparatus further includes an augmentor fan having an augmentor hub ring and a plurality of augmentor fan blades. The augmentor fan blades are arranged circumferentially around the augmentor hub ring and project outwardly relative to an outer surface of the nacelle. The augmentor fan is to rotate separately from the ducted fan. The example apparatus further includes an electrical drive to rotate the augmentor hub ring in response to a supply of electrical energy provided to the electrical drive.


Find Patent Forward Citations

Sankrithi, Mithra M. K. V.. (2020). Hybrid aircraft propulsors having electrically-driven augmentor fans (U.S. Patent No. 10710734). U.S. Patent and Trademark Office. https://idiyas.com/patent/badge/10710734

Data source: USPTO (United States Patent and Trademark Office) public patent records. Weekly synchronization. How IDiyas builds this profile

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