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. 29, 2021

Filed:

Mar. 22, 2016
Applicant:

Safran Aircraft Engines, Paris, FR;

Inventors:

Nils Bordoni, Moissy-Cramayel, FR;

Guillaume Patrice Kubiak, Moissy-Cramayel, FR;

Kevin Morgane Lemarchand, Moissy-Cramayel, FR;

Assignee:
Attorney:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 15/12 (2006.01); F01D 19/00 (2006.01); F02K 3/06 (2006.01); F02C 7/36 (2006.01); F02C 7/275 (2006.01); F02C 7/277 (2006.01);
U.S. Cl.
CPC ...
F01D 15/12 (2013.01); F01D 19/00 (2013.01); F02C 7/275 (2013.01); F02C 7/277 (2013.01); F02C 7/36 (2013.01); F02K 3/06 (2013.01); F05D 2260/402 (2013.01); F05D 2260/4023 (2013.01); F05D 2260/40311 (2013.01); F05D 2260/85 (2013.01); Y02T 50/60 (2013.01);
Abstract

Aircraft turbine engine comprising a low-pressure spool that comprises a low-pressure shaft (), means () for taking off power from said low-pressure shaft, and a fan () that is driven by said low-pressure shaft by means of a reduction gear (), said reduction gear comprising at least one first element () that is connected to said low-pressure shaft for conjoint rotation, at least one second element () that is connected to said fan for conjoint rotation, and at least one third element () that is connected to a stator casing of the turbine engine, characterised in that said at least one third element is connected to said stator casing by disengageable connection means (), and comprising at least one member that can move from a first position in which said at least one third element is fixedly connected to said stator casing into a second position in which said at least one third element is separated from said stator casing and is free to rotate about said longitudinal axis.


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