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:
May. 01, 2018

Filed:

Sep. 21, 2015
Applicant:

General Electric Company, Schenectady, NY (US);

Inventors:

Patrick Michael Marrinan, Mason, OH (US);

Thomas Lee Becker, Symmes Township, OH (US);

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

Assignee:

General Electric Company, Schenectady, NY (US);

Attorneys:
Primary Examiner:
Int. Cl.
CPC ...
B64D 29/04 (2006.01); B64D 27/10 (2006.01); B64C 21/06 (2006.01); F02K 3/06 (2006.01); B64C 1/16 (2006.01); B64D 27/20 (2006.01); B64D 33/02 (2006.01);
U.S. Cl.
CPC ...
B64D 27/10 (2013.01); B64C 1/16 (2013.01); B64C 21/06 (2013.01); B64D 27/20 (2013.01); B64D 29/04 (2013.01); B64D 33/02 (2013.01); F02K 3/06 (2013.01); B64C 2230/04 (2013.01); Y02T 50/166 (2013.01); Y02T 50/44 (2013.01);
Abstract

A propulsion system for an aircraft including a plurality of primary engines is provided. The plurality of primary engines includes at least a first primary engine and a second primary engine, each configured for mounting to a respective one of a pair of wings of the aircraft. The propulsion system additionally includes an aft engine configured for mounting at a tail section of the aircraft. The plurality of primary engines are sized to provide an amount of thrust sufficient for the aircraft to takeoff without use of the aft engine, such that the aft engine may be configured as a non-prime reliable engine.


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