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:
Oct. 05, 2021

Filed:

Jul. 21, 2016
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Nicolas Jérôme Jean Tantot, Moissy-Cramayel, FR;

Antoine Jean-Philippe Beaujard, Moissy-Cramayel, FR;

Pascal Coat, Moissy-Cramayel, FR;

Didier Jean-Louis Yvon, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02K 1/70 (2006.01); F02K 1/60 (2006.01); F02C 3/10 (2006.01); F01D 13/02 (2006.01); F02K 3/06 (2006.01); F02K 3/072 (2006.01); F02C 6/02 (2006.01); F02K 1/74 (2006.01); F02K 1/76 (2006.01);
U.S. Cl.
CPC ...
F02K 1/70 (2013.01); F01D 13/02 (2013.01); F02C 3/10 (2013.01); F02C 6/02 (2013.01); F02K 1/60 (2013.01); F02K 1/74 (2013.01); F02K 1/763 (2013.01); F02K 1/766 (2013.01); F02K 3/06 (2013.01); F02K 3/072 (2013.01);
Abstract

An aircraft propulsion assembly, including a turbine engine comprising at least one gas generator configured to generate a main flow, which is supplied by a central jet to at least one power turbine, the central jet being surrounded by an outer fairing, and the power turbine driving, on the periphery thereof, at least one fan rotor. The aircraft propulsion assembly comprises first movable means which are arranged so as to divert at least some of the main flow from the central jet to the outside of the outer fairing and preferably upstream of the turbine engine so as to generate thrust reversal. An aircraft which uses the propulsion assembly, particularly on the rear tip of the fuselage of the aircraft.


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