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.
Patent No.:
Date of Patent:
Nov. 26, 2019
Filed:
Apr. 28, 2015
Applicant:
Safran Aircraft Engines, Paris, FR;
Inventors:
Augustin Curlier, Moissy-Cramayel, FR;
Kevin Morgane Lemarchand, Moissy-Cramayel, FR;
Nathalie Nowakowski, Moissy-Cramayel, FR;
Thomas Alain Christian Vincent, Moissy-Cramayel, FR;
Assignee:
SAFRAN AIRCRAFT ENGINES, Paris, FR;
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 25/16 (2006.01); F02C 7/32 (2006.01); F02C 7/06 (2006.01); F02C 7/36 (2006.01);
U.S. Cl.
CPC ...
F02C 7/32 (2013.01); F01D 25/162 (2013.01); F02C 7/06 (2013.01); F02C 7/36 (2013.01); F05D 2230/60 (2013.01); F05D 2230/72 (2013.01); F05D 2240/90 (2013.01); F05D 2260/4031 (2013.01);
Abstract
A modular assembly for a turbine engine has an annular bearing support that is configured to be connected to a first anti-friction bearing, which is configured to be fitted around a first shaft of the turbine engine. The modular assembly further includes a second anti-friction bearing configured to be fitted around a second shaft of the turbine engine, wherein the second shaft is not parallel to said first shaft.