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:
Jun. 23, 2020

Filed:

Jan. 16, 2018
Applicant:

Safran Aero Boosters SA, Herstal (Milmort), BE;

Inventor:

Stephane Hiernaux, Oupeye, BE;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F04D 29/58 (2006.01); F01D 25/24 (2006.01); F01D 25/02 (2006.01); F01D 9/04 (2006.01); F01D 11/02 (2006.01); F01D 5/14 (2006.01); F01D 11/00 (2006.01); F01D 15/12 (2006.01); F01D 11/24 (2006.01); F02C 7/14 (2006.01); F02C 7/06 (2006.01); F01D 25/14 (2006.01); F02C 7/047 (2006.01); F01D 25/10 (2006.01); F01D 25/16 (2006.01); F04D 29/54 (2006.01);
U.S. Cl.
CPC ...
F04D 29/584 (2013.01); F01D 5/143 (2013.01); F01D 9/04 (2013.01); F01D 9/041 (2013.01); F01D 11/005 (2013.01); F01D 11/025 (2013.01); F01D 11/24 (2013.01); F01D 15/12 (2013.01); F01D 25/02 (2013.01); F01D 25/10 (2013.01); F01D 25/14 (2013.01); F01D 25/162 (2013.01); F01D 25/246 (2013.01); F02C 7/047 (2013.01); F02C 7/06 (2013.01); F02C 7/14 (2013.01); F04D 29/542 (2013.01); F05D 2220/323 (2013.01); F05D 2240/11 (2013.01); F05D 2240/14 (2013.01); F05D 2260/30 (2013.01); F05D 2260/40311 (2013.01); F05D 2300/40 (2013.01); F05D 2300/505 (2013.01); F05D 2300/5021 (2013.01); F05D 2300/50212 (2013.01); F05D 2300/603 (2013.01); Y02T 50/672 (2013.01); Y02T 50/675 (2013.01);
Abstract

An assembly for a turbojet, wherein the assembly includes an outer shroud and an inner shroud that are concentric, wherein the inner shroud is segmented and includes circumferential clearances between the segments thereof. The assembly additionally includes an annular row of stator vanes connecting the inner shroud to the outer shroud, a drive with a reduction ratio that is intended to be coupled to a fan, and a circuit for cooling and for lubricating the drive. The circuit is configured to heat up at least the outer shroud during the operation of the turbine engine such as to circumferentially reduce the circumferential clearances between the segments.


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