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:
Sep. 14, 2021

Filed:

May. 31, 2018
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Thomas Julien Nguyen Van, Moissy-Cramayel, FR;

Olivier Belmonte, Moissy-Cramayel, FR;

Jeremy Phorla Lao, Moissy-Cramayel, FR;

Clementine Charlotte Marie Mouton, Moissy-Cramayel, FR;

Emmanuel Pierre Dimitri Patsouris, Moissy-Cramayel, FR;

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

Assignee:
Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 6/20 (2006.01); F02K 3/065 (2006.01); F02K 3/072 (2006.01); B64D 27/14 (2006.01); B64D 27/26 (2006.01);
U.S. Cl.
CPC ...
F02C 6/206 (2013.01); B64D 27/14 (2013.01); B64D 27/26 (2013.01); F02K 3/065 (2013.01); F02K 3/072 (2013.01); B64D 2027/262 (2013.01); F05D 2220/323 (2013.01); F05D 2260/40311 (2013.01);
Abstract

A turbojet of the unducted rotor type and an aircraft including such a turbojet, the turbojet including a gas generator, a first unducted propeller connected to a shaft of the gas generator via first reduction gearing, and a second unducted propeller connected to a shaft of the gas generator via second reduction gearing, wherein the first propeller and the first reduction gearing are mounted at the front of the gas generator, and wherein the second propeller and the second reduction gearing are mounted at the rear of the gas generator.


Find Patent Forward Citations

Loading…