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:
Aug. 16, 2022

Filed:

Oct. 09, 2019
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Paul Ghislain Albert Levisse, Moissy-Cramayel, FR;

Olivier Belmonte, Moissy-Cramayel, FR;

Olivier Formica, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F02C 3/067 (2006.01); F02C 7/06 (2006.01); F02C 7/36 (2006.01); F01D 25/16 (2006.01);
U.S. Cl.
CPC ...
F02C 3/067 (2013.01); F01D 25/16 (2013.01); F02C 7/06 (2013.01); F02C 7/36 (2013.01); F05D 2220/323 (2013.01); F05D 2230/60 (2013.01); F05D 2240/50 (2013.01); F05D 2250/44 (2013.01); F05D 2260/40311 (2013.01);
Abstract

Aircraft turbomachine with mechanical reducer and counter-rotating turbine are described. The turbomachine includes a fan driven in rotation by a fan shaft, a mechanical reducer with epicyclic gear train, a gas generator comprising a counter-rotating turbine, a first turbine shaft of which is coupled to an input shaft of the reducer and to a pin, and a second turbine shaft of which is coupled to the fan shaft. The guidance of the reducer input shaft is provided by a first ball bearing, the guidance of the pin is provided by a second roller bearing, and the guidance of the first shaft is provided by a third roller bearing axially interposed between the first and second bearings.


Find Patent Forward Citations

Loading…