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:
Dec. 10, 2019

Filed:

Sep. 25, 2015
Applicant:

Techspace Aero S.a., Herstal, BE;

Inventor:

Stéphane Hiernaux, Oupeye, BE;

Assignee:

SAFRAN AERO BOOSTERS SA, Herstal (Milmort), BE;

Attorney:
Primary Examiner:
Int. Cl.
CPC ...
F02C 7/36 (2006.01); F02K 3/06 (2006.01); F02C 3/067 (2006.01); F02C 3/107 (2006.01); F04D 19/02 (2006.01);
U.S. Cl.
CPC ...
F02C 7/36 (2013.01); F02C 3/067 (2013.01); F02C 3/107 (2013.01); F02K 3/06 (2013.01); F04D 19/024 (2013.01); F05D 2220/32 (2013.01); F05D 2260/40 (2013.01); F05D 2260/40311 (2013.01); Y02T 50/671 (2013.01);
Abstract

The present application relates to an axial turbine engine with a turbine, a low-pressure compressor, and a fan. The turbine drives the compressor and the fan via a plurality of epicyclic reducing gears. The rotor of the compressor includes upstream a disc with a row of vanes and downstream a drum with a plurality of rows of vanes. The disc and the drum are connected to different parts of the epicyclic reducing gears, so as to be counter-rotating. The turbine engine includes a row of stator vanes arranged between two rows of rotor blades of the drum of the compressor, so as to straighten the flow and improve the efficiency. The turbine engine includes at least two epicyclic reducing gears, so that the vane rows of the drum turn faster than that downstream, which itself turns faster than the fan.


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