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:
Nov. 10, 2020

Filed:

Jul. 21, 2016
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventor:

Nicolas Jerome Jean Tantot, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
B64D 27/20 (2006.01); B64D 33/04 (2006.01); B64D 35/06 (2006.01); F02K 3/062 (2006.01); B64D 27/14 (2006.01); F01D 13/00 (2006.01); B64D 27/26 (2006.01); F02C 6/02 (2006.01); F02K 3/02 (2006.01); F02K 3/072 (2006.01);
U.S. Cl.
CPC ...
B64D 27/20 (2013.01); B64D 27/14 (2013.01); B64D 27/26 (2013.01); B64D 33/04 (2013.01); B64D 35/06 (2013.01); F01D 13/003 (2013.01); F02C 6/02 (2013.01); F02K 3/025 (2013.01); F02K 3/062 (2013.01); F02K 3/072 (2013.01); F05D 2220/323 (2013.01);
Abstract

The present invention relates to an aircraft including a fuselage and a thruster downstream of the fuselage. The thruster includes a power turbine, located inside a main flow jet, and at least one fan, located inside a secondary flow jet and mechanically driven by the power turbine. The main flow jet of the power turbine and the secondary flow jet of the fan are concentric. The power turbine is supplied with gases from two gas turbine gas generators via two supply channels. The gas turbine gas generators have axes parallel to that of the fuselage. The air inlet sleeve is spaced apart from the fuselage, and the supply channels each have a hatch for controlling the flow between a position for guiding the gas flow to the power turbine and a position for ejecting the gases into the atmosphere while bypassing the power turbine.


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