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:
Jun. 19, 2018

Filed:

Dec. 15, 2015
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Jeffrey Anthony Hamel, Maineville, OH (US);

Kurt David Murrow, Liberty Township, OH (US);

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64D 27/24 (2006.01); B64C 21/06 (2006.01); B64D 27/20 (2006.01); B64D 27/18 (2006.01); B64D 27/02 (2006.01);
U.S. Cl.
CPC ...
B64D 27/24 (2013.01); B64C 21/06 (2013.01); B64D 27/18 (2013.01); B64D 27/20 (2013.01); B64D 2027/026 (2013.01); B64D 2205/00 (2013.01); Y02T 50/166 (2013.01); Y02T 50/62 (2013.01); Y10S 903/905 (2013.01); Y10S 903/906 (2013.01); Y10S 903/907 (2013.01);
Abstract

In one aspect the present subject matter is directed to a gas-electric propulsion system for an aircraft. The system may include a turbofan jet engine, an electric powered boundary layer ingestion fan that is coupled to a fuselage portion of the aircraft aft of the turbofan jet engine, and an electric generator that is electronically coupled to the turbofan jet engine and to the boundary layer ingestion fan. The electric generator converts rotational energy from the turbofan jet engine to electrical energy and provides at least a portion of the electrical energy to the boundary layer ingestion fan. In another aspect of the present subject matter, a method for propelling an aircraft via the gas-electric propulsion system is disclosed.


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